COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-07-1012 INERT GAS SYSTEM - AIR SEPARATION UNIT - INSPECTION OF TUBES AND CLAMP INSTALLATION. SERVICE BULLETIN RECOMMENDED MOS 12-APR-2012 SB 737-09-1119 APU - ELECTRONIC CONTROL UNIT. SERVICE BULLETIN 10-JUN-1999 MOS - (s) SB 737-09-1133 AIRBORNE AUXILIARY POWER- AUXILARY POWER UNIT AIR INLET - AUXILARY POWER UNIT FLAP AND VORTEX GENERATOR ASSEMBLY MOSIFICATION. SERVICE BULLETIN MOS 22-SEP-2005 SB 737-09-1133 RI 21-SEP-2007 SB 737-09-1133 R2 26-JAN-2009 SB 737-09-1130 16-OCT-2007 MOS SB 737-09-1139 AIRBORNE AUXILIARY POWER - COWL DOOR INSULATION PANEL AND AFT BULKHEAD SEAL REPLACEMENT SUPERSEDED (SUPERSEDED BY S8 737-09-1139 RI). SERVICE BULLETIN MOS SB 737-09-1139 RI AIRBORNE AUXILIARY POWER -COWL DOOR INSULATION PANEL AND AFT BULKHEAD SEAL REPLACEMENT. SERVICE RECOMMENDED 04-OCT-2012 BULLETIN MOS SB 737-51-1017 RI EVES MOISTURE SHROUD SEAL INSTALLATION, SERVICE BULLETIN RECOMMENDED 28-MAR-2002 MOS SB 737-51-1018 CARGO DOORWAY STOP PAD REPLACEMENT. SERVICE BULLETIN RECOMMENDED AIRBORNE AUXILIARY POWER - AUXILIARY POWER UNIT AIR INLET - AUXILIARY POWER UNIT FLAP AND VORTEX GENERATOR ASSEMBLY MODIFICATION. SERVICE BULLETIN MOS AUXILIARY POWER UNIT FLAP AND VORTEX GENERATOR ASSEMBLY MODIFICATION. SERVICE BULLETIN MOS AIRBORNE AUXILIARY POWER - APU AIR INLET - INLET PLENUM REPLACEMENT. SERVICE BULLETIN RECOMMENDED I I -APR-2002 MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 101 Of 748 @ Camp Systems EFTA00618392

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-51-1019 25-APR-2002 STRUCTURES - WIRE SHIELD ASSEMBLY INSTALLATION UNDER THE E5-2 SHELF. SERVICE BULLETIN MOS SB 737-51-1019 RI STRUCTURES - WIRE SHIELD ASSEMBLY INSTALLATION UNDER THE E5-2 SHELF. SERVICE BULLETIN MOS 18-DEC-2003 SB 737-52-1136 EMERGENCY EXIT. SERVICE BULLETIN MOS 22-JUN-2000 - (s) SB 737-52-1137 DOORS - CONTROL CABIN EMERGENCY EXIT PANEL. SERVICE BULLETIN MOS - (s) SB 737-52-1138 ELECTRONIC EQUIPMENT ACCESS DOOR, SERVICE BULLETIN MOS 29-JUL-1999 - (s) SB 737-52-1140 FORWARD ENTRY - UPPER AFT CORNER DOOR STOP REPLACEMENT. SERVICE BULLETIN MOS 20-AUG-2001 RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED AFL 18000 (s) SB 737-52-1142 AFT GALLEY SERVICE DOOR, SERVICE BULLETIN RECOMMENDED MOS 4 (s) 22-FEB-2001 SB 737-52-1148 HORIZONTAL AIRSTAIRS MOISTURE SHROUD INSTALATION SUPPORT RAIL REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 12-DEC-2002 SB 737-52-1148 RI FUSELAGE - HORIZONTAL AIRSTAIRS MOISTURE SHROUD INSTALLATION - SUPPORT RAIL REPLACEMENT. SERVICE BULLETIN MOS 11-MAY-2006 SB 737-52-1152 DOORS - FORWARD AIRSTAIR DOOR RELIABILITY IMPROVEMENT - REPLACE DOOR LOCKPIN ACTUATORS. OPEN UMITAMARNING SWITCH BRACKETS. AND RACEWAY COVER ASSEMBLY. SERVICE BULLETIN MOS 08-SEP-2005 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 102 Of 748 @ Camp Systems EFTA00618393

CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YO006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-52-1156 01-DEC-2005 DOORS - FORWARD AIRSTAIR AND DOOR - FORWARD AIRSTAIR SPEEDUP AND SLOWDOWN SYSTEM DELETION. SERVICE BULLETIN MOS SB 737-52-1157 ENTRANCE STAIRS - FORWARD AIRSTAIR - AIRSTAIR HANDRAIL SAFETY IMPROVEMENTS (SUPERSEDED BY SB SUPERSEDED 737-52-1157 RI). SERVICE BULLETIN MOS SB 737-52-1157 RI DOORS - ENTRANCE STAIRS - FORWARD AIRSTAIR AIRSTAIR HANDRAIL SAFETY IMPROVEMENTS. SERVICE BULLETIN SB 737-52-1159 26-NOV-2C07 SB 737-52-1159 RI 21-SEP-2009 SB 737-52-1164 20-JAN-2009 SB 737-52-1165 29-JUL-2008 SB 737-52-1165 RI 15-JAN-2009 SB 737-52-1169 13-DEC-201 I MOS DOORS - DOOR WARNING SYSTEM - FORWARD ENTRY DOOR LATCH SWITCH AND WIRING INSTALLATION AND MODIFICATION. SERVICE BULLETIN MOS DOOR WARNING SYSTEM - FORWARD ENTRY DOOR LATCH SWITCH AND WIRING INSTALLATION AND MODIFICATION. SERVICE BULLETIN MOS FORWARD AND AFT CARGO DOORS - LANYARD ASSEMBLY REPLACEMENT. SERVICE BULLETIN MOS AFT ENTRY AND AFT GALLEY SERVICE DOOR - DOOR SNUBBER STOP LINK ASSEMBLY CHANGE. SERVICE BULLETIN MOS AFT ENTRY AND AFT GALLEY SERVICE DOOR - DOOR SNUBBER STOP LINK ASSEMBLY CHANGE. SERVICE BULLETIN MOS DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. SERVICE BULLETIN MOS RECOMMENDED SB 737-52-1169 TABLE 1 PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED SERVICE BULLETIN A GENERAL VISUAL INSPECTION OF THE INBOARD MLG DOOR FOR IDENTIFICATION MOS 13-DEC-2011 AFL 51)03(s1 ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 103 Of 748 Camp Systems EFTA00618394

CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YO006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-52-1169 TABLE 2.1L 13-DEC-2011 PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED SERVICE BULLETIN A DETAILED INSPECTION OF THE LEFT INBOARD MLG DOOR FOR ANY CRACKS MOS AFL 5500(s) SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 2.1R SERVICE BULLETIN A DETAILED INSPECTION OF THE RIGHT INBOARD MLG DOOR FOR ANY CRACKS MOS 13-DEC-2011 AFL 5500 (5) SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 2.2L SERVICE BULLETIN APPLICABLE SRM REPAIR WITHIN THE ALLOWABLE DAMAGE 1 LIMITS ( ANY PART-THROUGH CRACK IS FOUND.) LEFT MLG INBOARD DOOR MOS BF,'F (5) SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 2.2R SERVICE BULLETIN APPLICABLE SRM REPAIR WITHIN THE ALLOWABLE DAMAGE I LIMITS ( ANY PART-THROUGH CRACK IS FOUND.) RIGHT MLG INBOARD DOOR MOS BF,F (so SB 737-52-1169 TABLE REPLACE DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 2.3L SERVICE BULLETIN THE LEFT INBOARD MLG DOOR AND PREFORM A DETAILED INSPECTION OF THE INBOARD MLG DOOR FOR ANY CRACKS MOS BF,F (so SB 737-52-1169 TABLE REPLACE DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 2.3R SERVICE BULLETIN THE RIGHT INBOARD MLG DOOR AND PREFORM A DETAILED INSPECTION OF THE INBOARD MLG DOOR FOR ANY CRACKS MOS BF,F (so SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.1L SERVICE BULLETIN A DETAILED INSPECTION OF THE LEFT INBOARD MLG DOOR FOR ANY CRACKS MOS 13-DEC-2011 AFL 5503 (5) SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.1R SERVICE BULLETIN A DETAILED INSPECTION OF THE RIGHT INBOARD MLG DOOR FOR ANY CRACKS MOS 31-DEC-2011 AFL 5503 (5) ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 104 Of 748 Camp Systems EFTA00618395

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.2L SERVICE BULLETIN APPLICABLE SRM REPAIR WITHIN THE ALLOWABLE DAMAGE 1 LIMITS AND DETAILED INSPECTION OF THE LEFT INBOARD MLG DOOR MOS BFIF (s) SB 737-52-1169 TABLE PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.2R SERVICE BULLETIN APPLICABLE SRM REPAIR WITHIN THE ALLOWABLE DAMAGE 1 LIMITS AND DETAILED INSPECTION OF THE RIGHT INBOARD MLG DOOR MOS BF/F (s) SB 737-52-1169 TABLE REPLACE DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.3L SERVICE BULLETIN THE LEFT INBOARD MLG DOOR DOOR WITH INBOARD MLG DOOR MADE FROM MACHINED ALUMINUM. 113A8335-( ). OR INBOARD MLG DOOR MADE FROM CAST ALUMINUM. 113A8331-( ). AND DETAILED INSPECTION MOS BFIF (s) SB 737-52-1169 TABLE REPLACE DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOORS - INSPECTION AND REPAIR. RECOMMENDED 3.3R SERVICE BULLETIN THE RIGHT INBOARD MLG DOOR DOOR WITH INBOARD MLG DOOR MADE FROM MACHINED ALUMINUM. 113A8335-( ). OR INBOARD MLG DOOR MADE FROM CAST ALUMINUM. 113A8331- ). AND DETAILED INSPECTION SB 737-52-1170 29-JUL-2014 MOS BFIF (s) DOORS - LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR AND MODIFICATION. RECOMMENDED SERVICE BULLETIN MOS SB 737-52-1170 T84. 1.1 DETAILED INSPECTION DOORS - LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR RECOMMENDED AND MODIFICATION. SERVICE BULLETIN OF MLG CENTER DOOR ASSEMBLY ATTACHMENTS (PART 2) FOR ANY LOOSE. MISSING. DAMAGED OR BOTTOMED OUT BOLTS. OR ANY WEAR TO THE RETENTION CLIP ASSEMBLIES. OR IF RETENTION CLIP ASSEMBLIES ARE NOT INSTALLED. FOR ANY LOOSE. MISSING OR DAMAGED BOLTS (ALL AIRPLANES) MOS AFL 12000 (s) SB 737-52-1170 TB1 1.2 DO DOORS -LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR AND MODIFICATION. RECOMMENDED SERVICE BULLETIN PART 4: MLG CENTER DOOR ASSEMBLY ATTACHMENTS - REMOVAL! PART 5: MLG CENTER DOOR ASSEMBLY RETENTION CLIP ASSEMBLIES - MODIFICATION f REPEAT PART -2 (IF CONDITION 1: NO LOOSE. MISSING. DAMAGED OR BOTTOMED OUT BOLTS AND NO WEAR TO THE RETENTION CLIP ASSEMBLIES) MOS 29-JUL-2014 BFIF 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 105 Of 748 @ Camp Systems EFTA00618396

CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2O14 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-52-1170 TBL 1.3 DO DOORS - LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR AND MODIFICATION. RECOMMENDED SERVICE BULLETIN PART 3 MLG CENTER DOOR ASSEMBLY ATTACHMENTS - REMOVAL AND BUSHING DETAILED INSPECTION MEASUREMENT FOR EXCESSIVE WEAR. GALLING AND CRACKS (IF CONDITION 2: ANY LOOSE. MISSING. DAMAGED OR BOTTOMED OUT BOLTS. OR ANY WEAR TO THE RETENTION CLIP ASSEMBLIES) MOS 29-JUL-2014 BPIF SB 737-52-1170 TBL 1.4 DO DOORS - LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR AND MODIFICATION. RECOMMENDED SERVICE BULLETIN PART 7: BUSHING REMOVAL/ REPAIR. LUG MAGNETIC PARTICLE INSPECTION' REPAIR PART 5: MLG CENTER DOOR ASSEMBLY RETENTION CLIP ASSEMBLIES - MODIFICATION PART 7: BUSHING REMOVAL] REPAIR. LUG MAGNETIC PARTICLE INSPECTION' REPAIR PART 6: MLG CENTER DOOR ASSEMBLY BOLTS AND RETENTION CLIP ASSEMBLIES - REPLACEMENT REPEAT PART 2 (IF CONDITION 3: ANY EXCESSIVE WEAR FOUND IN THE INTERNAL DIAMETER OF THE BUSHING OR ANY GALLING FOUND OR ANY CRACK FOUND) MOS 29-JUL-2014 BPIF SB 737-52-1170 TBL 1.5 DO DOORS - LANDING GEAR CENTER DOOR ASSEMBLY ATTACHMENTS - INSPECTION. REPAIR AND MODIFICATION. RECOMMENDED SERVICE BULLETIN PART 5 MLG CENTER DOOR RETENTION CLIP ASSEMBLIES - MODIFICATION / PART 6: MLG CENTER DOOR ASSEMBLY BOLTS AND RETENTION CLIP ASSEMBLIES - REPLACEMENT I REPEAT PART 2 (IF CONDITION 4: NO EXCESSIVE WEAR FOUND IN THE INTERNAL DIAMETER OF THE BUSHING AND NO GALLING AND NO CRACKS FOUND) MOS 29-JUL-2014 BF.'F SB 737-52-1173 FORWARD AIRSTAIR - STAIR TREAD - ANTI-SLIP MATERIAL EDGE SEAL MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 24-JUN-201•I • (s) SB 737-52A1167 DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOOR HINGE FITTINGS - INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS (EFF) 01-DEC-201I SB 737-52A1167 TABLE 1 PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOOR HINGE FITTINGS - INSPECTION RECOMMENDED LMLG AND REPLACEMENT. SERVICE BULLETIN DETAILED INSPECTION OR HFEC INSPECTION OF THE LEFT INBOARD MLG DOOR HINGE FITTINGS FOR CRACKS FOR AIRPLANES MOS AFL 1C000 10000 SB 737-52A1167 TABLE 1 PERFORM DOORS - LANDING GEAR DOORS - INBOARD MAIN LANDING GEAR DOOR HINGE FITTINGS INSPECTION RECOMMENDED RMLG AND REPLACEMENT. SERVICE BULLETIN DETAILED INSPECTION OR SURFACE HFEC INSPECTION OF THE RIGHT INBOARD MLG DOOR HINGE FITTINGS FOR CRACKS MOS AFL 1C000 10000 ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 106 Of 748 Camp Systems EFTA00618397

CAMP MionistAlmthermumlitli AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1217 SECTION 43 AND SECTION 47 - STIR 17 SKIN CRACKS AT STA 364-371 AND STA 890-900. SERVICE BULLETIN MOS 09-AUG-2001 RECOMMENDED AFL 36000 (s) SS 737-53-1219 FUSELAGE SECTION 44- S18A WEB FITTING FLANGE CRACKS. INSPECTION AND REPAIR, SERVICE BULLETIN RECOMMENDED MOS I6-AUG-2001 AFL 30000 30000 SS 737-53-1222 FUSELAGE - SECTION 41 CAB - POINT D SPLICE FITTING REPLACEMENT (SUPERSEDED BY 737-53A1222 R1). SERVICE SUPERSEDED BULLETIN MOS 06-JUN-2002 SS 737-53-1223 29-NOV-2001 SS 737-53-1227 03-OCT-2002 SS 737-53-1227 RI 26-AUG-2006 SS 737-53-1227 R2 MAIN LANDING GEAR FAIRING REPLACEMENT. SERVICE BULLETIN MOS - Is) NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN MOS - (s) NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN MOS FUSELAGE - WHEEL WELLS - NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN MOS 22-AUG-2008 Id-NOV-2007 3260:48 RECOMMENDED RECERTIFY - INFORMATION REF TO R2 - INFORMATION REF TO R2 COMPUED WITH - TERMINATED AFL 782 SB 737-53-1227 R2 PARA REPLACE FUSELAGE - WHEEL WELLS - NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACE COMPUED WITH - REPLACEMENT 0 REPLACEMENT. SERVICE BULLETIN BUSHINGS MOS 22-AUG-2008 Id-NOV-2007 3260:48 AFL 782 SS 737-53-1227 R2 PARA INSPECT FUSELAGE - WHEEL WELLS - NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING COMPUED WITH - MIGRATION FOUND / E REPLACEMENT. SERVICE BULLETIN REPLACEMENT PERFORMED TERMINATING ACTION MOS 22-AUG-2008 3260:48 AFL 782 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 107 Of 748 @ Camp Systems EFTA00618398

CAMP Mianistfrn• thermiewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1227 R3 18-NOV-2009 SB 737-53-1227 R3 PARA DETAILED INSPECTION NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN E (DT INS) FOR CORROSION OF THE FITTINGS MOS 3 (s) NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN MOS RECOMMENDED SB 737-53-1227 R3 PARA INITIAL INSPECTION NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN RECOMMENDED E (I INSP) MOS 18-NOV-2009 AFL 2000(s) SB 737-53-1227 R3 PARA REPLACE NOSE WHEEL DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN BUSHING REPLACE E (RPL) 18-NOV-2009 SB 737-53-1232 SB 737-53-1232 RI SB 737-53-1232 RI TABLE SB 737-53-1232 R2 26-JUL-2013 SB 737-53-1232 R2 TABLE MOS 12 (s) FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTATIVE MODIFICATION (SUPERSEDED BY 737-53-1232 R1). SERVICE BULLETIN MOS SUPERSEDED FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTATIVE MODIFICATION SUPERSEDED (SUPERSEDED BY SB 737-53-1232 R2). SERVICE BULLETIN MOS DETAILED INSPECTION FUSELAGE - SKIN - CHEMICALLY MILLED STEPS- INSPECTION. REPAIR AND PREVENTATIVE RECOMMENDED MODIFICATION (SUPERSEDED BY SB 737-53-1232 R2). SERVICE BULLETIN AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKS IN THE FUSELAGE SKIN AT THE CHEM-MILLED STEPS AT SPECIFIED LOCATIONS MOS AFL 35000 35000 FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE RECOMMENDED BULLETIN MOS EXTERNAL - DETAILED INSPECTION FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND 1.01 PREVENTIVE MODIFICATION. SERVICE BULLETIN AND AN EXTERNAL NDI (EXT.MFECMCWC-SCAN/EXT.UTPA) FOR CRACKS IN THE FUSELAGE SKIN AT THE CHEM-MILLED STEPS AT SPECIFIED LOCATIONS (FOR AIRPLANES WITHOUT THE PREVENTATIVE MODIFICATION. TIME-LIMITED REPAIR OR PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 108 Of 748 @ Camp Systems EFTA00618399

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 737-53-1232 R2 TABLE REPAIR FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 1.02 SERVICE BULLETIN ANY CRACK THAT IS FOUND IN THE SKIN MOS SB 737-53-1232 R2 TABLE INSPECT FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 1A.01 SERVICE BULLETIN FOR CRACKS IN THE FUSELAGE SKIN AT THE CHEM-MILLED STEPS AT THE SPECIFIED LOCATIONS (FOR AIRPLANES WITH PREVENTATIVE MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SB AT OR BEFORE 30.000 TOTAL FC) MOS AFL SB 737-53-1232 R2 TABLE INSPECT FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 1A.02 SERVICE BULLETIN FOR CRACKS IN THE FUSELAGE SKIN AT THE CHEM-MILLED STEPS AT THE SPECIFIED LOCATIONS (FOR AIRPLANES WITH PREVENTATIVE MODIFICATION THAT WERE INSTALLED IN ACCORDANCE WITH THIS SB AFTER 30.000 TOTAL FC) MOS AFL 58 737-53-1232 R2 TABLE CONTACT FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 1A.03 SERVICE BULLETIN BOEING AND ACCOMPLISH THE WORK INSTRUCTED (IF ANY CRACK IS FOUND IN THE SKIN) MOS 58 737-53-1232 R2 TABLE HFEC FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 18.01.1 SERVICE BULLETIN INSPECTION FOR CRACKS (IF PREVENTATIVE MODIFICATION INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL 58 737-53-1232 R2 TABLE DEATILED INSPECTION FUSELAGE - SKIN - CHEMICALLY MILLED STEPS- INSPECTION. REPAIR AND PREVENTIVE 18.01.2 MODIFICATION. SERVICE BULLETIN FOR CRACKS AND ANY LOOSE OR MISSING FASTENERS (IF PREVENTATIVE MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS 58) MOS AFL SB 737-53-1232 R2 TABLE CONTACT FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 18.02 SERVICE BULLETIN BOEING AND ACCOMPLISH THE WORK INSTRUCTED (IF ANY CRACK FOUND IN THE SKIN) MOS SB 737-53-1232 R2 TABLE REPLACE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 18.03 SERVICE BULLETIN THE LOOSE OR MISSING FASTENER MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 109 Of 748 @ Camp Systems EFTA00618400

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1232 R2 TABLE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE 2.01.1.1 BULLETIN SKIN INSPECTION OPTION 1 - EXTERNAL LFEC FOR CRACKS (FOR AIRPLANES WITH THE PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE 2.01.1.2 BULLETIN SKIN INSPECTION OPTION 1 - DOUBLER INSPECTION: EXTERNAL LFEC FOR CRACKS AND AN EXTERNAL DETAILED INSPECTION FOR CRACKS AND LOOSE/MISSING FASTENERS (FOR AIRPLANES WITH THE PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION, SERVICE 2.01.2.1 BULLETIN SKIN INSPECTION OPTION 2 - EXTERNAL LFEC FOR CRACKS (FOR AIRPLANES WITH THE PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE 2.01.2.2 BULLETIN SKIN INSPECTION OPTION 2 - INTERNAL MFEC FOR CRACKS (FOR AIRPLANES WITH THE PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE 2.01.2.3 BULLETIN SKIN INSPECTION OPTION 2 - DOUBLER INSPECTION: EXTERNAL LFEC FOR CRACKS AND AN EXTERNAL DETAILED INSPECTION FOR CRACKS AND LOOSE/MISSING FASTENERS (FOR AIRPLANES WITH THE PERMANENT REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE REPAIR FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 2.02 SERVICE BULLETIN ANY CRACK FOUND (IF ANY CRACK IS FOUND IN THE SKIN) MOS SB 737-53-1232 R2 TABLE REPLACE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 2.03 SERVICE BULLETIN LOOSE AND MISSING FASTENERS (IF ANY LOOSE OR MISSING FASTENER) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 110 Of 748 @ Camp Systems EFTA00618401

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SS 737-53-1232 R2 TABLE INTERNAL FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 3.01.1 SERVICE BULLETIN / EXTERNAL DETAILED INSPECTION OF A TIME-LIMITED REPAIR FOR CRACKS AND LOOSE OR MISSING FASTENERS (FOR AIRPLANES WITH THE TIME-LIMITED REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE REPLACE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 3.01.2 SERVICE BULLETIN THE TIME-LIMITED REPAIR WITH THE PERMANENT REPAIR (FOR AIRPLANES WITH THE TIME-LIMITED REPAIR INSTALLED IN ACCORDANCE WITH THIS SB) MOS AFL SB 737-53-1232 R2 TABLE REPAIR FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 3.02 SERVICE BULLETIN ANY CRACK FOUND IN THE SKIN MOS SB 737-53-1232 R2 TABLE REPLACE FUSELAGE - SKIN - CHEMICALLY MILLED STEPS - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. 3.03 SERVICE BULLETIN LOOSE AND MISSING FASTENERS MOS SB 737-53-1232 TABLE 1 AIRPLANES WITHMJTHOUT THE PREVENTATIVE MODIFICATION INSTALLED. (SUPERSEDED BY 737-53-1232 RI). SUPERSEDED SERVICE BULLETIN MOS - (s) SB 737-53-1232 TABLE 2 AIRPLANES WITH THE PERMANENT REPAIR INSTALLED. (SUPERSEDED BY 737-53-1232 RI). SERVICE BULLETIN SUPERSEDED NOT APPLICABLE MOS - (s) SB 737-53-1232 TABLE 3 AIRPLANES WITH THE TIME-LIMITED REPAIR INSTALLED. INTERNAUEXTEFtNAL DETAILED INSPECTION OF A NOT APPLICABLE TIME-LIMITED REPAIR FOR CRACKS AND LOOSE OR MISSING FASTENERS AS GIVEN IN -PART IV - TIME-LIMITED REPAIR'.. SERVICE BULLETIN MOS 02-APR-2007 AFL 2500 (s) SB 737-53-1233 INSPECTION AND REPLACEMENT OF KEEL BEAM LOWER CHORD FORWARD SPLICE AT STATION 535. SERVICE BULLETIN DAYS 30 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 111 Of 748 @ Camp Systems EFTA00618402

C O MP Mien winin Mernund up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: O5-Aug-2O14 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1233 RI 28-FEB-2002 SB 737-53-1236 I I -JUL-2002 INSPECTION AND REPLACEMENT OF KEEL BEAM LOWER CHORD FORWARD SPLICE AT STATION 535. SERVICE BULLETIN MOS 18 (s) 25-JUL-2002 1057:48 AFL 271 AIRSTAIR DOORSTOP INTERCOSTAL - INSPECTION AND FASTENER REPLACEMENT. SERVICE BULLETIN MOS AFL 24000 (0 SB 737-53-1236 RI FUSELAGE - AIRSTAIR DOORSTOP INTERCOSTAL - INSPECTION AND FASTENER REPLACEMENT. SERVICE BULLETIN 10-NOV-2005 SB 737-53-1237 04-DEC-2003 SB 737-53-1237 RI 07-DEC-2006 SB 737-53-1239 22-AUG-2002 SB 737-53-1239 RI I4-AUG-2003 SB 737-53-1239 R2 28-APR-2005 SB 737-53-1239(A) 22-AUG-2002 SB 737-53-1239(E) 22-AUG-2002 MOS 29-AUG-2011 -(s) 3533:32 AFL FASTENER REPLACEMENT. SERVICE BULLETIN MOS 863 FUSELAGE - WING TO BODY FAIRING - WHEEL WELL - BONDED PANEL (BOW-TIE PANEL) - FASTENER REPLACEMENT. SERVICE BULLETIN MOS KEEL CHORD SPLICE WASHERS. BOLTS AND NUTS REPLACEMENT. SERVICE BULLETIN MOS KEEL CHORD SPLICE WASHERS. BOLTS. AND NUTS REPLACEMENT. SERVICE BULLETIN MOS 6 (s) FUSELAGE - KEEL BEAM LOWER CHORDS - FORWARD AND AFT SPLICES AT STATIONS 540 AND 727 - KEEL CHORD SPLICE WASHERS. BOLTS. AND NUTS REPLACEMENT. SERVICE BULLETIN MOS 6 (s) INSPECT KEEL CHORD SPLICE WASHERS. BOLTS AND NUTS REPLACEMENT. SERVICE BULLETIN MOS 6 (s) REPLACE KEEL CHORD SPLICE WASHERS. BOLTS AND NUTS REPLACEMENT. SERVICE BULLETIN MOS 6 (s) RECOMMENDED RECOMMENDED COMPUED WITH - REPLACEMENT COMPUED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 112 Of 748 @ Camp Systems EFTA00618403

COMP up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1243 AUTOMATIC OVERWING EXIT DOUBLERS (BEARSTRAPS) INSPECTION INTERVAL CHANGE. SERVICE BULLETIN MOS SB 26-SEP-2002 737-53-1244 AFL 75000 (s) PIVOT LINK ASSEMBLY REPAIR/REPLACE, SERVICE BULLETIN MOS SB 737-53-1244 RI PIVOT LINK ASSEMBLY REPAIR/REPLACE. SERVICE BULLETIN MOS SB 737-53-1244 RI (8)2 REPLACE PIVOT LINK ASSEMBLY REPAIR/REPLACE. SERVICE BULLETIN BLIND FASTENERS MOS AFL 10000 (s) SB 737-53-1244 R2 PIVOT LINK ASSEMBLY REPAIRIREPLACE. SERVICE BULLETIN MOS 12 (s) 15-MAR-2007 SB 737-53-1244 R2 (8)1 INSPECT PIVOT LINK ASSEMBLY REPAIR/REPLACE. SERVICE BULLETIN BLIND FASTNERS MOS 15-MAR-2007 AFL WOO (s) SB 737-53-1244 R2 (8)2 REPLACE PIVOT LINK ASSEMBLY REPAIR/REPLACE. SERVICE BULLETIN BLIND FASTNERS MOS 15-MAR-2007 AFL 10000 (s) SB 737-53-1244 R4 FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - PIVOT LINK ASSEMBLY REPAIR/REPLACE SUPERSEDED (SUPERSEDED BY S8 737-53-1244 R5), SERVICE BULLETIN MOS SB 737-53-1244 RS FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - PIVOT LINK ASSEMBLY REPAIR/REPLACE. SERVICE BULLETIN MOS 27-JUL-2011 SB 737-53-1244 R5 TABLE INSTALL FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540- PIVOT LINK ASSEMBLY REPAIR/REPLACE. RECOMMENDED 1.1 SERVICE BULLETIN NEW PIVOT LINK - NO CHANGES TO PIVOT LINK STRUCTURE AND PASSENGER SEATS HAVE NOT BEEN MOVED AFTER AIRPLANE DELIVERY MOS 12(s) I 7-APR-2003 RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time @ Camp Systems 113 Of 748 EFTA00618404

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1244 R5 TABLE ACCOMPLISH FUSELAGE - PASSENGER CABIN FLOORS- STATION 520 TO 540- PIVOT LINK ASSEMBLY RECOMMENDED 1.2 REPAIR/REPLACE. SERVICE BULLETIN MOVE THE SEATS - NO CHANGES TO PIVOT LINK STRUCTURE AND I 7-APR-2003 PASSENGER SEATS HAVE NOT BEEN MOVED AFTER AIRPLANE DELIVERY MOS 12 (s) 58 737-53-1244 RS TABLE INSTALL FUSELAGE - PASSENGER CABIN FLOORS- STATION 520 TO 540- PIVOT LINK ASSEMBLY FtEPAIRJREPLACE. RECOMMENDED 1.3 SERVICE BULLETIN BLIND CENTERLINE FASTNERS IN THE SEAT TRACK 17-APR-2003 MOS 12 (s) SB 737-53-1244 R5 TABLE INSPECT FUSELAGE - PASSENGER CABIN FLOORS- STATION 520 TO 540 - PIVOT UNK ASSEMBLY REPAIR/REPLACE. RECOMMENDED 1.3.1 SERVICE BULLETIN BLIND FASTENERS MOS AFL 3800 (s) SB 737-53-1244 RS TABLE REPLACE FUSELAGE - PASSENGER CABIN FLOORS- STATION 520 TO 540- PIVOT LINK ASSEMBLY REPAIR/REPLACE. RECOMMENDED 1.3.2 SERVICE BULLETIN BLIND FASTENERS WITH SOLID FASTENERS MOS AFL 10000 (s) 58 737-53-1244 R5 TABLE INSTALL FUSELAGE - PASSENGER CABIN FLOORS- STATION 520 TO 540- PIVOT LINK ASSEMBLY REPAIR/REPLACE. RECOMMENDED 1.4 SERVICE BULLETIN SOLID CENTERLINE FASTNERS IN THE SEAT TRACK 17-APR-2003 MOS 12 (s) 58 737-53-1244 R5 TABLE INSTALL FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540- PIVOT LINK ASSEMBLY REPAIR/REPLACE. RECOMMENDED 1.5 SERVICE BULLETIN NEW PIVOT LINK 27-JUL-2011 MOS 60 (s) SB 737-53-1245 HIGH PRESSURE DOOR AND DOUBLER-REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 05-AUG-2004 SB 737-53-1249 FUSELAGE - FRAMES AND BULKHEADS - BODY STATION 1016 AFT PRESSURE BULKHEAD - VERTICAL FIN ATTACHMENT FITTINGS -BOLT HOLE INSPECTION AND REPAIR. SERVICE BULLETIN MOS 16-NOV-2006 AFL 36000 (s) SB 737-53-1251 AFT PRESSURE BULKHEAD APEX INSPECTION. SERVICE BULLETIN MOS 22-AUG-2008 03-JUN-2004 3260:48 AFL 4000 (s) 782 COMPUED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 114 Of 748 @ Camp Systems EFTA00618405

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1252 13-OCT-2005 FUSELAGE - STABILIZER CENTER SECTION FRONT SPAR - SLIDING SEAL AND TRACK MODIFICATION. SERVICE BULLETIN MOS SB 737-53-1252 RI FUSELAGE - STABILIZER CENTER SECTION FRONT SPAR - SLIDING SEAL AND TRACK MODIFICATION.. SERVICE BULLETIN MOS 15-FEB-2007 SB 737-53-1256 CHEMICAL MILL PITTING AT S-4 LAP SPLICE. SERVICE BULLETIN MOS 18-SEP-2003 RECOMMENDED SB SB 737-53-1264 04-MAY-2006 737-53-1264 RI 24-JAN-2008 FUSELAGE - FILLET FAIRINGS - AFT WING-TO-BODY FAIRING - INBOARD FLAP PRIMARY TORQUE TUBE INSPECTION/REPAIR AND AFT WING-TO-BODY FAIRING MODIFICATION. SERVICE BULLETIN MOS FUSELAGE - FILLET FAIRINGS - AFT WING-TO-BODY FAIRING - INBOARD FLAP PRIMARY TORQUE TUBE INSPECTION/REPAIR AND AFT WING-TO-BODY FAIRING MODIFICATION, SERVICE BULLETIN MOS SB 737-53-1276 FUSELAGE - FORWARD AND AFT CARGO COMPARTMENT- CORROSION PREVENTION MODIFICATION (SUPERSEDED SUPERSEDED BY SB 737-53-1276 RI), SERVICE BULLETIN MOS SB 737-53-1276 RI FUSELAGE - FORWARD AND AFT CARGO COMPARTMENT - CORROSION PREVENTION MODIFICATION. SERVICE RECOMMENDED 01-AUG-2014 BULLETIN MOS - SB 737-53-1277 FUSELAGE - STRUCTURE ATTACHMENT FITTINGS - NOSE WHEEL WELL RETRACT ACTUATOR SUPPORT FITTING SUPERSEDED INSPECTION AND MODIFICATION (SUPERSEDED BY 737-53-1277 R1). SERVICE BULLETIN MOS 14-NOV-2007 SB 737-53-1277 RI FUSELAGE - STRUCTURE ATTACHMENT FITTINGS - NOSE WHEEL WELL RETRACT ACTUATOR SUPPORT FITTING INSPECTION AND MODIFICATION. SERVICE BULLETIN MOS 14-MAY-2010 SB 737-53-1280 22-MAY-2008 FUSELAGE - FILLET FAIRINGS - AFT OUTBOARD WING TO BODY FAIRING MODIFICATION. SERVICE BULLETIN MOS 74nsufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 115 Of 748 @ Camp Systems EFTA00618406

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1280 OPTION 1 INSTALL FUSELAGE - FILLET FAIRINGS - AFT OUTBOARD WING TO BODY FAIRING MODIFICATION. SERVICE BULLETIN MODIFICATION AS GIVEN IN PARAGRAPH 3.8.. WORK INSTRUCTIONS MOS 24 (s) 22-MAY-2008 SB 737-53-1280 OPTION 2 INSPECT FUSELAGE- FILLET FAIRINGS - AFT OUTBOARD WING TO BODY FAIRING MODIFICATION. SERVICE (A) BULLETIN AS GWEN IN PARAGRAPH 3.8.. WORK INSTRUCTIONS MOS 24 (5) 22-MAY-2008 SB 737-53-1280 OPTION 2 INSTALL FUSELAGE - FILLET FAIRINGS - AFT OUTBOARD WING TO BODY FAIRING MODIFICATION. SERVICE BULLETIN (3) MODIFICATION AS GIVEN IN PARAGRAPH 3.8., WORK INSTRUCTIONS MOS 72 (s) 22-MAY-2008 SB 737-53-1282 FUSELAGE - WHEEL WELL - NOSE WHEEL UPPER DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN MOS 14-NOV-2007 SB 737-53-1282 RI 14-MAR-2008 SB 737-53-1285 58 737-53-1285 RI 23-JUL-2014 FUSELAGE - WHEEL WELL - NOSE WHEEL UPPER DRAG BRACE AND TRUNNION BUSHING REPLACEMENT. SERVICE BULLETIN 61OS 22-AUG-2008 3260:48 AFL 782 FUSELAGE - PASSENGER CABIN FLOORS - SECTIONS 41 AND 47 - ADDITION OF GEL TAPE TO PREVENT CORROSION SUPERSEDED OF PASSENGER CABIN FLOOR PANEL SUPPORT STRUCTURE (SUPERSEDED BY SB 737-53-1285 RI ). SERVICE BULLETIN MOS FUSELAGE - PASSENGER CABIN FLOORS - SECTIONS 41 AND 47 - ADDITION OF GEL TAPE TO PREVENT CORROSION RECOMMENDED OF PASSENGER CABIN FLOOR PANEL SUPPORT STRUCTURE. SERVICE BULLETIN MOS 58 737-53-1294 FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SI3 737-53-1294 RI ). SERVICE BULLETIN MOS 58 737-53-1294 RI 12-JUN-2013 FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN MOS (EFF) SUPERSEDED RECOMMENDED COMPLIED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 116 Of 748 @ Camp Systems EFTA00618407

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1294 RI TABLE DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. 1.1 CHORD SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN AND A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE SKIN FOR CRACKS IN THE AREA AROUND THE EIGHT FASTENERS SECURING THE STA 540 BULKHEAD CHORDS BETWEEN STRINGER S-22 AND S-23 (AIRPLANES WITH LESS THAN 27.500 TOTAL FLIGHT CYCLES AS OF THE ORIGINAL ISSUE DATE OF THIS SERVICE BULLETIN) MOS SB 737-53-1294 RI TABLE DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. 1.2 CHORD SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN AND A HFEC INSPECTION OF THE SKIN FOR CRACKS IN THE AREA AROUND THE EIGHT FASTENERS SECURING THE STA 540 BULKHEAD CHORDS BETWEEN STRINGER S-22 AND S-23 (AIRPLANES WITH 27.500 OR MORE TOTAL FLIGHT CYCLES AS OF THE ORIGINAL ISSUE DATE OF THIS SERVICE BULLETIN) MOS 58 737-53-1294 RI TABLE REPAIR FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE 1.3 INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN THE CRACKING ON LEFT SIDE (AND) DO THE PREVENTIVE MODIFICATION ON THE RIGHT SIDE (IF ANY CRACK IS FOUND IN THE SKIN ON THE LEFT SIDE OF THE AIRPLANE AND NO CRACK IS FOUND ON THE RIGHT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE REPAIR FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPLICE 1.4 INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN THE CRACKING ON RIGHT SIDE (AND) DO THE PREVENTIVE MODIFICATION ON THE LEFT SIDE (IF ANY CRACK IS FOUND IN THE SKIN ON THE RIGHT SIDE OF THE AIRPLANE AND NO CRACK IS FOUND ON THE LEFT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE REPAIR FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE 1.5 INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN THE CRACKS (IF ANY CRACK IS FOUND IN THE SKIN ON BOTH SIDES OF THE AIRPLANE) MOS 58 737-53-1294 RI TABLE DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. 2.1.1 CHORD SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN OF THE SKIN SURROUNDING THE FILLER UNDER THE DRAG LINK ASSEMBLY FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD 2.1.2 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN EXTERNAL LOW FREQUENCY EDDY CURRENT (LFEC) INSPECTION OF THE SKIN AND DOUBLER AND AN EXTERNAL HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE TRIPLER FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 117 Of 748 @ Camp Systems EFTA00618408

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD 2.1.3 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN INTERNAL HFEC INSPECTION OF THE SKIN FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD 2.1.4 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN INTERNAL HFEC INSPECTION OF THE SPLICE PLATE AND STA 540 BULKHEAD OUTER CHORD FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. 2.2.1 CHORD SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN OF THE SKIN SURROUNDING THE FILLER UNDER THE DRAG LINK ASSEMBLY FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD 2.2.2 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN EXTERNAL LFEC INSPECTION OF THE SKIN AND DOUBLER AND AN EXTERNAL HFEC INSPECTION OF THE TRIPLER FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD 2.2.3 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN INTERNAL HFEC INSPECTION OF THE SKIN FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE ACCOMPLISH FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD 2.2.4 SPLICE INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN INTERNAL HFEC INSPECTION OF THE SPLICE PLATE AND STA 540 BULKHEAD OUTER CHORD FOR CRACKING (ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE) MOS SB 737-53-1294 RI TABLE CONTACT FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPUCE 2.3 INSTALLATION AND SKIN REPAIR. SERVICE BULLETIN BOEING FOR INSTRUCTIONS AND DO THE WORK (ANY CRACK IS FOUND) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 118 Of 748 @ Camp Systems EFTA00618409

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1294 TABLE 1.1 DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. RECOMMENDED CHORD SPLICE INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN AND A HFEC INSPECTION OF THE SKIN FOR CRACKS IN THE AREA AROUND THE EIGHT FASTENERS SECURING THE STA 540 BULKHEAD CHORDS BETWEEN STRINGER S-22 AND S-23 FOR AIRPLANES WITH LESS THAN 27.500 TOTAL FLIGHT CYCLES AS OF THE ORIGINAL ISSUE DATE OF THIS SERVICE BULLETIN MOS 31-MAR-2011 AFL 2000 (s) SB 737-53-1294 TABLE 1.2 DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. RECOMMENDED CHORD SPLICE INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN AND A HFEC INSPECTION OF THE SKIN FOR CRACKS IN THE AREA AROUND THE EIGHT FASTENERS SECURING THE STA 540 BULKHEAD CHORDS BETWEEN STRINGER S-22 AND S-23 FOR AIRPLANES WITH 27.500 OR MORE TOTAL FLIGHT CYCLES AS OF THE ORIGINAL ISSUE DATE OF THIS SERVICE BULLETIN. MOS 31-MAR-2011 SB 737-53-1294 TABLE 2.1.1 SB 737-53-1294 TABLE 2.1.2 SB 737-53-1294 TABLE 2.1.3 SB 737-53-1294 TABLE 2.1.4 AFL 750(s) DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. RECOMMENDED CHORD SPLICE INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN OF THE SKIN SURROUNDING THE FILLER UNDER THE DRAG LINK ASSEMBLY FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE MOS AFL 2500 (s) HFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE RECOMMENDED INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 RI). SERVICE BULLETIN EXTERNAL INSPECTION OF THE SKIN AND DOUBLER AND AN EXTERNAL HFEC INSPECTION OF THE TRIFLER FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE MOS AFL SCO0 (s) HFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE RECOMMENDED INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN INTERNAL INSPECTION OF THE SKIN FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE MOS AFL 5000 (s) HFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPLICE RECOMMENDED INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 RI). SERVICE BULLETIN INTERNAL INSPECTION OF THE SPLICE PLATE AND STA 540 BULKHEAD OUTER CHORD FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE LEFT SIDE OF THE AIRPLANE MOS AFL 5000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 119 Of 748 @ Camp Systems EFTA00618410

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1294 TABLE 2.2.1 DETAILED INSPECTION FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPLICE INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN OF THE SKIN SURROUNDING THE FILLER UNDER THE DRAG LINK ASSEMBLY FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE MOS RECOMMENDED AFL 2500 (5) SB 737-53-1294 TABLE LFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE RECOMMENDED 2.2.2 INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 RI). SERVICE BULLETIN EXTERNAL INSPECTION OF THE SKIN AND DOUBLER AND AN EXTERNAL HFEC INSPECTION OF THE TRIPLER FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE SB 737-53-1294 TABLE 2.2.3 SB 737-53-1294 TABLE 2.2.4 SB 737-53-1295 RI SB 737-53-1295 R2 18-JUN-20I3 SB 737-53-1295 R2 TABLE MOS AFL 5000 (s) HFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540- SKIN INSPECTION. CHORD SPLICE RECOMMENDED INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 R1). SERVICE BULLETIN INTERNAL INSPECTION OF THE SKIN FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE MOS AFL 5000 (s) HFEC FUSELAGE - SKIN - LOWER BULKHEAD CHORDS AT BODY STATION 540 - SKIN INSPECTION. CHORD SPLICE RECOMMENDED INSTALLATION AND SKIN REPAIR (SUPERSEDED BY SB 737-53-1294 RI). SERVICE BULLETIN INTERNAL INSPECTION OF THE SPLICE PLATE AND STA 540 BULKHEAD OUTER CHORD FOR CRACKING FOR ALL AIRPLANES THAT HAVE DONE THE SKIN REPAIR ON THE RIGHT SIDE OF THE AIRPLANE MOS AFL 5000(s) FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY REPLACEMENT SUPERSEDED (SUPERSEDED BY 93 737-53-1295 R2). SERVICE BULLETIN MOS FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY REPLACEMENT. RECOMMENDED SERVICE BULLETIN MOS EXTERNAL - DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER I WINDOW FRAME AND 1.1.1 WINDSHIELD ASSEMBLY REPLACEMENT. SERVICE BULLETIN OF THE CROWN SKIN FOR CORROSION (GROUP 1. CONFIGURATION 6: GROUP 2. CONFIGURATION 4) (ALL AIRPLANES) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 120 Of 748 @ Camp Systems EFTA00618411

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1295 R2 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD 1.1.2 ASSEMBLY REPLACEMENT. SERVICE BULLETIN FOR CORROSION AND INSTALL NEW FASTENERS (GROUP 1. CONFIGURATION 6: GROUP 2. CONFIGURATION 4) (ALL AIRPLANES) MOS - (s) SB 737-53-1295 R2 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY 1.2 REPLACEMENT. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED (IF CORROSION IS FOUND) MOS SB 737-53-1295 R2 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD 2.1 ASSEMBLY REPLACEMENT. SERVICE BULLETIN FOR CORROSION AND INSTALL NEW FASTENERS (ALL AIRPLANES) MOS - Is) SB 737-53-1295 R2 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY 2.2 REPLACEMENT. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED (IF CORROSION IS FOUND) SB 737-53-1296 11-JAN-2011 MOS FUSELAGE - PASSENGER CABIN FLOORS - STATION 7278 SPLICE STRAP INSTALLATION. SERVICE BULLETIN MOS SB 737-53-1296 TABLE 1.1 REPLACE FUSELAGE - PASSENGER CABIN FLOORS - STATION 727B SPLICE STRAP INSTALLATION. SERVICE RECOMMENDED BULLETIN SEAT TRACK BOLTS FOR ALL AIRPLANES MOS 24 (s) 11-JAN-2011 SB 737-53-1296 TABLE 1.2 DETAILED INSPECTION FUSELAGE - PASSENGER CABIN FLOORS - STATION 7278 SPLICE STRAP INSTALLATION. RECOMMENDED SERVICE BULLETIN AND HFEC INSPECTION OF SPLICE STRAP AND FORWARD SEAT TRACK FOR ALL AIRPLANES MOS 24 (s) 11-JAN-2011 SB 737-53-1297 FUSELAGE - EQUIPMENT ATTACHMENT FITTINGS- AFT CARGO WASTE TANK ENCLOSURE - STANCHION RECOMMENDED MODIFICATION. SERVICE BULLETIN MOS 03-SEP-2010 SB 737-53-1298 FUSELAGE - SKIN - DORSAL FIN SEAL RETAINER AND FUSELAGE SKIN STATION 847 TO 1007- INSPECTION. SERVICE BULLETIN MOS 27-AUG-2010 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 121 Of 748 @ Camp Systems EFTA00618412

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1298 TABLE 1.1/2 27-AUG-2010 INSPECTION FUSELAGE - SKIN - DORSAL FIN SEAL RETAINER AND FUSELAGE SKIN STATION 847 TO 1007- RECOMMENDED INSPECTION. SERVICE BULLETIN OF THE DORSAL FIN LOWER SEAL RETAINERS FOR CONTACT WITH THE FUSELAGE SKIN BETWEEN STA 847 AND STA 1007 IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 1 FOR ALL AIRPLANES MOS 24 (s) AFL 4000 SB 737-53-1298 TABLE 1.6 MODIFY FUSELAGE - SKIN - DORSAL FIN SEAL RETAINER AND FUSELAGE SKIN STATION 847 TO 1007 - INSPECTION. RECOMMENDED SERVICE BULLETIN THE LOWER AND VERTICAL SEALS IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5 FOR AIRPLANES THAT HAVE NOT MODIFIED THE LOWER AND VERTICAL SEALS OR. REPLACED THE LOWER SEAL IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 4. MOS 24 (s) 27-AUG-20I0 SB 737-53-1303 513 737-53-1303 RI 06-MAY-2014 513 737-53-1303 RI TBL 1.1 513 737-53-1303 RI TBL 1.2 06-MAY-2014 SB 737-53-1303 RI TBL AFL 4000 FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG SUPERSEDED INSTALLATION (SUPERSEDED BY SB 737-53-1303 RI). SERVICE BULLETIN MOS FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG RECOMMENDED INSTALLATION. SERVICE BULLETIN MOS HIGH FREQUENCY EDDY CURRENT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG INSTALLATION. SERVICE BULLETIN (HFEC) INSPECTION OF THE AFFECTED NUMBER 3 WINDOW FRAME FASTENER HOLES FOR CRACKS. COLD WORK AND INSTALL FREEZE PLUGS IN AFFECTED NUMBER 3 WINDOW FRAME HOLES MOS AFL INSTALL FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE RECOMMENDED PLUG INSTALLATION. SERVICE BULLETIN TEMPORARY REPAIR STRAP OR INSTALL THE NUMBER 3 WINDOW FRAME PERMANENT REPAIR (ANY CRACK INDICATION FOUND) MOS BFIF REPLACE FUSELAGE- STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME- INSPECTION AND FREEZE RECOMMENDED 1.3 PLUG INSTALLATION. SERVICE BULLETIN THE NUMBER 3 WINDOW FRAME OR INSTALL THE NUMBER 3 WINDOW FRAME PERMANENT REPAIR (IF ANY CRACK FOUND BEYOND THE TEMPORARY REPAIR STRAP INSTALLATION UMITS) MOS 06-MAY-2014 BF/F 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 122 Of 748 @ Camp Systems EFTA00618413

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1303 RI TBL EXTERNAL - DETAILED INSPECTION FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG INSTALLATION. SERVICE BULLETIN OF THE TEMPORARY REPAIR STRAP FOR CORROSION AND ANY OTHER NICKS. GAPS. LOOSE FASTENERS OR MISSING SEALANT (IF TEMPORARY REPAIR STRAP INSTALLED) MOS - (s) SB 737-53-1303 RI TBL REPLACE FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE 1.4.2 PLUG INSTALLATION. SERVICE BULLETIN THE NUMBER 3 WINDOW FRAME (IF TEMPORARY REPAIR STRAP INSTALLED) MOS - Is) SB 737-53-1303 RI TBL EXTERNAL - DETAILED INSPECTION FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - 1.5.1 INSPECTION AND FREEZE PLUG INSTALLATION. SERVICE BULLETIN OF THE TEMPORARY REPAIR STRAP FOR CORROSION AND ANY OTHER NICKS. GAPS. LOOSE FASTENERS OR MISSING SEALANT (IF TEMPORARY REPAIR STRAP OPTION 2 WITH STRAIGHT LINE FASTENER PATTERN INSTALLED) MOS - (s) SB 737-53-1303 RI TBL INSTALL FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE 1.5.2 PLUG INSTALLATION. SERVICE BULLETIN THE NUMBER 3 WINOW FRAME PERMANENT REPAIR OR REPLACE THE NUMBER 3 WINDOW FRAME (IF TEMPORARY REPAIR STRAP OPTION 2 WITH STRAIGHT LINE FASTENER PATTERN INSTALLED) MOS - (s) SB 737-53-1303 RI TBL REPLACE FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE RECOMMENDED 1.6 PLUG INSTALLATION. SERVICE BULLETIN THE NUMBER 3 WINDOW FRAME OR INSTALL THE NUMBER 3 WINDOW FRAME PERMANENT REPAIR (IF ANY CRACK FOUND AROUND THE NUMBER 3 WINDOW FRAME REPAIR FASTENERS COMMON TO THE TEMPORARY REPAIR STRAP) MOS OS-MAY-20M BF/F SB 737-53-1303 TABLE 1.1 HFEC FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG SUPERSEDED INSTALLATION (SUPERSEDED BY SB 737-53-1303 R1). SERVICE BULLETIN INSPECTION OF THE AFFECTED NUMBER 3 WINDOW FRAME FASTENER HOLES FOR CRACKS. COLD WORK AND INSTALL FREEZE PLUGS IN AFFECTED NUMBER 3 WINDOW FRAME HOLES FOR ALL AIRPLANES SB 737-53-1303 TABLE 1.4.1 MOS - Is) HFEC FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE PLUG SUPERSEDED INSTALLATION (SUPERSEDED BY SB 737-53-1303 R1). SERVICE BULLETIN - INTERNAL INSPECTION OF THE NUMBER 3 WINDOW FRAME MOUND THE REPAIR FASTENERS COMMON TO THE TEMPORARY REPAIR STRAP FOR CRACKS AND DO A GENERAL VISUAL INSPECTION OF THE TEMPORARY REPAIR STRAP FOR TEMPORARY REPAIR STRAP INSTALLED AIRPLANES MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 123 Of 748 @ Camp Systems EFTA00618414

COMP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1303 TABLE REPLACE FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - INSPECTION AND FREEZE SUPERSEDED 1.4.2 PLUG INSTALLATION (SUPERSEDED BY SB 737-53-1303 RI). SERVICE BULLETIN THE NUMBER 3 WINDOW FRAME MOS - S8 737-53-1307 FUSELAGE - FILLET FAIRINGS - AFT WING TO BODY FAIRING - PANEL 194E AND AFT CENTER WHEEL WELL PANEL RECOMMENDED 193D - INSPECTION AND REWORK. SERVICE BULLETIN 12-JAN-2012 MOS SB 737-53-1307 TABLE 1.1 PERFORM FUSELAGE - FILLET FAIRINGS - AFT WING TO BODY FAIRING - PANEL 194E AND AFT CENTER WHEEL WELL RECOMMENDED PANEL 193D - INSPECTION AND REWORK. SERVICE BULLETIN A GENERAL VISUAL INSPECTION OF THE LOWER AFT WING TO BODY FAIRING PANEL AND SUPPORT STRUCTURE MOS 24 (s) 12-JAN-2012 SB 737-53-1307 TABLE 1.4 PERFORM FUSELAGE - FILLET FAIRINGS -AFT WING TO BODY FAIRING -PANEL 194E AND AFT CENTER WHEEL WELL RECOMMENDED PANEL 193D - INSPECTION AND REWORK. SERVICE BULLETIN THE PANEL AND SUPPORT STRUCTURE REWORK MOS 72 (s) 12-JAN-2012 SB 737-53-1310 FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND MODIFICATION RECOMMENDED . SERVICE BULLETIN MOS 20-OCT-2011 SB 737-53-1310 TABLE 1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL DETAILED INSPECTION AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEPS AT SPECIFIED LOCATIONS OPTION 1 OR OPTION 2 FOR ALL AIRPLANES MOS 20-OCT-2011 AFL 1500(s) SB 737-53-1310 TABLE 2.1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN INSPECTION OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION DOUBLER OPTION 1 OR OPTION 2 FOR AU. EXTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS AFL 50000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 124 Of 748 @ Camp Systems EFTA00618415

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1310 TABLE 2.2 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL INSPECTION OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION FILLER OPTION 1 OR OPTION 2 FOR ALL INTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS AFL 50000 (s) SB 737-53-1310 TABLE 3 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL INSPECTION OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION FILLER OPTION 1 OR OPTION 2 FOR ALL INTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS AFL 50000 (s) SB 737-53-1310 TABLE 4 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL INSPECTION OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION FILLER OPTION 1 OR OPTION 2 FOR ALL INTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS AFL 50000 (s) 58 737-53-1310 TABLE 5.1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN BEFORE 32.000 TOTAL FLIGHT CYCLES MOS AFL 50000 (s) SB 737-53-1310 TABLE 5.2 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 31.999 TOTAL FLIGHT CYCLES BUT BEFORE 43.000 TOTAL FLIGHT CYCLES MOS AFL 43000 (s) SB 737-53-1310 TABLE 5.3 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NDI - FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 42.999 TOTAL FLIGHT CYCLES MOS AFL 5500 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 125 Of 748 @ Camp Systems EFTA00618416

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1310 TABLE 6.1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN BEFORE 32.000 TOTAL FLIGHT CYCLES MOS AFL 50000 (s) 513 737-53-1310 TABLE 6.2 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 31.999 TOTAL FLIGHT CYCLES BUT BEFORE 43.000 TOTAL FLIGHT CYCLES MOS AFL 5500 (s) SB 737-53-1310 TABLE 6.3 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN DO AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 42.999 TOTAL FLIGHT CYCLES MOS AFL 5500(s) 513 737-53-1310 TABLE 7.1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN BEFORE 32.000 TOTAL FLIGHT CYCLES MOS AFL 50000 (s) SB 737-53-1310 TABLE 7.2 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 31.999 TOTAL FLIGHT CYCLES BUT BEFORE 43.000 TOTAL FLIGHT CYCLES MOS AFL 5500(s) SB 737-53-1310 TABLE 7.3 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED MODIFICATION . SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 42.999 TOTAL FLIGHT CYCLES MOS AFL 5500 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 126 Of 748 @ Camp Systems EFTA00618417

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1311 21-OCT-201 I FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN MOS AFL 28-MAY-20I3 3714:04 900 NOT APPLICABLE - N/A BY AIRCRAFT MODEL SB 737-53-1311 TABLE 1 EXTERNAL - DETAILED INSPECTION FUSELAGE - SKIN - CHEK1-MILL STEPS IN CROWN SKINS AT SPECIFIED RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEPS AT SPECIFIED LOCATIONS FOR ALL AIRPLANES MOS 21-OCT-2011 - (s) 28-MAY-20I3 3714:04 AFL 900 SB 737-53-1311 TABLE 2 EXTERNAL - DETAILED INSPECTION FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) OF THE FUSELAGE SKIN FOR CRACKING AT THE CHEM-MILL STEPS COMMON TO SHEAR WRINKLE AREAS FOR ALL AIRPLANES. GROUP 2.5-6 MOS 28-MAY-2013 21-OCT-2011 -(s) 3714:04 AFL 900 SB 737-53-1311 TABLE 3.1 NON DESTRUCTIVE FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL AND MODIFICATION. SERVICE BULLETIN INSPECTION OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION DOUBLER FOR ALL EXTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS - (s) 28-MAY-2013 3714:04 AFL 900 SB 737-53-1311 TABLE 3.2 EXTERNAL INSPECTION FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL INSPECTION AND MODIFICATION. SERVICE BULLETIN OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION FILLER FOR ALL INTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS 28-MAY-2013 - (s) 3714:04 AFL 900 SB 737-53-1311 TABLE 4.1 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN BEFORE 32.000 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 AFL 5500 (s) 900 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 127 Of 748 @ Camp Systems EFTA00618418

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1311 TABLE 4.2 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 31.999 TOTAL FLIGHT CYCLES BUT BEFORE 43,000 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 AFL 5500 (s) 900 SB 737-53-1311 TABLE 4.3 PERFORM FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN AN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 42.999 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 AFL 5500 (s) 900 SB 737-53-1312 FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN MOS 28-MAY-2013 21-OCT-2011 3714:04 NOT APPLICABLE - N/A BY AIRCRAFT MODEL AFL 900 SB 737-53-1312 RI FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS- INSPECTION AND MODIFICATION. RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL SERVICE BULLETIN MOS 28-MAY-2013 I4-MAR-2012 3714:04 AFL 900 SB 737-53-1312 TABLE 1 EXTERNAL - DETAILED INSPECTION FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEPS AT SPECIFIED LOCATIONS AND OPTION 1 (OR) OPTION 2 FOR ALL AIRPLANES MOS 28-MAY-2013 21-OCT-2011 -(s) 3714:04 AFL 900 SB 737-53-1312 TABLE 2 EXTERNAL - DETAILED INSPECTION FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL LOCATIONS - INSPECTION AND MODIFICATION. SERVICE BULLETIN AND AN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) OF THE FUSELAGE SKIN FOR CRACKING AT THE CHEM-MILL STEPS AT SPECIFIED LOCATIONS AND OPTION 1 (OR) OPTION 2 FOR ALL AIRPLANES MOS 28-MAY-2013 21-OCT-2011 -(s) 3714:04 AFL 900 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 128 Of 748 @ Camp Systems EFTA00618419

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1312 TABLE 3 EXTERNAL INSPECTION FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS- INSPECTION AND MODIFICATION. SERVICE BULLETIN OF THE FUSELAGE SKIN FOR CRACKING AT THE OUTER ROW OF FASTENERS COMMON TO THE MODIFICATION FILLER AND OPTION 1 (OR) OPTION 2 FOR ALL INTERNAL MODIFICATIONS INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN MOS - (s) 28-MAY-2013 3714:04 RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL AFL 900 SB 737-53-1312 TABLE 4.1 ACCOMPLISH FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN EXTERNAL NON DESTRUCTIVE INSPECTION (NDI) FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN BEFORE 32.000 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 AFL 5500 (s) 900 SB 737-53-1312 TABLE 4.2 ACCOMPLISH FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 31.999 TOTAL FLIGHT CYCLES BUT BEFORE 43.000 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 AFL 5500 (s) 900 SB 737-53-1312 TABLE 4.3 ACCOMPLISH FUSELAGE - SKIN - CHEM-MILL STEPS IN CROWN SKINS AT SPECIFIED LOCATIONS - INSPECTION AND RECOMMENDED NOT APPLICABLE - N/A BY AIRCRAFT MODEL MODIFICATION. SERVICE BULLETIN EXTERNAL NDI FOR CRACKING IN THE FUSELAGE SKIN AT THE CHEM-MILL STEP AT THE SPECIFIED LOCATIONS FOR ALL INTERNAL MODIFICATIONS THAT WERE INSTALLED IN ACCORDANCE WITH THIS SERVICE BULLETIN AFTER 42.999 TOTAL FLIGHT CYCLES MOS 28-MAY-2013 3714:04 SB 737-53-1316 SB 737-53-1316 RI 03-JUL-2013 SB 737-53-1316 RI TABLE AFL 5500 (s) 900 FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY REPLACEMENT SUPERSEDED AND HEAD UP DISPLAY REALIGNMENT (SUPERSEDED BY SB 737-53-1316 R1). SERVICE BULLETIN MOS FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY REPLACEMENT RECOMMENDED AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN MOS EXTERNAL - DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND 1.1.1 WINDSHIELD ASSEMBLY REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN OF THE CROWN SKIN FOR CORROSION FOR ALL AIRPLANES (GROUP 1. CONFIGURATION 6) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 129 Of 748 @ Camp Systems EFTA00618420

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1316 R1 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD 1.1.2 ASSEMBLY REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN FOR CORROSION AND INSTALL NEW FASTENERS FOR ALL AIRPLANES (GROUP 1. CONFIGURATION 6) MOS SB 737-53-1316 RI TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY 1.2 REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF CORROSION IS FOUND (GROUP 1. CONFIGURATION 6) MOS SB 737-53-1316 RI TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD 2.1 ASSEMBLY REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN FOR CORROSION AND INSTALL NEW FASTENERS FOR ALL AIRPLANES (GROUP 1. CONFIGURATION 5) MOS SB 737-53-1316 RI TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - NUMBER 1 WINDOW FRAME AND WINDSHIELD ASSEMBLY 2.2 REPLACEMENT AND HEAD UP DISPLAY REALIGNMENT. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF CORROSION IS FOUND (GROUP 1. CONFIGURATION 5) MOS SB 737-53-1326 FUSELAGE - CARGO COMPARTMENT SIDEWALL LININGS - INSPECTION AND REPAIR. SERVICE BULLETIN MOS 26-OCT-2012 RECOMMENDED SB 737-53-1326 TABLE 1.1 INSPECTION FUSELAGE - CARGO COMPARTMENT SIDEWALL LININGS - INSPECTION AND REPAIR. SERVICE BULLETIN RECOMMENDED OF THE FORWARD AND AFT CARGO COMPARTMENTS SIDEWALL PANELS FOR ALL AIRPLANES MOS 24 (5) 26-OCT-2012 SB 737-53-1326 TABLE 1.2 REMOVE FUSELAGE - CARGO COMPARTMENT SIDEWALL LININGS - INSPECTION AND REPAIR. SERVICE BULLETIN RECOMMENDED AND REPLACE ALUMINUM SIDEWALL LININGS MOS 60 (s) 26-OCT-2012 SB 737-53-1330 FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. RECOMMENDED SERVICE BULLETIN MOS 26-FEB-2013 SB 737-53-1330 RI FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. RECOMMENDED SERVICE BULLETIN MOS 10-JUN-2013 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 130 Of 748 @ Camp Systems EFTA00618421

C O MP Atiant.fran Meowed lip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1330 TABLE 1 (1.1.1) DO FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. SERVICE BULLETIN A HFEC INSPECTION OF THE CRACK IN THE NUMBER 1 WINDOW FRAME TO DETERMINE IF THE CRACK HAS GROWN BEYOND THE ALLOWABLE STOP DRILL REGION AND STOP DRILL THE CRACK IF WITHIN THE ALLOWABLE STOP DRILL REGION MOS BF/F RECOMMENDED SB 737-53-1330 TABLE 1 OO FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. RECOMMENDED (1.1.2) SERVICE BULLETIN A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION ABOVE AND BELOW THE CRACKED NUMBER 1 WINDOW FRAME AROUND THE FASTENERS THAT HOLD THE NUMBER 1 AND NUMBER 2 WINDOW FRAMES TOGETHER MOS BF/F SB 737-53-1330 TABLE 1 OO FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. RECOMMENDED (1.1.3) SERVICE BULLETIN A DETAILED INSPECTION OF THE AREA TWO INCHES ABOVE AND BELOW THE CRACK MOS BF/F SB 737-53-1330 TABLE 1 INSTALL FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY RECOMMENDED (1.1.4) REPAIR. SERVICE BULLETIN THE TEMPORARY REPAIR DOUBLER ON THE NUMBER 1 WINDOW FRAME MOS BF/F SB 737-53-1330 TABLE 1 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY RECOMMENDED (1.2) REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING. FOR CRACK FOUND OUTSIDE OF THE UPPER AFT CORNER AREA OF THE NUMBER 1 WINDOW FRAME MOS BF1F SB 737-53-1330 TABLE 1 OO FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY REPAIR. RECOMMENDED (1.3.1) SERVICE BULLETIN AN EXTERNAL DETAILED INSPECTION FOR CORROSION AND ANY OTHER NICKS. GAPS. LOOSE FASTENERS OR MISSING SF41 ANT FOR TEMPORARY REPAIR DOUBLER INSTALLED MOS 6 (s) SB 737-53-1330 TABLE 1 REPLACE FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER I WINDOW FRAME CRACKING - TEMPORARY RECOMMENDED (1.3.2) REPAIR. SERVICE BULLETIN THE NUMBER 1 WINDOW FRAME FOR TEMPORARY REPAIR DOUBLER INSTALLED MOS 24 (s) AFL 6000 SB 737-53-1330 TABLE 1 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME CRACKING - TEMPORARY RECOMMENDED (1.4) REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING FOR ANY CRACK FOUND AROUND THE NUMBER 1 WINDOW FRAME FASTENERS COMMON TO THE TEMPORARY REPAIR DOUBLER MOS BF/F 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 131 Of 748 @ Camp Systems EFTA00618422

CAMP Mianistfrn• thermiewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1334 04-AUG-2014 SB 737-53-1334 TBL 1.1.1 SB 737-53-1334 TBL 1.1.2 SB 737-53-1334 TBL 1.3 04-AUG-2014 SB 737-53-1334 TBL 1.5 04-AUG-2014 SB 737-53-1334 TBL 2.1.1 SB 737-53-1334 T/31. 2.12 FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN MOS - (s) RECOMMENDED OO FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN PART 2: CROWN RECOMMENDED SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - HIGHER STRESS LOCATIONS (ALL AIRPLANES) (GROUP 1-5) MOS AFL 7500 (s) OO FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN PART 3: CROWN RECOMMENDED SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - LOWER STRESS LOCATIONS (ALL AIRPLANES) (GROUP 1-5) MOS AFL 10000 (s) CONTACT FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN THE BOEING RECOMMENDED COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR! REPEAT PART 2: CROWN SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - HIGHER STRESS LOCATIONS (IF CONDITION 2: ANY CRACK FOUND (DURING PART 2 MFEC INSPECTION OF HIGHER STRESS LOCATIONS)) (GROUP 1-5) MOS BFIF (s) CONTACT FUSELAGE -CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN THE BOEING RECOMMENDED COMPANY FOR REPAIR INSTRUCTIONS AND OO THE REPAIR! REPEAT PART 3: CROWN SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - LOWER STRESS LOCATIONS (IF CONDITION 2 ANY CRACK FOUND (DURING PART 3 MFEC INSPECTION OF LOWER STRESS LOCATIONS)) (GROUP 1-5) MOS BFIF (s) OO FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN PART 2: CROWN RECOMMENDED SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - HIGHER STRESS LOCATIONS (ALL AIRPLANES) (GROUP 6) MOS AFL 7500 (s) OO FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN PART 3: CROWN RECOMMENDED SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - LOWER STRESS LOCATIONS (ALL AIRPLANES) (GROUP 6) MOS AFL 20O00 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 132 Of 748 @ Camp Systems EFTA00618423

CAMP Aiont.inn• AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YO006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2O14 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1334 TBL 2.3 CONTACT FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN THE BOEING RECOMMENDED COMPANY REPAIR INSTRUCTIONS AND DO THE REPAIR/REPEAT PART 2: CROWN SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC)INSPECTION - HIGHER STRESS LOCATIONS (B) MOS 04-AUG-2014 BF/F (s) SB 737-53-1334 TBL 2.5 CONTACT FUSELAGE - CROWN SKIN - CHEM MILL POCKET TROUGH INSPECTIONS. SERVICE BULLETIN THE BOEING RECOMMENDED COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR/ REPEAT PART 3: CROWN SKIN PANEL ASSEMBLY - EXTERNAL MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION - LOWER STRESS LOCATIONS (IF CONDITION 3: ANY CRACK FOUND (DURING PART 3 MFEC INSPECTION OF LOWER STRESS LOCATIONS)) (GROUP 6) MOS 04-AUG-2014 SB 737-53-1335 31-JUL-2013 BF/F (s) FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS SB 737-53-1335 TABLE 11 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN NUMBER 1 WINDOW FRAME DETAILED AND HFEC INSPECTION FOR ANY CRACK INDICATION (FOR ALL AIRPLANES) (GROUP 1. CONFIGURATION 1-3) MOS AFL SB 737-53-1335 TABLE 1.2 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN NUMBER 1 WINDOW FRAME PREVENTIVE MODIFICATION DOUBLER INSTALLATION (IF NO CRACK INDICATION FOUND) (GROUP 1. CONFIGURATION 1-3) MOS AFL SB 737-53-1335 TABLE 1.3 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN NUMBER 1 WINDOW FRAME TEMPORARY REPAIR INSTALLATION OR REPLACEMENT (IF ANY CRACK INDICATION FOUND) (GROUP 1. CONFIGURATION 1-3) MOS SB 737-53-1335 TABLE 2.1 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN POST PREVENTIVE MODIFICATION DOUBLER INSTALLATION SEALANT INSPECTION (FOR AIRPLANES WITH THE PREVENTIVE MODIFICATION DOUBLER INSTALLED) (GROUP 1. CONFIGURATION 1-3) MOS AFL SB 737-53-1335 TABLE 2.3 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN SEALANT APPLICATION (IF SEALANT CRACKS. EROSION. SPLITS. LOOSE BEADS OR MISSING SECTIONS FOUND) (GROUP I. CONFIGURATION 1-3) MOS ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time 133 Of 748 '2 Camp Systems EFTA00618424

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1335 TABLE 3.1 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER I WINDOW FRAME - MODIFICATION. SERVICE BULLETIN POST PREVENTIVE MODIFICATION DOUBLER INSTALLATION WINDOW FRAME DETAILED AND HFEC INSPECTION (FOR AIRPLANES WITH THE PREVENTIVE MODIFICATION DOUBLER INSTALLED) (GROUP 1. CONFIGURATION 1-3) MOS AFL SB 737-53-1335 TABLE 3.3 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - MODIFICATION. SERVICE BULLETIN BOEING (IF ANY CRACK INDICATION FOUND) (GROUP 1. CONFIGURATION 1-3) SB 737-53-1336 23-OCT-2013 MOS FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 11MNDOW FRAME - PERMANENT REPAIR. SERVICE RECOMMENDED BULLETIN MOS SB 737-53-1336 TABLE 1.1 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN PART 12: POST PERMANENT REPAIR INSTALLATION NUMBER 1 WINDOW FRAME AND PERMANENT REPAIR TRIPLER HFEC INSPECTION (AIRPLANES WITH THE PERMANENT REPAIR DOUBLER AND TRIPLER INSTALLED) MOS AFL SB 737-53-1336 TABLE 1.2 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN PART 12: POST PERMANENT REPAIR INSTALLATION NUMBER 1 WINDOW FRAME AND PERMANENT REPAIR TRIPLER HFEC INSPECTION (CONDITION 1: NO CRACK INDICATION FOUND) MOS AFL SB 737-53-1336 TABLE 1.3 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (CONDITION 2: ANY CRACK INDICATION FOUND) MOS SB 737-53-1336 TABLE 2.1 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN PART 13: POST PERMANENT REPAIR INSTALLATION FUSELAGE SKIN LFEC INSPECTION (AIRPLANES WITH THE PERMANENT REPAIR DOUBLER AND TRIPLER INSTALLED) MOS AFL 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 134 Of 748 @ Camp Systems EFTA00618425

CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1336 TABLE 2.2 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN PART 13: POST PERMANENT REPAIR INSTALLATION FUSELAGE SKIN LFEC INSPECTION (CONDITION 1: NO CRACK INDICATION FOUND) MOS AFL SB 737-53-1336 TABLE 2.3 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - PERMANENT REPAIR. SERVICE BULLETIN THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (CONDITION 2: ANY CRACK INDICATION FOUND) MOS SB 737-53-1341 FUSELAGE - MISCELLANEOUS EXTERIOR SERVICE DOORS - EXTERNAL POWER RECEPTACLE DOOR - BONDING SUPERSEDED JUMPER INSPECTION AND REPLACEMENT (SUPERSEDED BY SB 737-53-1341 R1). SERVICE BULLETIN MOS SB 737-53-1341 RI FUSELAGE - MISCELLANEOUS EXTERIOR SERVICE DOORS - EXTERNAL POWER RECEPTACLE DOOR - BONDING RECOMMENDED JUMPER INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS 11-APR-2014 SB 737-53-1345 FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR RECOMMENDED . SERVICE BULLETIN MOS 05-NOV-2013 SB 737-53-1345 TABLE 1.1 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 1 NUMBER 3 WINDOW FRAME INSPECTION. COLD WORKING AND FREEZE PLUG INSTALLATION (AIRPLANES THAT COULD NOT BE REPAIRED WITH THE MAXIMUM FREEZE PLUG DIAMETER ALLOWED IN ACCORDANCE WITH BOEING SERVICE BULLETIN 737-53.1303) MOS SB 737-53-1345 TABLE 1.2.1 SB 737-53-1345 TABLE 1.2 .2 AFL ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 2: NUMBER 3 WINDOW FRAME SEPARATION (CONDITION 1: CRACK IN SECOND LOWER CORNER FASTENER HOLE THAT CANNOT BE REMOVED WITH A 0.450 INCH DIAMETER FREEZE PLUG) MOS ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 3: NUMBER 3 WINDOW FRAME CUTTING (CONDITION 1 CRACK IN SECOND LOWER CORNER FASTENER HOLE THAT CANNOT BE REMOVED WITH A 0.450 INCH DIAMETER FREEZE PLUG) MOS ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 135 Of 748 Camp Systems EFTA00618426

C O MP Mien winin Mernund up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1345 TABLE 1.2.3 SB 737-53-1345 TABLE 1.2.4 ACCOMPLISH FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 4: NUMBER 3 WINDOW FRAME PERMANENT REPAIR INSTALLATION (CONDITION 1: CRACK IN SECOND LOWER CORNER FASTENER HOLE THAT CANNOT BE REMOVED WITH A 0.450 INCH DIAMETER FREEZE PLUG) MOS REPLACE FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN THE NUMBER 3 WINDOW FRAME (CONDITION 1: CRACK IN SECOND LOWER CORNER FASTENER HOLE THAT CANNOT BE REMOVED WITH A 0.450 INCH DIAMETER FREEZE PLUG) MOS SB 737-53-1345 TABLE 1.3 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 4: NUMBER 3 WINDOW FRAME PERMANENT REPAIR INSTALLATION (CONDITION 2: CRACK IN SECOND LOWER CORNER FASTENER HOLE THAT CAN BE REMOVED WITH A 0.450 INCH DIAMETER FREEZE PLUG) MOS SB 737-53-1345 TABLE 2.1.1 SB 737-53-1345 TABLE 2.1.2 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 5: POST PERMANENT REPAIR INSTALLATION PERMANENT REPAIR TRIPLER HFEC INSPECTION (AIRPLANES WITH THE PERMANENT REPAIR DOUBLER AND TRIPLER INSTALLED) MOS AFL ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 6: POST PERMANENT REPAIR INSTALLATION NUMBER 3 WINDOW FRAME HFEC INSPECTION (AIRPLANES WITH THE PERMANENT REPAIR DOUBLER AND TRIPLER INSTALLED) MOS AFL SB 737-53-1345 TABLE ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR 2.2.1 . SERVICE BULLETIN PART 5: POST PERMANENT REPAIR INSTALLATION PERMANENT REPAIR TRIPLER HFEC INSPECTION (CONDITION 1: NO CRACK INDICATION FOUND) MOS SB 737-53-1345 TABLE 2.2.2 AFL ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 6: POST PERMANENT REPAIR INSTALLATION NUMBER 3 WINDOW FRAME HFEC INSPECTION (CONDITION 1: NO CRACK INDICATION FOUND) MOS AFL 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 136 Of 748 @ Camp Systems EFTA00618427

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53-1345 TABLE 2.3 CONTACT FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (CONDITION 2: ANY CRACK INDICATION FOUND) MOS SB 737-53-1345 TABLE 3.1 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 7: POST PERMANENT REPAIR INSTALLATION REPAIR DOUBLER LFEC INSPECTION (AIRPLANES WITH THE PERMANENT REPAIR DOUBLER AND TRIPLER INSTALLED) MOS AFL SB 737-53-1345 TABLE 3.2 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN PART 7: POST PERMANENT REPAIR INSTALLATION REPAIR DOUBLER LFEC INSPECTION (CONDITION 1: NO CRACK INDICATION FOUND) MOS AFL SB 737-53-1345 TABLE 3.3 ACCOMPLISH FUSELAGE - STRUCTURE MOUND OPENINGS - NUMBER 3 WINDOW FRAME - PERMANENT REPAIR . SERVICE BULLETIN THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (CONDITION 2: ANY CRACK INDICATION FOUND) MOS SB 737-53A1222 R1 POINT D SPLICE FITTING REPLACEMENT (SUPERSEDED BY 737-53A1222 R2). SERVICE BULLETIN SUPERSEDED MOS SB 737-53A1222 R2 FUSELAGE - SECTION 41 CAB - POINT D SPLICE FITTING REPLACEMENT (SUPERSEDED BY 737-53A1222 R3). SERVICE SUPERSEDED BULLETIN MOS SB 737-53A1222 R3 FUSELAGE - SECTION 41 CAB - POINT D SPLICE FITTING REPLACEMENT (SUPERSEDED BY 737-53A1222 R4). SERVICE SUPERSEDED BULLETIN MOS SB 737-53A1222 R4 FUSELAGE - SECTION 41 CAB - POINT D SPLICE FITTING REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 20-OCT-2005 AFL 13500 (s) SB 737-53A1238 FUSELAGE - SECTION 08 - STRUCTURE - INSPECTION (SUPERSEDED BY SS 737-53A1238 R1). SERVICE BULLETIN SUPERSEDED MOS - (s) 74nsufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 137 Of 748 @ Camp Systems EFTA00618428

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1238 RI FUSELAGE - SECTION 48 - STRUCTURE - INSPECTION. SERVICE BULLETIN RECOMMENDED DAYS 30 (s) 10-OCT-2002 SB 737-53A1242 SEALING AROUND VERTICAL FIN LUGS. SERVICE BULLETIN MOS 18 (s) I 7-OCT-2002 AFL 2500 SB 737-53A1242 RI FUSELAGE - STRUCTURE ATTACHMENT FITTINGS - INADEQUATE SEALING AROUND VERTICAL FIN LUGS. SERVICE COMPUED WITH - PREVIOUSLY BULLETIN MOS )8 (s) 13-OCT-2006 28-APR-2005 2686:29 AFL 2500 644 SB 737-53A1242 R2 FUSELAGE - STRUCTURE ATTACHMENT FITTINGS-INADEQUATE SEALING AROUND VERTICAL FIN LUGS. SERVICE COMPUED WITH - IAW THE AD BULLETIN MOS 22-AUG-2008 23-APR-2007 -(s) 3260:48 AFL 782 SB 737-53A1248 NDT INSPECTION OF WEB AT "r CHORD-ABOVE STR 15L AND ISR (STR SL TO 7L AND STR SR TO 9R). SERVICE RECOMMENDED BULLETIN MOS 09-SEP-2004 S8 737-53A1248 E(A)1 INSPECT (NON-DESTRUCTIVE TEST) NDT INSPECTION OF WEB AT 'r CHORD-ABOVE STR ISL AND 15R (STR 5L TO 7L RECOMMENDED AND STR 5R TO 9R). SERVICE BULLETIN (STR SL TO 7L AND STR SR TO 9R) MOS 09-SEP-2004 AFL 25000 (s) SB 737-53A1248 E(A)2 INSPECT (NON-DESTRUCTIVE TEST) NDT INSPECTION OF WEB AT 'r CHORD-ABOVE STR 15L AND 15R (STR 5L TO 7L RECOMMENDED AND STR 5R TO 9R). SERVICE BULLETIN (ABOVE STR 15L AND 15R EXCEPT 5L TO 7L AND 5R TO BR) MOS 09-SEP-2004 AFL 25000 (s) SB 737-53A1248 E(B) INSPECT (NON-DESTRUCTIVE TEST) NDT INSPECTION OF WEB AT -NT CHORD-ABOVE STR 15L AND 15R (STR 5L TO 7L RECOMMENDED AND STR 5R TO 9R). SERVICE BULLETIN 'Y-CHORD BELOW S-15UR MOS 09-SEP-2004 AFL 66000 (s) SB 737-53A1248 RI FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB - INSPECTION FOR WEB CRACKS AT THE Y-CHORD. SERVICE BULLETIN MOS 10-SEP-2007 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 138 Of 748 @ Camp Systems EFTA00618429

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1248 R1 E (A) INSPECTION FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB - INSPECTION FOR WEB 1 CRACKS AT THE Y-CHORD. SERVICE BULLETIN - NDT - OF WEB AT 1Y" CHORD STR 15L AND 15R (STR 5L TO 7L AND STR 5R TO 9R) MOS 10-SEP-2007 AFL 25000 (s) SB 737-53A1248 RI E (A) INSPECTION FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB- INSPECTION FOR WEB 2 CRACKS AT THE Y-CHORD. SERVICE BULLETIN - NDT - OF WEB AT'Y" CHORD (ABOVE STR 15L AND 15R EXCEPT 5L TO 7L AND 5R TO 9R) 10-SEP-2007 SB 737-53A1248 RI E (B) 10-SEP-2007 SB 737-53A1253 SB 737-53A1253 RI 13-MAY-2011 MOS AFL 25000 (s) INSPECTION FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB - INSPECTION FOR WEB CRACKS AT THE Y-CHORD. SERVICE BULLETIN - NDT - OF WEB ATI"' CHORD -BELOW S-15UR MOS AFL 66000 (s) FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING (SUPERSEDED BY SB 737-53A1253 R1). SERVICE BULLETIN MOS 22-AUG-2008 3260:48 AFL 782 FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING. SERVICE BULLETIN MOS (EFF) SUPERSEDED COMPUED WITH - TABLE 1 I.A.W. AD 2007-25-03 / TABLE 2 8 3 ARE N/A TO At SB 737-53A1253 RI GENERAL VISUAL INSPECTION FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR MANDATORY TABLE 1.1 WEB OIL CANNING. SERVICE BULLETIN FOR OIL CAN CONDITIONS OR BULGES FOR ALL AIRPLANES MOS RECURRING SB 737-53A1253 RI TABLE 1.2 SB 737-53A1253 RI TABLE 2.1 AFL 15000 15000 PERFORM FUSELAGE - GENERAL - STATION 1016 Af T PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING. MANDATORY SERVICE BULLETIN OPTION A: STEP 1 OF 2 OR STEP 2 OF 2 OR OPTION B MOS BF/F (s) GENERAL VISUAL INSPECTION FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR MANDATORY WEB OIL CANNING. SERVICE BULLETIN TO IDENTIFY REPAIRS TO THE GORE WEB 8 VERIFY THAT THEY HAVE FOLLOW-ON INSPECTIONS (SRM SECTION 53-80-08-2R) FOR ALL AIRPLANES MOS AFL 15000 15000 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 139 Of 748 @ Camp Systems EFTA00618430

COMP Astant.fran 'Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1253 RI TABLE 2.2 DETERMINE FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING. SERVICE BULLETIN FAA APPROVED FOLLOW-ON INSPECTION PROCEDURES. THRESHOLDS. AND REPEAT INTERVALS AND INCORPORATE INTO MAINTENANCE PROGRAM IF A REPAIR IS FOUND THAT DOES NOT HAVE FOLLOW-ON SUPPLEMENTAL INSPECTIONS MOS 12(s) MANDATORY SB 737-53A1253 RI FM FUSELAGE - GENERAL - STATION 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB OIL CANNING. MANDATORY TABLE 3 SERVICE BULLETIN APPROVED REPAIR INSPECTION PROCEDURES MOS AFL 36000 (s) SB 737-53A1253 TABLE 1 PERFORM A GENERAL VISUAL INSPECTION FOR OIL CAN CONDITIONS OR BULGES AS GIVEN IN ACCOMPLISHMENT INSTRUCTIONS. 3.8.2 OR 3.8.3. SERVICE BULLETIN MOS 22-AUG-2008 I8-MAY-2007 3260:48 AFL 10000 (s) 782 SB 737-53A1253 TABLE 2 GENERAL VISUAL INSPECTION TO IDENTIFY REPAIRS TO THE GORE WEB 8 VERIFY THAT THEY HAVE FOLLOW-ON INSPECTIONS (SRM SECTION 53-80-08-2R). SERVICE BULLETIN MOS 22-AUG-2008 I8-MAY-2007 - (s) 3260:48 AFL 782 SB 737-53A1253 TABLE 3 FM APPROVED REPAIR INSPECTION PROCEDURES. SERVICE BULLETIN MOS 22-AUG-2008 I8-MAY-2007 3260:48 SB 737-53A1289 SB 737-53A1289 R1 I8-NOV-2009 SB 737-53A1289R1 TABLE (1.1) I8-NOV-2009 AFL 24000 (s) 782 INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN MOS AFL INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN MOS SUPERSEDED RECOMMENDED EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE FOR ANY SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.6.1. PART 1 -SKIN LAP JOINT - ZONE 1 INSPECTION (GROUP 1-5) MOS AFL 4000 (s) COMPLIED WITH NOT APPLICABLE NOT APPLICABLE 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 140 Of 748 @ Camp Systems EFTA00618431

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1289 RI TABLE (1.10) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN . HFEC INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10.A. PART 10 - LRTS PROGRAM INSPECTION.IN ZONE 17 (GROUP 1-5) MOS RECOMMENDED AFL 40O00 (s) SS 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (1.11) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.6.10.8. PART 10 -LRTS PROGRAM INSPECTION. IN ZONE 18 (GROUP 1-5) MOS AFL 50000 (s) S8 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (1.12) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.6.10.C. PART 10 -LRTS PROGRAM INSPECTION. IN ZONE 19 (GROUP 1-5) SB 737-53A1289 RI TABLE (1.14) S8 737-53A1289 RI TABLE (1.2) I8-NOV-2009 MOS AFL 50000 (s) CONTACT INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN BOEING FOR ADDITIONAL INSPECTIONS OR REPAIR (GROUP 1-5) MOS RECOMMENDED AFL 75000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.2. PART 2 -SKIN LAP JOINT - ZONE 2 INSPECTION (GROUP 1-5) MOS AFL 40O0 (s) SS 737-53A1289 RI PERFORM INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN INSPECTIONS AS NEEDED IF ANY RECOMMENDED TABLE (1.4) SCRIBE LINE IS FOUND (GROUP 1-5) S8 737-53AI289 RI TABLE (1.7) MOS BF/F (s) HFEC INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN AND UT INSPECTION OF THE SCRIBE LINE RECOMMENDED FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.9. PART 9 - SCRIBE UNE INSPECTION. IN ZONE 1 (GROUP 1-5) MOS AFL 40000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 141 Of 748 @ Camp Systems EFTA00618432

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 737-53A1289 RI TABLE (1.8) SS 737-53A1289 Ft1 TABLE (10.1) HFEC INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN INSPECTION AND UT INSPECTION OF THE RECOMMENDED SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.9. PART 9 - SCRIBE LINE IN ZONE 2 (GROUP 1-5) INSPECTION. MOS AFL 50000 (s) DETERMINE INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN THE THICKNESS OF THE PARENT RECOMMENDED SKIN IN THE AREA OF THE EXTERNAL APPROVED REPAIR BETWEEN STA 360 AND STA 1016 AND BELOW S-10L AND 5-10R WHICH IS 20 INCHES OR LONGER IN THE FORE AND AFT DIRECTION WITH NO CIRCUMFERENTIAL LIMITATIONS MOS AFL 40O0 (s) SS 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (10.11) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10- LRTS PROGRAM EXTERNAL APPROVED REPAIR REPEAT INSPECTION.(G) SCRIBE LINE IS FOUND COMMON TO EXTERNAL APPROVED REPAIR WITH PARENT SKIN THICKNESS 0.040 - 0.044 INCH AND WITHIN THE LIMITS OF A TYPICAL SCRIBE LINE WITH NO CRACK INDICATION MOS AFL 1500 (s) SS 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (10.12) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10- LRTS PROGRAM EXTERNAL APPROVED REPAIR REPEAT INSPECTION.(G) SCRIBE LINE IS FOUND COMMON TO EXTERNAL APPROVED REPAIR WITH PARENT SKIN THICKNESS 0.045 - 0.049 INCH AND WITHIN THE LIMITS OF A TYPICAL SCRIBE LINE WITH NO CRACK INDICATION 61OS AFL 2000 (s) SS 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (10.13) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10- LRTS PROGRAM EXTERNAL APPROVED REPAIR REPEAT INSPECTION.(G) SCRIBE LINE IS FOUND COMMON TO EXTERNAL APPROVED REPAIR WITH PARENT SKIN THICKNESS 0.050 - 0.055 INCH AND WITHIN THE LIMITS OF A TYPICAL SCRIBE LINE WITH NO CRACK INDICATION. S8 737-53A1289 RI TABLE (10.15) MOS AFL 3000(s) CONTACT INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN BOEING FOR ADDITIONAL INSPECTIONS OR REPAIR ALL AIRPLANES WITH SCRIBE LINE USING A LRTS PROGRAM INSPECTION MOS AFL 75000 (s) RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 142 Of 748 @ Camp Systems EFTA00618433

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1289 RI TABLE (10.2) SB 737-53AI289 RI TABLE (10.3) SB 737-53A1289 R1 TABLE (10.4) I8-NOV-2009 SB 737-53AI289 RI TABLE (10.5) I8-NOV-2009 SB 737-53A1289 RI TABLE (11.1) 18-N0V-2809 DETERMINE INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN THE THICKNESS OF THE PARENT RECOMMENDED SKIN IN THE AREA OF THE EXTERNAL APPROVED REPAIR EXISTING EXTERNAL APPROVED REPAIR LOCATED BETWEEN STA 360 AND STA 1016 AND ABOVE S-10L AND S-10R WHICH IS 20 INCHES OR LONGER IN THE FORE AND AFT DIRECTION OR WIDER THAN 12 INCHES CIRCUMFERENTIALLY. (B) MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AROUND THE EDGE OF THE REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.5. PART 5 - EXTERNAL APPROVED REPAIR - INSPECTION PARENT SKIN THICKNESS 0.040 - 0.044 INCH IN THE AREA OF THE EXTERNAL APPROVED REPAIR MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AROUND THE EDGE OF THE REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.5. PART 5 - EXTERNAL APPROVED REPAIR - INSPECTION PARENT SKIN THICKNESS 0.045 - 0.049 INCH IN THE AREA OF THE EXTERNAL APPROVED REPAIR. MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AROUND THE EDGE OF THE REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 32.5. PART 5 - EXTERNAL APPROVED REPAIR - INSPECTION (AXB) PARENT SKIN THICKNESS 0.050 - 0.055 INCH IN THE AREA OF THE EXTERNAL APPROVED REPAIR MOS AFL 4000 (s) DETERMINE INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN THE THICKNESS OF THE PARENT RECOMMENDED SKIN IN THE AREA OF THE INTERNAL APPROVED REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.6. PART 6- INTERNAL APPROVED REPAIR - INSPECTION.EXISTING INTERNAL APPROVED REPAIR LOCATED BETWEEN STA 360 AND STA 1016 AND BELOW 5-10L AND 5-10R AND THE SKIN CUTOUT IS GREATER THAN 20 INCHES LONG IN THE FORE AND AFT DIRECTION WITH NO CIRCUMFERENTIAL LIMITATIONS. MOS AFL 4000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 143 Of 748 @ Camp Systems EFTA00618434

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 737-53A1289 R1 TABLE (11.10) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10- LRTS PROGRAM INTERNAL APPROVED REPAIR REPEAT INSPECTION SCRIBE LINE IS FOUND COMMON TO INTERNAL APPROVED REPAIR WITH PARENT SKIN THICKNESS 0.040 - 0.044 INCH AND WITHIN THE LIMITS OF A TYPICAL SCRIBE LINE WITH NO CRACK INDICATION MOS RECOMMENDED AFL 2600 (s) SB 737-53A1289 RI EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN HFEC RECOMMENDED TABLE (11.11) INSPECTION AND UT INSPECTION OR UT PHASED ARRAY INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10- LRTS PROGRAM INTERNAL APPROVED REPAIR REPEAT INSPECTION SCRIBE LINE IS FOUND COMMON TO INTERNAL APPROVED REPAIR WITH PARENT SKIN THICKNESS 0.045 - 0.049 INCH AND WITHIN THE LIMITS OF A TYPICAL SCRIBE LINE WITH NO CRACK INDICATION SB 737-53A1289 RI TABLE (11.12) SB 737-53A1289 RI TABLE (11.2) I8-NOV-2009 S8 737-53A1289 RI TABLE (11.3) I8-NOV-2009 MOS AFL 2500 (s) CONTACT INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN BOEING FOR ADDITIONAL INSPECTIONS OR REPAIR. ALL AIRPLANES WITH SCRIBE LINE USING A LRTS PROGRAM INSPECTION MOS RECOMMENDED AFL 75000 (s) DETERMINE INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN THE THICKNESS OF THE PARENT RECOMMENDED SKIN IN THE AREA OF THE INTERNAL APPROVED REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.6. PART 6- INTERNAL APPROVED REPAIR - INSPECTION EXISTING INTERNAL APPROVED REPAIR LOCATED BETWEEN STA 360 AND STA 1016 AND ABOVE S-10L AND S-10R AND THE SKIN CUTOUT IS GREATER THAN 20 INCHES LONG IN THE FORE AND AFT DIRECTION OR WIDER THAN 12 INCHES CIRCUMFERENTIALLY MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN ANY SCRIBE RECOMMENDED UNE AROUND THE EDGE OF THE REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.6. PART 6 - INTERNAL APPROVED REPAIR - INSPECTION PARENT SKIN THICKNESS 0.040 - 0.044 INCH INCHES IN THE AREA OF THE INTERNAL APPROVED REPAIR. MOS AFL 4000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 144 Of 748 @ Camp Systems EFTA00618435

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1289 RI TABLE (11.4) I8-NOV-20D9 SB 737-53AI289 RI TABLE (3.1) SB 737-53A1289 RI TABLE (3.11) SB 737-53A1289 RI TABLE (3.2) SB 737-53A1289 RI TABLE (3.4) SB 737-53A1289 RI TABLE (3.8) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AROUND THE EDGE OF THE REPAIR IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.6. PART 6 - INTERNAL APPROVED REPAIR - INSPECTION PARENT SKIN THICKNESS 0.045 - 0.049 INCH IN THE AREA OF THE INTERNAL APPROVED REPAIR MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN OF CIRCUMFERENTIAL BUTT JOINT STA 887 BETWEEN S-10L AND 5-10R FOR ANY SCRIBE LINE IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.3. PART 3-CIRCUMFERENTIAL BUTT JOINT -INSPECTION. (GROUP 1-3.5-8.10) MOS AFL 40000 (s) CONTACT INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN BOEING FOR ADDITIONAL INSPECTIONS OR REPAIR FOR ALL AIRPLANES WITH SCRIBE LINE USING A LRTS PROGRAM INSPECTION. (GROUP 1-3.5-8. 10) MOS AFL 75000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN OF CIRCUMFERENTIAL BUTT JOINT STA 360 BETWEEN S-10L AND S-1 0R FOR ANY SCRIBE LINE IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.3. PART 3 -CIRCUMFERENTIAL BUTT JOINT -INSPECTION. (GROUP 1-3.5-8.10) MOS RECOMMENDED RECOMMENDED RECOMMENDED AFL 45000 (s) ACCOMPLISH INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN INSPECTIONS AS NEED FOR ANY RECOMMENDED SCRIBE LINE FOUND MOS BF/F (s) LFEC INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN - EXTERNAL - SLIDING PROBE INSPECTION RECOMMENDED OR AN INTERNAL MFEC INSPECTION OR AN EXTERNAL HFEC PENCIL PROBE INSPECTION OR AN INTERNAL HFEC INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS (GROUP 1-3.5-8. 10) PARAGRAPH 3.6.10.D. PART 10 - LRTS PROGRAM CIRCUMFERENTIAL BUTT JOINT - REPEAT INSPECTION STATION 360 (GROUP 1-3.5-8.10) MOS AFL 45000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 145 Of 748 @ Camp Systems EFTA00618436

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1289 RI TABLE (3.9) SB 737-53A1289 RI TABLE (6.1) 18-NOV-2009 SB 737-53A1289 RI TABLE (6.12) SB 737-53A1289 RI TABLE (6.13) SB 737-53A1289 RI TABLE (6.14) LFEC INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN - EXTERNAL - SLIDING PROBE INSPECTION RECOMMENDED OR AN INTERNAL MFEC INSPECTION OR AN EXTERNAL HFEC PENCIL PROBE INSPECTION OR AN INTERNAL HFEC INSPECTION OF THE SCRIBE LINE FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10.D. PART 10 - LRTS PROGRAM CIRCUMFERENTIAL BUTT JOINT -REPEAT INSPECTION. STATION 887 (GROUP 1-3.5-8. 10) MOS AFL 40000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 32.4. PART 4 -DECAL - INSPECTION. IN ZONE 6 (GROUP 2.7) MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN AND HFEC RECOMMENDED INSPECTION OF THE SCRIBE LINES FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.6.10. PART 10 - LRTS PROGRAM REPEAT INSPECTION. (A)IN ZONE 6 (GROUP 2. 7) MOS AFL 10000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN AND HFEC RECOMMENDED INSPECTION OF THE SCRIBE LINES FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.8.10. PART 10 - LRTS PROGRAM REPEAT INSPECTION. IN ZONE 7 (GROUP 2.7) MOS AFL WOO (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN AND HFEC RECOMMENDED INSPECTION OF THE SCRIBE LINES FOR ANY CRACK IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.6.10. PART 10 - LRTS PROGRAM REPEAT INSPECTION IN ZONE 8 (GROUP 2.7) MOS AFL 2500 (s) SB 737-53A1289 RI CONTACT INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN BOEING FOR FOR ADDITIONAL RECOMMENDED TABLE (6.16) INSPECTIONS OR REPAIRALL AIRPLANES WITH SCRIBE LINE USING A LRTS PROGRAM INSPECTION (GROUP 2. 7) MOS AFL 75000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 146 Of 748 @ Camp Systems EFTA00618437

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1289 RI TABLE (6.2) I8-NOV-2009 SB 737-53A1289 RI TABLE (6.3) I8-NOV-2009 ACCOMPLISH INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN EXTERNAL GENERAL VISUAL INSPECTIONFOR ANY SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.4. PART 4 - DECAL - INSPECTIONIN ZONE 6 (GROUP 2. 7) MOS RECOMMENDED AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.4. PART 4 - DECAL - INSPECTION. IN ZONE 7 (GROUP 2. 7) MOS AFL 4000 (s) SB 737-53A1289 RI PERFORM INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN AN EXTERNAL GENERAL VISUAL RECOMMENDED TABLE (6.4) INSPECTION FOR ANY SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 32.4. PART 4 - DECAL -INSPECTION. IN ZONE 7 (GROUP 2.7) I8-NOV-2009 SB 737-53A1289 RI TABLE (6.5) I8-NOV-2009 MOS AFL 4000 (s) EXTERNAL - DETAILED INSPECTION INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN FOR ANY RECOMMENDED SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.4. PART 4 -DECAL - INSPECTION. IN ZONE 8 (GROUP 2.7) MOS AFL 4000 (s) SB 737-53A1289 Ft1 ACCOMPLISH INSPECTION OF THE SKIN FOR SCRIBE LINES. SERVICE BULLETIN EXTERNAL GENERAL VISUAL RECOMMENDED TABLE (6.6) INSPECTION FOR ANY SCRIBE LINE AT THE LOCATIONS IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 3.B.4. PART 4 - DECAL -INSPECTION IN ZONE 8 (GROUP 2.7) I8-NOV-2009 SB 737-53A1325 03-DEC-2013 MOS AFL 4000 (s) FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER MANDATORY CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN MOS SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 1.01 LH WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE LEFT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE LEFT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1 (FOR ALL AIRPLANES) (GROUP 1) MOS AFL 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 147 Of 748 @ Camp Systems EFTA00618438

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 1.01 RH DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1 (FOR ALL AIRPLANES) (GROUP 1) MOS AFL SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 1.02 LH WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE LEFT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE LEFT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.J. (IF NO CRACK FOUND ON BOTH THE LEFT AND RIGHT SIDES) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 1.02 RH WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.J. (IF NO CRACK FOUND ON BOTH THE LEFT AND RIGHT SIDES) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.03 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 1 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP IA. (IF ANY CRACK FOUND. ON THE LEFT SIDE. LESS THAN OR EQUAL TO 0.18 INCHES) (GROUP 1) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.04 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 1 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.8. (ANY CRACK FOUND. ON THE RIGHT SIDE. LESS THAN OR EQUAL TO 0.18 INCHES) (GROUP 1) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.05 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 2 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.0 (IF ANY CRACK FOUND. ON THE LEFT SIDE. GREATER THAN 0.18 INCHES AND LESS THAN OR EQUAL TO 1.50 INCHES IN LENGTH. THAT DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 1) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 148 Of 748 @ Camp Systems EFTA00618439

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.06 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 2 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.0. (IF ANY CRACK FOUND. ON THE RIGHT SIDE. GREATER THAN 0.18 INCHES AND LESS THAN OR EQUAL TO 1.50 INCHES IN LENGTH. THAT DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 1) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.07 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 3 IN ACCOR DANCE WITH PARAGRAPH 3.B..WORK INSTRUCTIONS. PART 2. STEP 1.E. (IF ANY CRACK FOUND. ON THE LEFT SIDE. GREATER THAN 0.18 INCHES. THAT EXTENDS INTO THE FLANGE OF THE INNER CHORD) (GROUP 1) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.08 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 3 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP IF. (IF ANY CRACK FOUND. ON THE RIGHT SIDE. GREATER THAN 0.18 INCHES. THAT EXTENDS INTO THE FLANGE OF THE INNER CHORD) (GROUP 1) MOS SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 1.09 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING. (IF ANY CRACK FOUND GREATER THAN 1.50 INCHES IN LENGTH AND DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 1) MOS SB 737-53A1325 TABLE ACCOMPLISH FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB 1.10 AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN PREVENTIVE MODIFICATION ON THE LEFT SIDE IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.H. (IF NO CRACK FOUND ON THE LEFT SIDE AND A REPAIR WAS ACCOMPLISHED ON THE RIGHT SIDE) (GROUP 1) MOS SB 737-53A1325 TABLE ACCOMPLISH FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB 1.11 AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN PREVENTIVE MODIFICATION ON THE RIGHT SIDE IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 1.1. (IF NO CRACK FOUND ON THE RIGHT SIDE AND A REPAIR WAS ACCOMPLISHED ON THE LEFT SIDE) (GROUP 1) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 149 Of 748 @ Camp Systems EFTA00618440

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 2.01 DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2 (ALL AIRPLANES) (GROUP 2) MOS AFL SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 2.02 WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.E. (NO CRACK FOUND ON THE RIGHT SIDE) (GROUP 2) MOS - Is) SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 2.03 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 1 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.A. (ANY CRACK FOUND LESS THAN OR EQUAL TO 0.18 INCHES) (GROUP 2) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 2.04 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 2 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.8. (ANY CRACK FOUND GREATER THAN 0.18 INCHES AND LESS THAN OR EQUAL TO 1.50 INCHES IN LENGTH. THAT DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 2) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 2.05 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 3 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.C. (ANY CRACK FOUND GREATER THAN 0.18 INCHES. THAT EXTENDS INTO THE FLANGE OF THE INNER CHORD) (GROUP 2) MOS SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 2.06 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ANY CRACK FOUND GREATER THAN 1.50 INCHES IN LENGTH AND DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 2) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 150 Of 748 @ Camp Systems EFTA00618441

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 2.07 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR LEFT SIDE INSPECTION AND MODIFICATION INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ALL AIRPLANES) (GROUP 2) MOS AFL SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 3.01 WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2 (ALL AIRPLANES) (GROUP 3) MOS AFL SB 737-53A1325 TABLE DETAILED INSPECTION FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME 3.02 WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN OF THE RIGHT SIDE LOWER FRAME WEB AND INNER CHORD AND AN OPEN HOLE HFEC INSPECTION OF THE RIGHT SIDE LOWER FRAME WEB IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2. (NO CRACK FOUND) (GROUP 3) MOS - (s) SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 3.03 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 1 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.A. (ANY CRACK FOUND LESS THAN OR EQUAL TO 0.18 INCHES) (GROUP 3) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 3.04 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 2 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.8. (ANY CRACK FOUND GREATER THAN 0.18 INCHES AND LESS THAN OR EQUAL TO 1.50 INCHES IN LENGTH. THAT DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 3) MOS SB 737-53A1325 TABLE REPAIR FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 3.05 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN 3 IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 2. STEP 2.C. (ANY CRACK FOUND GREATER THAN 0.18 INCHES. THAT EXTENDS INTO THE FLANGE OF INNER CHORD) (GROUP 3) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 151 Of 748 @ Camp Systems EFTA00618442

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 3.06 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ANY CRACK FOUND GREATER THAN 1.50 INCHES IN LENGTH AND DOES NOT EXTEND INTO THE FLANGE OF THE INNER CHORD) (GROUP 3) MOS SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.01.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 4. STEP 2.A. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.01.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 4. STEP 2.8. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.02.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 4. STEP 5.A. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.02.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 4. STEP 5.8. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.03.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.A. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.03.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.8. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 152 Of 748 @ Camp Systems EFTA00618443

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 4.04.1 HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.A. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.04.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.8. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPUSHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.05 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 4. STEP 3. (AIRPLANES WITH REPAIR 2 ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.06 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 3. (AIRPLANES WITH REPAIR 2 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.07 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 4. STEP 4. (AIRPLANES WITH REPAIR 3 ACCOMPLISHED. ON THE LEFT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 4.08 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 4. (AIRPLANES WITH REPAIR 3 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 1) MOS - (s) SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 4.09 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ANY CRACK FOUND) (GROUP 1) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 153 Of 748 @ Camp Systems EFTA00618444

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 5.01.1 HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.A. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 2) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 5.01.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.8. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 2) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 5.02.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.A. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 2) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 5.02.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.8. (AIRPLANES WITH THE PREVENTNE MODIFICATION ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 2) MOS - Is) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 5.03 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 3. (AIRPLANES WITH REPAIR 2 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 2) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 5.04 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 4. (AIRPLANES WITH REPAIR 3 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 2) MOS - (s) SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 5.05 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ANY CRACK FOUND) (GROUP 2) MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 154 Of 748 @ Camp Systems EFTA00618445

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 6.01.1 HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE LEFT SIDE FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 4. STEP 6.A. (ALL AIRPLANES) (GROUP 3) MOS AFL SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 6.01.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE LEFT SIDE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 4. STEP 6.8. (ALL AIRPLANES) (GROUP 3) MOS AFL SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 802.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.A. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 3) MOS - SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 802.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 2.8. (AIRPLANES WITH THE REPAIR 1 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 3) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 803.1 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF FRAME WEB AND FRAME INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.A. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 3) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 803.2 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 5. STEP 5.8. (AIRPLANES WITH THE PREVENTIVE MODIFICATION ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 3) MOS - (s) SB 737-53A1325 TABLE HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER 6.04 CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 3. (AIRPLANES WITH REPAIR 2 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS S8) (GROUP 3) MOS - Is) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 155 Of 748 @ Camp Systems EFTA00618446

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-53A1325 TABLE 6.05 HFEC FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN INSPECTION OF THE FRAME WEB AND INNER CHORD IN ACCORDANCE WITH PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 5. STEP 4. (AIRPLANES WITH REPAIR 3 ACCOMPLISHED. ON THE RIGHT SIDE. IN ACCORDANCE WITH THIS SB) (GROUP 3) MOS - (s) SB 737-53A1325 TABLE CONTACT FUSELAGE - FRAMES AND BULKHEADS - BODY STATION (STA) 727 BULKHEAD LOWER FRAME WEB AND 6.06 INNER CHORD - INSPECTION. PREVENTIVE MODIFICATION AND REPAIR. SERVICE BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING (ANY CRACK FOUND) (GROUP 3) MOS SB 737-54-1039 STRUT -APPLICATION OF °saki ANT AT BULKHEAD/DIAGONAL BRACE INTERFACE. SERVICE BULLETIN 13-JUN-2002 MOS 18 (5) 800 SB 737-54-1039 RI APPLICATION OF SEALANT AT BULKHEAD/DIAGONAL BRACE INTERFACE, SERVICE BULLETIN COMPLIED WITH MOS 18(s) 11-MAY-2006 IO-OCT-2002 2619:10 AFL 3500 629 SB 737-54-1040 14-NOV-2002 GENERAL VISUAL INSPECTION OF SEALANT ON ENGINE STRUT STRUCTURE. SERVICE BULLETIN MOS 18 (s) AFL 3500 SB 737-54-1040 RI APPLICATION OF SEALANT ON ENGINE STRUT STRUCTURE. SERVICE BULLETIN COMPLIED WITH MOS 18 (s) 18-AUG-2006 14-NOV-2002 2633:50 AFL 3500 633 SB 737-54-1040 R2 APPLICATION OF SEALANT ON ENGINE STRUT STRUCTURE. SERVICE BULLETIN MOS 18 (5) 07-NOV-2006 AFL 3500 SB 737-54-1040 R3 APPLICATION OF SEALANT ON ENGINE STRUT STRUCTURE. SERVICE BULLETIN MOS 18 (5) 14-NOV-2002 AFL 3500 SB 737-54-1041 ENGINE STRUT AFT FAIRING. SERVICE BULLETIN COMPLIED WITH 22,JAN-2004 MOS AR 24-AUG-2007 2968:28 AFL 699 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 156 Of 748 @ Camp Systems EFTA00618447

COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-54-1041 PART 1811 INSPECT ENGINE STRUT AFT FAIRING. SERVICE BULLETIN FOR FLUID ACCUMULATION MOS 30 (s) 22-JAN-2004 24-AUG-2007 2968:28 AFL 4000 699 SB 737-54-1041 PART MODIFY ENGINE STRUT AFT FAIRING. SERVICE BULLETIN SEALS IIIBN 22-JAN-2004 MOS 24-AUG-2007 2968:28 AFL 9000 (s) 699 SB 737-54-1041 RI ENGINE STRUT AFT FAIRING. SERVICE BULLETIN MOS 24-AUG-2007 OI -DEC-2005 2968:28 COMPUED WITH COMPUED WITH RECOMMENDED COMPUED WITH - IAW THE AD AD 2006-07-04 /MARTS 1.11 AND III MOD SB 737-54-1041R1 REF (R2) - IN 02) AFL 699 SB 737-54-1041 RI PART INSPECT ENGINE STRUT AFT FAIRING. SERVICE BULLETIN FOR FLUID ACCUMULATION COMPUED WITH 18.11 MOS 30 (s) 24-AUG-2007 OI -DEC-2005 2968:28 AFL 4000 699 SB 737-54-1041 RI PART MODIFY ENGINE STRUT AFT FAIRING. SERVICE BULLETIN SEALS RECOMMENDED COMPUED WITH IIIBN MOS 24-AUG-2007 12-JAN-2005 - (s) 2968:28 AFL 699 SB 737-54-1041 R2 NACELLES / PYLONS - AFT FAIRING - FLUID ACCUMULATION IN ENGINE STRUT AFT FAIRING -INSTALLATION OF NEW ENGINE STRUT AFT FAIRING SEALS. SERVICE BULLETIN MOS 03-OCT-2007 SB 737-54-1041 R2 PART INSPECT NACELLES / PYLONS - AFT FAIRING - FLUID ACCUMULATION IN ENGINE STRUT AFT FAIRING -INSTALLATION 1811 OF NEW ENGINE STRUT AFT FAIRING SEALS. SERVICE BULLETIN FOR FLUID ACCUMULATION MOS 30 (s) 03-OCT-2007 AFL 4000 SB 737-54-1041 R2 PART MODIFY NACELLES / PYLONS - AFT FAIRING - FLUID ACCUMULATION IN ENGINE STRUT AFT FAIRING -INSTALLATION III & IV OF NEW ENGINE STRUT AFT FAIRING SEALS. SERVICE BULLETIN SEALS 03-OCT-2007 MOS AFL 9000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 157 Of 748 @ Camp Systems EFTA00618448

COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-54-1042 I2-FEB-2004 SB 737-54-1042 RI ENGINE STRUT UPPER LINK - INSPECTION / MODIFICATION. SERVICE BULLETIN 30-JUL-2009 SB 737-54-1043 NACELLES/PYLONS - STRUT DRAINS AND SEALS - AFT FAIRING DRAIN TUBE ASSEMBLY REPLACEMENT.. SERVICE BULLETIN 02-MAY-2007 ENGINE STRUT UPPER LINK-INSPECTION MODIFICATION. SERVICE BULLETIN MOS 30 (s) MOS 30 (s) MOS 60 (s) RECOMMENDED SB 737-54-1043 RI STRUT DRAINS AND SEALS - AFT FAIRING DRAIN TUBE ASSEMBLY SUPERSEDED REPLACEMENT.(SUPPERSEDED BY 737-54-1043 R2). SERVICE BULLETIN MOS - Is) SB 737-54-1043 R2 NACELLES/PYLONS- STRUT DRAINS AND SEALS- AFT FAIRING DRAIN TUBE ASSEMBLY REPLACEMENT SUPERSEDED (SUPERSEDED BY SB 737-54-1043 R3). SERVICE BULLETIN MOS - Is) SB 737-54-1043 R3 NACELLES/PYLONS - STRUT DRAINS AND SEALS - AFT FAIRING DRAIN TUBE ASSEMBLY REPLACEMENT. SERVICE RECOMMENDED BULLETIN MOS 60 (s) 31-DEC-2012 SB 737-54-1045 NACELLES/PYLONS - HEAT INSULATION BLANKETS - REPLACEMENT. SERVICE BULLETIN MOS 29-AUG-2011 25-JUL-2007 - (s) 3533:32 SB 737-54-1046 SB 737-54-1046 RI AFL 863 NACELLES/PYLONS -STRUT TO WING FAIRINGS - THUMBNAIL FAIRING EDGE SEAL REPLACEMENT (SUPERSEDED BY SUPERSEDED SB 737-54-1046 RI), SERVICE BULLETIN MOS - (s) NACELLES/PYLONS - STRUT TO WING FAIRINGS - THUMBNAIL FAIRING EDGE SEAL REPLACEMENT. SERVICE BULLETIN MOS SB 737-54-1047 NACELLES/PYLONS - STRUT AFT FAIRING HEAT SHIELD ASSEMBLY AND INSULATION BLANKET INSTALLATION. RECOMMENDED SERVICE BULLETIN MOS 14-SEP-2012 COMPLIED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 158 Of 748 @ Camp Systems EFTA00618449

C O MP Mien winin Mernund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SS 737-54-1049 13-SEP-2012 NACELLES/PYLONS- STRUT DRAINS AND SEALS - STRUT SEAL PLANE ACCESS PANELS LEAK INSPECTION. SERVICE RECOMMENDED BULLETIN MOS SB 737-54-1049 TABLE 1.1 DETAILED INSPECTION NACELLES/PYLONS- STRUT DRAINS AND SEALS - STRUT SEAL PLANE ACCESS PANELS LEAK RECOMMENDED INSPECTION. SERVICE BULLETIN OF THE STRUT SEAL PLANE ACCESS PANELS FOR ANY LEAK (GROUP 1 AIRPLANES) MOS 30 (s) AFL 9000 SB 737-54-1049 TABLE 1.2 DETAILED INSPECTION NACELLES/PYLONS- STRUT DRAINS AND SEALS - STRUT SEAL PLANE ACCESS PANELS LEAK INSPECTION. SERVICE BULLETIN OF THE STRUT SEAL PLANE ACCESS PANELS FOR ANY LEAK (GROUP 2 AIRPLANES) MOS 36 (s) RECOMMENDED SB 737-55-1062 LEADING EDGE RIB. SERVICE BULLETIN RECOMMENDED MOS 10-AUG-2000 - (s) SB 737-55-1063 TAB MAST FITTING. SERVICE BULLETIN RECOMMENDED COMPLIED WITH - CM MOS 13-SEP-1999 01 -JUL-1999 - SB 737-55-1063 RI TAB MAST FITTING. SERVICE BULLETIN RECOMMENDED MOS 18 (s) 14-SEP-2000 AFL 4000 SB 737-55-1067 ELEVATOR HINGE PLATES. SERVICE BULLETIN NOT APPLICABLE - NO ACTION REQUIRED MOS 22-AUG-2003 1342 AFL 351 SB 737-55-1069 LOWER CLOSURE RIB & RUDDER HINGE PLATE NUT. SERVICE BULLETIN RECOMMENDED MOS 31-AUG-2000 - (s) SB 737-55-1074 INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS. SERVICE BULLETIN RECOMMENDED COMPLIED WITH - PERMANENT REPAIR. PART 3 OF SB. MOS 09-AUG-2010 15-AUG-2000 3448:31 AFL 841 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 159 Of 748 @ Camp Systems EFTA00618450

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1074 PART 1 ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS. SERVICE BULLETIN INSPECTION MOS 18 (s) IS-AUG-2002 09-AUG-20I0 3448:31 AFL 841 SB 737-55-1074 PART 2 ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS. SERVICE BULLETIN INTERIM REPAIR MOS 18 (s) 22-AUG-2008 3260:48 COMPLIED WITH - PERMANENT REPAIR. PART 3 OF SB. COMPLIED WITH AFL 782 SB 737-55-1074 PART 3 ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS. SERVICE BULLETIN PERMANENT REPAIR COMPLIED WITH - PERMANENT REPAIR. PART 3 OF SB. MOS 09-AUG-2010 - (s) 3448:31 AFL 841 SB 737-55-1074 RI INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS BETWEEN THE HORIZONTAL STABILIZERS AND THE RECOMMENDED COMPLIED WITH - PERMANENT REPAIR HORIZONTAL STABILIZER CENTER SECTION. SERVICE BULLETIN MOS 29-AUG-2011 18-DEC-2003 3533:32 AFL 863 SB 737-55-1074 RI PART ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS BETWEEN THE HORIZONTAL STABILIZERS COMPLIED WITH 1 AND THE HORIZONTAL STABILIZER CENTER SECTION. SERVICE BULLETIN INSPECTION MOS 18 (5) 29-AUG-20I I 18-DEC-2003 3533:32 AFL 863 SB 737-55-1074 RI PART ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS BETWEEN THE HORIZONTAL STABILIZERS RECOMMENDED 2 AND THE HORIZONTAL STABILIZER CENTER SECTION, SERVICE BULLETIN INTERIM REPAIR MOS 18 (5) 12-DEC-2003 SB 737-55-1074 RI PART ACCOMPLISH INSPECTION AND REPAIR OF THE INTERFACE BUSHINGS BETWEEN THE HORIZONTAL STABILIZERS RECOMMENDED COMPLIED WITH 3 AND THE HORIZONTAL STABILIZER CENTER SECTION. SERVICE BULLETIN PERMANENT REPAIR MOS 29-AUG-2011 09-SEP-2004 - (s) 3533:32 AFL 863 SB 737-55-1086 INSPECTION OF THE PINS AND BOLTS THAT ATTACH THE HORIZONTAL STABILIZER TO THE HORIZONTAL STABLIZER - IAW THE SB CENTER SECTION (SUPERSEDED BY SB 737-55-1086 RI). SERVICE BULLETIN MOS 22-AUG-2008 II -DEC-2003 3260:48 AFL 782 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 160 Of 748 @ Camp Systems EFTA00618451

CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB SB 737-55-1086 RI 16-DEC-2004 737-55-1086 R2 INSPECTION OF THE PINS AND BOLTS THAT ATTACH THE HORIZONTAL STABILIZER TO THE HORIZONTAL STABLIZER CENTER SECTION (SUPERSEDED BY SB 737-55-1086 R2). SERVICE BULLETIN MOS STABILIZERS - HORIZONTAL STABILIER - INSPECTION OF THE PINS AND BOLTS THAT ATTACH THE HORIZONTAL STABILIZER TO THE HORIZONTAL STABILIZER CENTER SECTION (SUPERSEDED BY SB 737-55-1086 R3). SERVICE BULLETIN - INFORMATION REF TO IR AND REV.2 (REPLACEMENT) SUPERSEDED COMPLIED WITH MOS 29-AUG-20m 3533:32 AFL 863 SB 737-55-1086 R3 STABILIZERS - HORIZONTAL STABILIZER - INSPECTION OF THE PINS AND BOLTS THAT ATTACH THE HORIZONTAL RECOMMENDED STABILIZER TO THE HORIZONTAL STABILIZER CENTER SECTION. SERVICE BULLETIN DAYS 90 (5) 13-JUN-2012 SB 737-55-1089 HORIZONTAL STABILIZER - TRAILING EDGE PANEL. CONDUCTIVE STRIP AND TIP CAP ASSEMBLY - CHANGE SUPERSEDED (SUPERSEDED BY SB 737-55-1089 R1). SERVICE BULLETIN MOS SB 737-55-1089 RI STABILIZERS - HORIZONTAL STABILIZER - TRAILING EDGE PANEL. CONDUCTIVE STRIP AND TIP CAP ASSEMBLY - RECOMMENDED CHANGE. SERVICE BULLETIN MOS 09-SEP-201 SB 737-55-1090 STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR TERMINATION FITTING- INSPECTION. SERVICE BULLETIN MANDATORY MOS 30-MAR-201 I SB 737-55-1090 TABLE 1 INSPECTION STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR TERMINATION FITTING - INSPECTION. SERVICE MANDATORY BULLETIN OF THE LEFT AND RIGHT SIDE HORIZONTAL STABILIZER IDENTIFICATION PLATE FOR A SERIAL NUMBER THAT START WITH SAX FOR ALL AIRPLANES MOS 12 (5) 30-MAR-201 I SB 737-55-1090 TABLE 1.2 DETAILED INSPECTION STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR TERMINATION FITTING - INSPECTION. MANDATORY SERVICE BULLETIN OF THE HORIZONTAL STABILIZER TERMINATION FITTING FASTENERS FOR INCORRECT BOLT PROTRUSION AND CHAMFER FOR HORIZONTAL STABILIZERS IDENTIFICATION PLATES WHICH HAVE A SERIAL NUMBER STARTING WITH SAIC. MOS 12 (5) 30-MAR-201 I SB 737-55-1090 TABLE 1.6 HFEC STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR TERMINATION FITTING - INSPECTION. SERVICE BULLETIN AND UT INSPECTIONS OF THE TERMINATION FITTING FOR CRACKS FOR NEW BACB30US14K( ) BOLT IS INSTALLED MOS 12 (5) 3C-MAR-201I MANDATORY ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time Camp Systems 161 Of 748 EFTA00618452

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1093 09-APR-2012 SB 737-55-1096 22-MAR-2013 STABILIZERS - HORIZONTAL STABILIZER - REPLACEMENT OF REAR SPAR ATTACH PINS WITH UNAPPROVED SURFACE COATING. SERVICE BULLETIN MOS AFL 3000(s) STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN MOS SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN DO A 1(01.1) DETAILED INSPECTION OF THE SKIN. MODIFICATION SKIN AND SPAR DOUBLERS FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN AN 1(01.2) EDDY CURRENT INSPECTION OF THE SKIN. MODIFICATION SKIN. SPLICE DOUBLERS AND SPAR LOWER CHORDS FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL 58 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(01.3) LOW FREQUENCY EDDY CURRENT (LFEC) INSPECTION OF THE FRONT SPAR UPPER CHORD AFT FLANGE. FROM STAB STA 66.50 TO STAB TIP. FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(01.4) HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE FRONT SPAR UPPER CHORD FORWARD FLANGE. FROM STAB STA 66.50 TO STAB TIP. FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(01.5) LFEC INSPECTION OF THE FRONT SPAR UPPER CHORD WEB FLANGE. FROM STAB STA 66.50 TO STAB STA 175.5 AND FROM STAB STA 258.28 TO STAB TIP. FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 162 Of 748 @ Camp Systems EFTA00618453

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1096 TABLE 1(01.6) DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A HFEC INSPECTION OF THE FRONT SPAR UPPER CHORD WEB FLANGE. FROM STAB STA 66.50 TO STAB STA 175.5 AND FROM STAB STA 258.28 TO STAB TIP. FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(01.7) HFEC INSPECTION OF THE FRONT SPAR UPPER CHORD FORWARD FLANGE. FROM STAB STA 175.5 TO STAB STA 258.28. FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL RIGHT CYCLES MOS AFL SB 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE 1(02.1) BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IN ANY CRACK FOUND IN THE SKIN. MODIFICATION SKIN. SPAR DOUBLERS. SPLICE DOUBLERS OR SPAR LOWER CHORDS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS SB 737-55-1096 TABLE REMOVE STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN 1(03.1) THE CRACK DAMAGE IF ANY CRACK FOUND IN THE FRONT SPAR UPPER CHORD FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS 58 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(00.1) DETAILED INSPECTION OF THE SKIN. MODIFICATION SKIN AND SPAR DOUBLERS FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN AN 1(00.2) EDDY CURRENT INSPECTION OF THE SKIN. MODIFICATION SKIN. SPLICE DOUBLERS AND SPAR LOWER CHORDS FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 163 Of 748 @ Camp Systems EFTA00618454

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1096 TABLE 1(04.3) DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A LFEC INSPECTION OF THE FRONT SPAR UPPER CHORD AFT FLANGE. FROM STAB STA 66.50 TO STAB TIP. FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(04.4) HFEC INSPECTION OF THE FRONT SPAR UPPER CHORD FORWARD FLANGE. FROM STAB STA 66.50 TO STAB TIP. FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(04.5) LFEC INSPECTION OF THE FRONT SPAR UPPER CHORD WEB FLANGE. FROM STAB STA 66.50 TO STAB STA 175.5 AND FROM STAB STA 258.28 TO STAB TIP. FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL 58 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(04.6) HFEC INSPECTION OF THE FRONT SPAR UPPER CHORD WEB FLANGE. FROM STAB STA 66.50 TO STAB STA 175.5 AND FROM STAB STA 258.28 TO STAB TIP. FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL 58 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(04.7) HFEC INSPECTION OF THE FRONT SPAR UPPER CHORD FORWARD FLANGE. FROM STAB STA 175.5 TO STAB STA 258.28. FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE 1(05.1) BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF ANY CRACK FOUND IN THE SKIN. MODIFICATION SKIN. SPAR DOUBLERS. SPLICE DOUBLERS OR SPAR LOWER CHORDS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 164 Of 748 @ Camp Systems EFTA00618455

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1096 TABLE REMOVE STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN THE CRACK DAMAGE IF ANY CRACK FOUND IN THE FRONT SPAR UPPER CHORD FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED BEFORE 56.000 TOTAL FLIGHT CYCLES 1(06.1) MOS SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(07.1) DETAILED INSPECTION OF THE SKIN. MODIFICATION SKIN AND SPAR DOUBLERS FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS AFL 58 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN AN 1(07.2) EDDY CURRENT INSPECTION OF THE SKIN. MODIFICATION SKIN. SPLICE DOUBLERS AND SPAR LOWER CHORDS FOR CRACKS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE RECOMMENDED 1(07.3) BULLETIN BOEING FOR ADDITIONAL POST MODIFICATION INSPECTIONS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS SB 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE 1(08.1) BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF ANY CRACK FOUND IN THE SKIN. MODIFICATION SKIN. SPAR DOUBLERS. SPLICE DOUBLERS OR SPAR LOWER CHORDS FOR LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS 58 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN A 1(09.1) DETAILED INSPECTION OF THE SKIN. MODIFICATION SKIN AND SPAR DOUBLERS FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS AFL 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 165 Of 748 @ Camp Systems EFTA00618456

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55-1096 TABLE DO STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE BULLETIN AN 1(09.2) EDDY CURRENT INSPECTION OF THE SKIN. MODIFICATION SKIN. SPLICE DOUBLERS AND SPAR LOWER CHORDS FOR CRACKS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS AFL SB 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE RECOMMENDED 1(09.3) BULLETIN BOEING FOR ADDITIONAL POST MODIFICATION INSPECTIONS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES MOS 58 737-55-1096 TABLE CONTACT STABILIZERS - HORIZONTAL STABILIZER - LOWER SKIN CRACKING AND MODIFICATION. SERVICE 1(10.1) BULLETIN BOEING FOR REPAIR INSTRUCTIONS AND DO THE WORK INSTRUCTED BY BOEING IF ANY CRACK FOUND IN THE SKIN. MODIFICATION SKIN. SPAR DOUBLERS. SPLICE DOUBLERS OR SPAR LOWER CHORDS FOR RIGHT SIDE HORIZONTAL STABILIZER LOWER SKIN MODIFICATION INSTALLED AT OR AFTER 56.000 TOTAL FLIGHT CYCLES SB 737-55A1064 I5-OCT-1998 MOS ELEVATOR BALANCE PANEL ASSEMBLIES. SERVICE BULLETIN MOS 250(s) 44 RECOMMENDED SB 737-55A1064 R1 ELEVATOR BALANCE PANEL ASSEMBLIES. SERVICE BULLETIN RECOMMENDED NOT APPLICABLE - BY SERIAL NUMBER MOS 20-APR-2001 07-DEC-2000 - (s) 697:54 AFL 188 SB 737-55A1066 FRONT SPAR HINGE FITTING REPLACEMENT-HINGE 3-8. SERVICE BULLETIN NOT APPLICABLE - NO ACTION REQUIRED MOS 24 (s) 22-AUG-2003 19-SEP-2002 1342 AFL 18000 351 SB 737-55A1066 RI FRONT SPAR HINGE FITTING REPLACEMENT-HINGES 3-8. SERVICE BULLETIN - 737-55A1080R1 MOS 24 (s) 19-SEP-2002 AFL 18000 SB 737-55A1068 ELEVATOR TAB ASSEMBLY. SERVICE BULLETIN RECOMMENDED COMPLIED WITH -OW MOS I3-SEP-1999 09-JUN-1999 - Is) SB 737-55A1068 R1 ELEVATOR TAB ASSEMBLY. SERVICE BULLETIN RECOMMENDED MOS 11-JUN-1999 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 166 Of 748 @ Camp Systems EFTA00618457

COMP Astant.frn• thernand up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55A1068 R2 ELEVATOR TAB ASSEMBLY. SERVICE BULLETIN DAYS 15 (s) 24-FEB-2000 AFL 100 SB 737-55A1072 PKG 1 STABILIZERS - ELEVATOR - TAB ASSEMBLY - INSPECTION OF ELEVATOR TAB HINGE AND ELEVATOR TAB CONTROL MECHANISM. SERVICE BULLETIN MOS 28-DEC-2000 - Is) RECOMMENDED SB 737-55A1072 PKG 2 STABILIZERS - ELEVATOR - TAB ASSEMBLY- INSPECTION OF ELEVATOR TAB HINGE AND ELEVATOR TAB CONTROL RECOMMENDED MECHANISM. SERVICE BULLETIN MOS 28-DEC-2000 AFL 750(s) SB 737-55A1072 PKG 3 STABILIZERS - ELEVATOR - TAB ASSEMBLY- INSPECTION OF ELEVATOR TAB HINGE AND ELEVATOR TAB CONTROL RECOMMENDED MECHANISM. SERVICE BULLETIN MOS 28-DEC-2000 1500 (s) AFL 750 SB 737-55A1072 RI ELEVATOR HINGE AND TAB ASSEMBLY. SERVICE BULLETIN RECOMMENDED MOS 11 -JAN-2001 - (s) SB 737-55A1072 RI PKG 1 INSPECT ELEVATOR HINGE AND TAB ASSEMBLY. SERVICE BULLETIN MOS 20-APR-2001 11 -JAN-2001 702:24 AFL 250(s) 188 SB 737-55A1072 RI PKG 2 INSPECT ELEVATOR HINGE AND TAB ASSEMBLY. SERVICE BULLETIN MOS IWAN-2001 AFL 750(s) SB 737-55A1072 RI PKG 3 INSPECT ELEVATOR HINGE AND TAB ASSEMBLY. SERVICE BULLETIN MOS I I -JAN-2001 1500 (s) SB 737-55A1076 AFL 750 ELEVATOR TAB HINGE FASTNER REPLACEMENT. SERVICE BULLETIN MOS 24 (s) AFL 4500 RECOMMENDED RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 167 Of 748 @ Camp Systems EFTA00618458

MP Aseant.ftne tAernand up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BB.1): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-55A1079 19-JUL-2001 ELEVATOR TAB. SPEEDBRAKE RESTRICTION. PLACARD INSTALLATION. SERVICE BULLETIN MOS 1 (s) SB 737-55A1079 RI ELEVATOR TAB. SPEEDBREAK RESTRICTION, PLACARD INSTALLATION. SERVICE BULLETIN RECOMMENDED MOS I (s) 16-MAY-2002 SB 737-55A1080 ELEVATOR AND ELEVATOR TAB REPLACEMENT. SERVICE BULLETIN COMPUED WITH - PREVIOUSLY REF. AD 2003-03-22 / 737-55A1080R1 MOS 24 (s) 18-AUG-2006 19-SEP-2002 2633:50 AFL 18000 633 SB 737-55A1080 RI ELEVATOR AND ELEVATOR TAB REPLACEMENT, SERVICE BULLETIN COMPUED WITH MOS 22-AUG-2003 19-SEP-2002 1342 AFL 351 SB 737-55A1082 ELEVATOR MODIFICATION. SERVICE BULLETIN COMPLIED WITH - PREVIOUSLY MOS 24 (s) 22-AUG-2003 19-SEP-2002 1342 AFL 18000 351 SB 737-55A1082 RI MODIFICATION TO IMPROVE THE STRUCTURAL DAMPING CHARACTERISTICS AND ENHANCE THE WEAR - 737-55A1080RI CHARACTERISTICS OF THE ELEVATOR TAB. SERVICE BULLETIN MOS 24 (s) 19-SEP-2002 AFL 18000 SB 737-55A1084 HORIZONTAL STABILIZER - TRAILING EDGE - ELEVATOR BALANCE BAY PANEL SEAL TRIM. SERVICE BULLETIN RECOMMENDED MOS 07-MAR-2002 - (s) SB 737-55A1084 RI HORIZONTAL STABILIZER - ELEVATOR BALANCE BAY PANEL SEAL TRIM. SERVICE BULLETIN RECOMMENDED MOS 20-JUN-2002 - (s) SB 737-56-1011 DRAIN OPENABLE WINDOWS INSTALLATIONS. SERVICE BULLETIN RECOMMENDED MOS 19-NOV-1998 - (s) SB 737-56-1011 RI DRAIN OPENABLE WINDOWS INSTALLATIONS. SERVICE BULLETIN RECOMMENDED MOS 29-JUN-2000 - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks *-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 168 Of 748 @Camp Systems EFTA00618459

COMP Jm. tMrrnM•O AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-56-1014 INSPECTION AND REPLACEMENT OF NO. 3 FLIGHT COMPARTMENT WINDOWS. SERVICE BULLETIN MOS 26-APR-2001 SB 737-56-1016 -AUG-2005 SB 737-56-1017 I7-MAY-2006 SB 737-56-1017 RI AFL 2000 (s) WINDOWS - CONTROL CABIN SLIDING WINDOWS - NUMBER 2 OPENABLE WINDOW - HOLD OPEN LATCH ASSEMBLY - INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS WINDOWS - FLIGHT COMPARTMENT - CONTROL CABIN FIXED WINDOWS - DELEATION OF NUMBER 4 AND NUMBER 5 WINDOWS (SUPERSEDED BY 737-56-1017 R1). SERVICE BULLETIN MOS WINDOWS - FLIGHT COMPARTMENT - CONTROL CABIN FIXED WINDOWS - DELETION OF NUMBER 4 AND NUMBER 5 SUPERSEDED WINDOWS. (SUPERSEDED BY SB 737-56-1017 R2). SERVICE BULLETIN MOS SB 737-56-1017 R2 WINDOWS - FLIGHT COMPARTMENT - CONTROL CABIN FIXED WINDOWS - DELETION OF NUMBER 4 AND NUMBER 5 RECOMMENDED WINDOWS.. SERVICE BULLETIN MOS 28-JAN-2011 SB 737-56-1024 WINDOWS - CONTROL CABIN SLIDING WINDOWS - LEFT SIDE AND RIGHT SIDE NUMBER 2 WINDOW FRAME REPAIR AND MODIFICATION. SERVICE BULLETIN MOS 21 -SEP-2007 SB 737-56-1025 20-JAN-2010 SB 737-56-1025 (LH) SB 737-56-1025 (RH) FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2 WINDOW PANE - REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS REPLACE FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2 WINDOW PANE- REPLACEMENT. SERVICE BULLETIN RECOMMENDED LEFT FLIGHT DECK NUMBER 2 (SLIDING) WINDOW MOS REPLACE FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2 WINDOW PANE - REPLACEMENT. SERVICE BULLETIN RECOMMENDED RIGHT FLIGHT DECK NUMBER 2 (SLIDING) WINDOW MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 169 Of 748 @ Camp Systems EFTA00618460

C O MP &Wiwi's. Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-56A1022 WINDOWS - FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - INSPECTION SUPERSEDED COMPUED WITH - INSPECTIONS TABLES 2 & 3 (SUPERSEDED BY 737-56A1022 RI). SERVICE BULLETIN FOR THE 114 AND #5 WINDOWS ONLY LA.W. AD 2008-11-08 FOUND SATSFACTORY MOS 16-FEB-20I0 18-JUL-2007 3417:51 AFL 829 SB 737-56A1022 RI WINDOWS - FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - INSPECTION. RECOMMENDED COMPUED WITH - DETAIL INSPECTION I.A.W. AD SERVICE BULLETIN 2008-11-08 (F) FLIGHT DECK NO2. NO.4 AND NO.5 WINDOWS MOS 12-FEB-2014 12-MAR-2010 3743:34 AFL 917 SB 737-56A1022 RI DETAILED INSPECTION WINDOWS - RIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 RECOMMENDED COMPUED WITH - DETAIL INSPECTION TABLE 1.01 12-MAR-2010 SB 737-56A1022 RI TABLE 1.02 12-MAR-2010 SB 737-56A1022 RI TABLE 2.01 12-MAR-2010 SB 737-56A1022 RI TABLE 2.02 12-MAR-2010 SB 737-56A1022 RI TABLE 3.01 12-MAR-2010 SB 737-56A1022 RI TABLE 3.02 WINDOWS - INSPECTION. SERVICE BULLETIN OF THE LEFT AND RIGHT FLIGHT DECK NUMBER 2 WINDOW (GROUP 1-2) MOS 36 (s) 12-FEB-2014 7500 3743:34 AFL 917 REPLACE WINDOWS - FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - RECOMMENDED INSPECTION. SERVICE BULLETIN THE LEFT AND RIGHT FLIGHT DECK NUMBER 2 WINDOW AND PERFORM A DETAILED INSPECTION (GROUP 1-2) MOS DETAILED INSPECTION WINDOWS - RIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 RECOMMENDED COMPUED WITH - DETAIL INSPECTION WINDOWS - INSPECTION. SERVICE BULLETIN OF FLIGHT DECK NUMBER 4 WINDOW (GROUP 1. CONFIGURATION 1) MOS 24 (s) I2-FEB-2014 6000 3743:34 AFL 917 REPLACE WINDOWS - FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - RECOMMENDED INSPECTION. SERVICE BULLETIN THE FLIGHT DECK NUMBER 4 WINDOW AND PERFORM DETAILED INSPECTION (GROUP 1. CONFIGURATION 1) MOS BFIF (s) DETAILED INSPECTION WINDOWS - RIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 RECOMMENDED COMPUED WITH - DETAIL INSPECTION WINDOWS - INSPECTION. SERVICE BULLETIN OF THE FLIGHT DECK NUMBER 5 WINDOW (GROUP 1. CONFIGURATION 1) MOS 24 (s) 6000 I2-FEB-2014 3743:34 AFL 917 REPLACE WINDOWS - FLIGHT COMPARTMENT - FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - RECOMMENDED INSPECTION. SERVICE BULLETIN THE FLIGHT DECK NUMBER 5 WINDOW (GROUP 1. CONFIGURATION 1) MOS I2-MAR-2010 BFIF (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 170 Of 748 @ Camp Systems EFTA00618461

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-56A1022 TABLE 1 18-JUL-2007 SB 737-56A1022 TABLE 2 18-JUL-2007 SB 737-56A1022 TABLE 3 18-JUL-2007 SB 737-57-1250 07-FEB-2002 DETAIL INSPECTION WINDOWS - FLIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - INSPECTION (SUPERSEDED BY 737-56A1022 RI). SERVICE BULLETIN OF FLIGHT DECK NUMBER 2 WINDOW FOR GROUP 1 AND 2 MOS 36 (5) 7500 14-FEB-2008 3151:22 AFL 746 DETAIL INSPECTION WINDOWS- FLIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - INSPECTION (SUPERSEDED BY 737-56A1022 R1). SERVICE BULLETIN OF FLIGHT DECK NUMBER 4 WINDOW FOR GROUP 1 CONFIGURATION 1 MOS 24 (s) I6-FEB-2010 6000 3417:51 AFL 829 DETAIL INSPECTION WINDOWS - FLIGHT COMPARTMENT- FLIGHT DECK NUMBER 2. NUMBER 4 AND NUMBER 5 WINDOWS - INSPECTION (SUPERSEDED BY 737-56A1022 RI). SERVICE BULLETIN OF FLIGHT DECK NUMBER 5 WINDOW FOR GROUP 1 CONFIGURATION 1 MOS 24 (5) I6-FEB-2010 6000 3417:51 AFL 829 INSPECTION OF SECONDARY FUEL VAPOR-BARRIER APPLICATION ON THE WING CENTER SECTION. SERVICE BULLETIN MOS 48 (5) - INSPECTION SB 737-57-1250 RI INSPECTION OF THE SECONDARY FUEL VAPOR-BARRIER APPLICATION ON THE WING CENTER SECTION TOP PANEL COMPUED WITH AND FRONT SPAR. SERVICE BULLETIN MOS 48 (5) 28-SEP-2009 04-SEP-2003 3378:04 AFL 812 SB 737-57-1250 R2 INSPECTION OF THE SECONDARY FUEL VAPOR-BARRIER APPLICATION ON THE WING CENTER SECTION TOP PANEL COMPUED WITH AND FRONT SPAR. SERVICE BULLETIN MOS 28-SEP-2009 28-NOV-2006 - (s) 3378:04 AFL 812 SB 737-57-1253 CENTER WING REAR SPAR - STIFFENER MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 16-DEC-1999 AFL 4500 (s) SB 737-57-1253 RI CENTER WING REAR SPAR - STIFFENER MODIFICATION. SERVICE BULLETIN MOS II -JAN-2001 AFL 4500 (s) RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 171 Of 748 @ Camp Systems EFTA00618462

COMP Astant.frn• thernand up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57-1255 WING - LEFT SIDE MIDSPAR LOWER PANEL REPLACEMENT. SERVICE BULLETIN MOS 21 -JUN-2001 - Is) SB 737-57-1255 RI LEFT SIDE MIDSPAR LOWER PANEL REPLACEMENT. SERVICE BULLETIN MOS II -MAR-2004 SB 737-57-1264 FLAP CARRIAGE BUSHING REPLACEMENT. SERVICE BULLETIN MOS 24-MAY-2001 SB 737-57-1268 WINGS-LOWER WING SKIN PANELS-INSTALLATION OF THE RUB STRIPS. SERVICE BULLETIN - (s) MOS 06-JUN-2002 - (s) SB 737-57-1268 RI WING LOWER SKIN PANELS INSTALLATION OF THE RUB STRIPS. SERVICE BULLETIN MOS I7-OCT-2002 - SB 737-57-1272 OUTBOARD KRUEGER FLAP INSPECTION. REPAIR. AND PREVENTIVE MODIFICATION. SERVICE BULLETIN MOS 24-JUN-2004 - (s) SB 737-57-1272 PART 1 INSPECT OUTBOARD KRUEGER FLAP INSPECTION. REPAIR. AND PREVENTIVE MODIFICATION. SERVICE BULLETIN MOS 24-JUN-2004 3000 (s) SB 737-57-1272 PART 2 MODIFICATION OUTBOARD KRUEGER FLAP INSPECTION. REPAIR. AND PREVENTIVE MODIFICATION. SERVICE BULLETIN !REPLACEMENT MOS 24-JUN-2004 RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED SB 737-57-1275 LOWER WING SKIN PANEL - NACELLE SUPPORT FITTINGS ATTACHMENT FASTENERS INSPECTION AND RECOMMENDED REPLACEMENT. SERVICE BULLETIN MOS 04-SEP-2003 30000 Is) AFL 30000 SB 737-57-1275 RI LOWER WING SKIN PANEL - NACELLE SUPPORT FITTINGS ATTACHMENT FASTENERS INSPECTION AND REPLACEMENT. SERVICE BULLETIN MOS I8-AUG-2005 30000 Is) AFL 30000 - REF: REV.3 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 172 Of 748 @ Camp Systems EFTA00618463

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57-1275 R2 LOWER WING SKIN PANEL - NACELLE SUPPORT FITTINGS ATTACHMENT FASTENERS INSPECTION AND - REF: REV.3 REPLACEMENT. SERVICE BULLETIN MOS 12-JUL-2006 - (s) SB 737-57-1275 R3 LOWER WING SKIN PANEL - NACELLE SUPPORT FITTINGS ATTACHMENT FASTENERS INSPECTION AND COMPLIED WITH - IAW THE AD 2005-24-03R1 REPLACEMENT. SERVICE BULLETIN MOS 24-AUG-2007 I7-OCT-2006 - (5) 2968:28 AFL 699 SB 737-57-1278 OUTBOARD FLAP BELLCRANK ASSEMBLY INSPECTION AND MODIFICATION. SERVICE BULLETIN RECOMMENDED 02-DEC-2004 MOS SB 737-57-1278 RI WINGS - TRAILING EDGE AND TRAIUNG EDGE DEVICES - OUTBOARD FLAP BELLCRANK ASSEMBLY INSPECTION AND MODIFICATION.. SERVICE BULLETIN MOS 27 -SEP-2006 58 737-57-1278 R2 WINGS - TRAILING EDGE AND TRAIUNG EDGE DEVICES - OUTBOARD FLAP BELLCRANK ASSEMBLY INSPECTION AND MODIFICATION.. SERVICE BULLETIN MOS 04-JUN-2007 SB 737-57-1281 REPAIR OF INBOARD MAIN FLAP UPPER SKIN AND MODIFICATION OF NUTPLATE STRIP ASSEMBLY. SERVICE RECOMMENDED BULLETIN MOS I 5-JUL-2004 SB 737-57-1284 WINGS - TRAILING EDGE AND TRAIUNG EDGE DEVICES - INSPECTION. REPAIR 7 MODIFICATION - WING BUTTOCK LINE 147 TO WING BUTTOCK LINE 201. SERVICE BULLETIN MOS 09-APR-2007 SB 737-57-1285 WINGS - WING STRINGERS - INSTALL STRINGERS 7 AND 9 REINFORCEMENT. SERVICE BULLETIN MOS SB 737-57-1285 RI WINGS - WING STRINGERS - INSTALL STRINGERS 7 AND 9 REINFORCEMENT. SERVICE BULLETIN MOS SB 737-57-1286 WINGS - CENTER - REAR SPAR VAPOR BARRIER - INSPECTION. REPAIR AND MODIFICATION.. SERVICE BULLETIN MOS 03-APR-2006 - INFORMATION REFER TO REV.1 AFL 5500 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 173 Of 748 @ Camp Systems EFTA00618464

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57-1286 RI 26-JUL-2007 SB 737-57-1288 30-MAR-2007 SB 737-57-1288 RI 03-JUN-2008 SB 737-57-1293 13-NOV-2008 MOS 24 (5) SB 737-57-1293 RI LEADING EDGE AND LEADING EDGE DEVICES - FUEL DRAIN PATH MODIFICATION (SUPERSEDED BY SB 737-57-1293 SUPERSEDED R2). SERVICE BULLETIN MOS SB 737-57-1293 R2 WINGS - LEADING EDGE AND LEADING EDGE DEVICES - FUEL DRAIN PATH MODIFICATION (SUPERSEDED BY SB SUPERSEDED 737-57-1293 R3). SERVICE BULLETIN MOS - Is) SB 737-57-1293 R3 WINGS - LEADING EDGE AND LEADING EDGE DEVICES - FUEL DRAIN PATH MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 24 (s) 28-SEP-2011 SB 737-57-1295 WINGS - TRAILING EDGE AND TRAIUNG EDGE DEVICES - WING INBOARD FIXED TRAILING EDGE UPPER PANEL BULB SEAL CHAFING ON WING-TO-BODY FAIRING PANEL - INSPECTION. REPAIR AND MODIFICATION.. SERVICE BULLETIN WINGS - CENTER WING - REAR SPAR VAPOR BARRIER - INSPECTION. REPAIR AND MODIFICATION. SERVICE BULLETIN MOS 28-SEP-2009 3378:04 AFL 5500 812 6312 TRAILING EDGE FLAP - NUMBER 3 AND NUMBER 6 TAILCONE ASSEMBLIES - INSPECTION AND REPAIR. SERVICE BULLETIN MOS AFL 5600 (s) WINGS - TRAILING EDGE FLAP - NUMBER 3 AND NUMBER 6 TAILCONE ASSEMBLES - INSPECTION AND REPAIR. SERVICE BULLETIN MOS AFL 5000(s) LEADING EDGE AND LEADING EDGE DEVICES - FUEL DRAIN PATH MODIFICATION. SERVICE BULLETIN RECURRING COMPUED WITH - PARTIALLY GENERAL MOS 12 (s) 04-JUN-2007 4500 SB 737-57-1300 04-JUN-2007 WINGS - TRAILING EDGE FLAPS - INBOARD FLAPS- INBOARD MAIN FLAP TRACKS. K4 AND #5- INSPECTION AND RECOMMENDED EXCHANGE PROGRAM. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 174 Of 748 @ Camp Systems EFTA00618465

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57-1300 NO 4 DETAILED INSPECTION WINGS - TRAILING EDGE FLAPS - INBOARD FLAPS - INBOARD MAIN FLAP TRACKS. 84 AND 85 - RECOMMENDED FLAP INSPECTION AND EXCHANGE PROGRAM. SERVICE BULLETIN MOS 24 (5) 03-FEB-2010 AFL 5500 SB 737-57-1300 NO 5 DETAILED INSPECTION WINGS - TRAILING EDGE FLAPS - INBOARD FLAPS - INBOARD MAIN FLAP TRACKS. #4 AND 85 - RECOMMENDED FLAP INSPECTION AND EXCHANGE PROGRAM. SERVICE BULLETIN MOS 24 (s) 03-FEB-2010 SB 737-57-1306 26-SEP-2008 AFL 5500 INBOARD FLAPS - INBOARD MAIN FLAP TRACKS. #4 AND 85 - SUPER 0-GUN COATING. DETAILED INSPECTION AND EXCHANGE PROGRAM. SERVICE BULLETIN MOS 24 (s) AFL 5500 SB 737-57-1309 28-JAN-2011 WINGS - CENTER WING BOX- FRONT SPAR SHEAR FITTING - INSPECTION. REPAIR AND PREVENTIVE MODIFICATION. SERVICE BULLETIN MOS RECOMMENDED SB 737-57-1310 WINGS - CENTER WING - WING SPARS- FORWARD TRUNNION SUPPORT FITTING- FUSE PIN BORES - INSPECTION SUPERSEDED FOR CORROSION (SUPERSEDED BY SB 737-57-1310 RN. SERVICE BULLETIN MOS - Is) SB 737-57-1310 RI WINGS - CENTER WING - WING SPARS- FORWARD TRUNNION SUPPORT FITTING- FUSE PIN BORES - INSPECTION SUPERSEDED FOR CORROSION (SUPERSEDED BY SB 737-57-1310 R2). SERVICE BULLETIN MOS - Is) SB 737-57-1310 R2 WINGS - CENTER WING - WING SPARS- FORWARD TRUNNION SUPPORT FITTING- FUSE PIN BORES - INSPECTION RECOMMENDED FOR CORROSION. SERVICE BULLETIN MOS 120(s) SB 737-57-1312 WINGS - OUTER WING - WIRE BUNDLE SUPPORT GENERAL VISUAL INSPECTION. REPLACE TFE-4X WITH TFE-2X RECOMMENDED SLEEVE. SERVICE BULLETIN MOS 60 (s) 07-SEP-2010 SB 737-57-1316 WINGS - SPOILERS - INSTALLATION OF POLYURETHANE PROTECTIVE TAPE ON LOWER SKIN SURFACE OF INBOARD RECOMMENDED GROUND SPOILER NUMBER 6 AND 7. SERVICE BULLETIN MOS 05-SEP-2012 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 175 Of 748 @ Camp Systems EFTA00618466

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1279 24-JAN-2007 WINGS - CENTER AND OUTER WING - FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL INSPECTION (SUPERSEDED BY 737-57A1279 R1). SERVICE BULLETIN MOS SUPERSEDED S8 737-57A1279 RI CENTER AND OUTER WING - FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL INSPECTION SUPERSEDED (SUPERSEDED BY 737-57A1279 R2), SERVICE BULLETIN MOS (EFF) S8 737-57A1279 R2 WINGS - CENTER AND OUTER WING- FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL SUPERSEDED INSPECTION (SUPERSEDED BY SB 737-57A1279 R3). SERVICE BULLETIN MOS - (s) S8 737-57A1279 R3 WINGS - CENTER AND OUTER WING - FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL INSPECTION. SERVICE BULLETIN I5-FEB-20 I 1 SB 737-57A1279 R3 TABLE 1 24-JAN-2007 MOS (EFF) PERFORM WINGS - CENTER AND OUTER WING - FASTENER SEALING AND WIRE BUNDLE SUPPORT GENERAL VISUAL RECOMMENDED INSPECTION. SERVICE BULLETIN ACTIONS REQUIRED FOR FASTENER SEALEANT IN THE FUEL TANK AND WIRE CLAMP FOR GROUP 1.4 AIRPLANES MOS 60 (s) SB 737-57A1294 WINGS - WING CENTER SECTION - UPPER AND LOWER SWINGERS - DRILL START INSPECTION AND REPAIR. NOT APPLICABLE - BY EFFECTIVITY SB FOUND SERVICE BULLETIN TO BE NA BY VARIABLE NUMBER (YG006) MOS 16-FEB-2010 23-APR-2007 3417:51 AFL 829 SB 737-57A1294 TABLE 1 DETAILED INSPECTION WINGS - WING CENTER SECTION - UPPER AND LOWER STRINGERS - DRILL START INSPECTION AND REPAIR. SERVICE BULLETIN OF THE WING CENTER SECTION LOWER AND UPPER STRINGERS TO MINIMIZE CRACK SIZE. MOS 23-APR-2007 AFL 9000 9000 SB 737-57A1294 TABLE2 DETAILED INSPECTION WINGS - WING CENTER SECTION - UPPER AND LOWER STRINGERS - DRILL START INSPECTION AND REPAIR. SERVICE BULLETIN OF THE WING CENTER SECTION LOWER STRINGERS FOR SAFETY MOS 23-APR-2007 AFL 18000 18000 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 176 Of 748 @ Camp Systems EFTA00618467

C O MP Atiant.fran Ad-own/lop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1302 SB 737-57A1302 RI 78-OCT-2010 SB 737-57A1302 RI TABLE 1 A 15-DEC-2008 SB 737-57A1302 RI TABLE 1 LEADING EDGE SLATS- MAIN TRACK DOWN STOP MODIFICATION AND DETAILED INSPECTION (SUPERSEDED BY SB SUPERSEDED 737-57A1302 R1). SERVICE BULLETIN MOS WINGS - LEADING EDGE SLATS- MAIN TRACK DOWN STOP MODIFICATION AND DETAILED INSPECTION, SERVICE BULLETIN MOS 12-FEB-2014 3743:34 AFL 917 REPLACE WINGS - LEADING EDGE SLATS- MAIN TRACK DOWN STOP MODIFICATION AND DETAILED INSPECTION. SERVICE BULLETIN DOWN STOP ASSEMBLY HARDWARE WITH NEW DOWN STOP ASSEMBLY HARDWARE AND DOA DETAILED INSPECTION OF THE SLAT CANS AND SLAT MAIN TRACKS FOR DEBRIS IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. STEP 2. AT ALL 16 SLAT MAIN TRACK LOCATIONS.(A) FOR ALL AIRPLANES MOS 12-FEB-2014 - (s) 3743:34 AFL 917 REPLACE WINGS - LEADING EDGE SLATS- MAIN TRACK DOWN STOP MODIFICATION AND DETAILED INSPECTION. SERVICE BULLETIN AFT SIDE GUIDE BOLTS WITH NEW AFT SIDE GUIDE BOLTS IN ACCORDANCE WITH PARAGRAPH 3.8.. WORK INSTRUCTIONS. STEP 2. AT ALL 16 SLAT MAIN TRACK LOCATIONS.(A) FOR ALL AIRPLANES MOS 12-FEB-2014 15-DEC-2008 -(s) 3743:34 AFL 917 SB 737-57A1308 RI OUTER WING - SKINS - LOWER WING SKIN AT FUEL TANK ACCESS DOOR CUTOUT KEYWAY - INSPECTION AND CHANGE. SERVICE BULLETIN MOS 01-OCT-2009 SB 737-57A1308 RI TABLE 1.1 01-OCT-2009 SB 737-57A1308 RI TABLE 1.2 01-OCT-2009 PERFORM OUTER WING - SKINS - LOWER WING SKIN AT FUEL TANK ACCESS DOOR CUTOUT KEYWAY - INSPECTION AND CHANGE. SERVICE BULLETIN A ONE TIME INSPECTION FOR A KEYWAY IN THE FUEL TANK ACCESS DOOR 53188 AND 631BB CUTOUTS MOS AFL 7500 (s) PERFORM OUTER WING - SKINS - LOWER WING SKIN AT FUEL TANK ACCESS DOOR CUTOUT KEYWAY - INSPECTION AND CHANGE. SERVICE BULLETIN A ONE TIME HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE FUEL TANK ACCESS DOOR 531 BB CUTOUT KEYWAY AND FUEL TANK ACCESS DOOR 631BB CUTOUT KEYWAY ON THE LEFT AND RIGHT WING MOS AFL 7500 (s) COMPUED WITH - IAW. AD 2011-06-05 PARA (I) DETAILED INSPECTION AND MODIFICATION REPLACED ALL DOWN STOP ASSEMBLY HARDWARE- RECOMMENDED COMPUED WITH - DETAILED INSPECTION AND MODIFICATION REPLACED ALL DOWN STOP ASSEMBLY HARDWARE RECOMMENDED COMPUED WITH - DETAILED INSPECTION AND MODIFICATION REPLACED ALL DOWN STOP ASSEMBLY HARDWARE RECOMMENDED RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 177 Of 748 @ Camp Systems EFTA00618468

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1314 WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT - SUPERSEDED INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 RD. SERVICE BULLETIN MOS - (s) SB 737-57A1314 RI WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT - RECOMMENDED INSPECTION AND MODIFICATION. SERVICE BULLETIN MOS I5-JUL-2014 - (s) SB 737-57A1314 Ftt TBL TORQUE CHECK WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE RECOMMENDED 1.1 LH TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN FOR LOOSE FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (ALL AIRPLANES) MOS AFL 32000 (s) SB 737-57A1314 Rt TBL TORQUE CHECK WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY- INBOARD CARRIAGE TO TORQUE RECOMMENDED 1.1 RH TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN FOR LOOSE FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (ALL AIRPLANES) MOS AFL 32000 (s) SB 737-57A1314 RI TBL RETOROUE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 1.2 LH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT 7 ACCOMPLISH THE MODIFICATION (IF ANY LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE LEFT WING INBOARD FLAP ASSEMBLY) MOS 15-JUL-2014 BFIF (s) SB 737-57A1314 RI TBL RETOROUE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 1.3 RH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT / ACCOMPLISH THE MODIFICATION (IF ANY LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE RIGHT WING INBOARD FLAP ASSEMBLY) MOS IS-JUL-2014 BFIF (s) SB 737-57A1314 RI TBL DO WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE 1.4 LH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN ONE OF THE OPTIONS THAT FOLLOW: OPTION 1: ACCOMPLISH THE MODIFICATION! OPTION 2: RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (IF NO LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE LEFT WING INBOARD FLAP ASSEMBLY) MOS I5-JUL-2014 BFIF (s) RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 178 Of 748 @ Camp Systems EFTA00618469

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1314 R1 TBL 1.5 RH 15-JUL-2014 DO WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN ONE OF THE OPTIONS THAT FOLLOW: OPTION 1: ACCOMPLISH THE MODIFICATION! OPTION 2: RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (IF NO LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE RIGHT WING INBOARD FLAP ASSEMBLY) MOS BFIF (s) RECOMMENDED SB 737-57A1314 RI TBL REPLACE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 1.6 ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN EACH PART THAT HAS A CRACK OR WEAR OR CONTACT BOEING FOR A REPAIR AND DO THE REPAIR (IF ANY CRACK OR WEAR FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 6 - LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION THAT CANNOT BE REMOVED BY OVERSIZING THE TORQUE TUBE ATTACHMENT HOLE TO SECOND OVERSIZE) 5-JUL-2014 MOS BF/F (s) SB 737-57A1314 RI TBL REPLACE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 1.8 ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE INBOARD CARRIAGE OR CONTACT BOEING FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (IF ANY CHAFING OR FRETTING FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 38.. WORK INSTRUCTIONS. PART 6- LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION THAT IS DEEPER THAN 0.020 INCH) MOS 15-JUL-2014 BF/F (s) SB 737-57AI314 RI TBL WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT - RECOMMENDED 1.9 INSPECTION AND MODIFICATION. SERVICE BULLETIN BLEND THE INBOARD CARRIAGE TO REMOVE THE CHAFING AND FRETTING (IF ANY CHAFING OR FRETTING FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 3.B.. WORK INSTRUCTIONS. PART 6 - LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION UP TO A MAXIMUM DEPTH OF 0.020 INCH) MOS 15-JUL-2014 BF/F (s) SB 737-57AI314 RI TBL TORQUE CHECK WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE RECOMMENDED 2.01 LH TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN FOR LOOSE FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (ALL AIRPLANES) MOS AFL 11000(s) SB 737-57A1314 RI TBL TORQUE CHECK WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE RECOMMENDED 2.01 RH TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN FOR LOOSE FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (ALL AIRPLANES) MOS AFL 11000 (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 179 Of 748 @ Camp Systems EFTA00618470

CAMP AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1314 RI TBL 2.02 LH I5-JUL-2014 DETAIL INSPECTION WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE RECOMMENDED TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN OF THE INBOARD CARRIAGE FOR CHAFING AND FRETTING / RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT /ACCOMPLISH THE MODIFICATION (IF ANY LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE LEFT WING INBOARD FLAP ASSEMBLY) MOS BFIF (s) SB 737-57A1314 RI TBL ACCOMPLISH WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY- INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 2.03 LH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE MODIFICATION (IF ANY CHAFING OR FRETTING FOUND BY DETAILED INSPECTION OF INBOARD CARRIAGE OF THE LEFT WING INBOARD FLAP ASSEMBLY) MOS 15-JUL-2014 BFIF (s) SB 737-57A1314 RI TBL DETAIL INSPECTION WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE RECOMMENDED 2.05 RH TUBE ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN OF THE INBOARD CARRIAGE FOR CHAFING AND FRETTING / RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT 1 ACCOMPLISH THE MODIFICATION (IF ANY LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE RIGHT WING INBOARD FLAP ASSEMBLY) MOS I5-JUL-2014 BFIF (s) SB 737-57A1314 RI TBL ACCOMPLISH WINGS - TRAILING EDGE FLAPS- INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 2.06 RH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE MODIFICATION (IF ANY CHAFING OR FRETTING FOUND BY DETAILED INSPECTION OF INBOARD CARRIAGE OF THE RIGHT WING INBOARD FLAP ASSEMBLY) MOS 15-JUL-2014 BF/F (s) SB 737-57A1314 RI TBL DO WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE 2.08 LH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN ONE OF THE OPTIONS THAT FOLLOW: OPTION 1: ACCOMPLISH THE MODIFICATION! OPTION 2: RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (IF NO LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE LEFT WING INBOARD FLAP ASSEMBLY) MOS 5-JUL-2014 BF/F (s) SB 737-57A1314 RI TBL DO WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE 2.09 RH ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN ONE OF THE OPTIONS THAT FOLLOW: OPTION 1: ACCOMPLISH THE MODIFICATION! OPTION 2: RE-TORQUE THE INBOARD FOUR FASTENERS AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT (IF NO LOOSE FASTENER FOUND AT THE INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT OF THE RIGHT WING INBOARD FLAP ASSEMBLY) MOS 5-JUL-2014 BF/F (s) RECOMMENDED RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 180 Of 748 @ Camp Systems EFTA00618471

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1314 R1 TBL REPLACE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 2.10 ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN EACH PART THAT HAS A CRACK OR WEAR OR CONTACT BOEING FOR A REPAIR AND DO THE REPAIR (IF ANY CRACK OR WEAR FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 6 - LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION THAT CANNOT BE REMOVED BY OVERSIZING THE TORQUE TUBE ATTACHMENT HOLE TO SECOND OVERSIZE) 5-JUL-2014 MOS BF/F (s) SB 737-57AI314 RI TBL REPLACE WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE RECOMMENDED 2.12 ATTACHMENT - INSPECTION AND MODIFICATION. SERVICE BULLETIN THE INBOARD CARRIAGE OR CONTACT BOEING FOR REPAIR INSTRUCTIONS AND DO THE REPAIR (IF ANY CHAFING OR FRETTING FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 6- LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION THAT IS DEEPER THAN 0.020 INCH) MOS 5-JUL-2014 BF/F (s) SB 737-57AI314 RI TBL WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE ATTACHMENT - RECOMMENDED 2.13 INSPECTION AND MODIFICATION. SERVICE BULLETIN BLEND THE INBOARD CARRIAGE TO REMOVE THE CHAFING AND FRETTING (IF ANY CHAFING OR FRETTING FOUND DURING ACCOMPLISHMENT OF PARAGRAPH 3.8.. WORK INSTRUCTIONS. PART 6 - LEFT WING - MODIFICATION OR PART 7 - RIGHT WING - MODIFICATION UP TO A MAXIMUM DEPTH OF 0.020 INCH) MOS I5-JUL-2014 BF/F (s) SB 737-57A1314 TABLE TORQUE CHECK WINGS- TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE SUPERSEDED 1.1 TUBE ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 R1). SERVICE BULLETIN (REQUIRED MINIMUM FOR SAFETY) MOS - (s) SB 737-57A1314 TABLE ACCOMPLISH WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE SUPERSEDED 1.2 ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 RH. SERVICE BULLETIN THE MODIFICATION FOR LEFT WING (REQUIRED MINIMUM FOR SAFETY) MOS - (s) SB 737-57A1314 TABLE ACCOMPLISH WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE SUPERSEDED 1.3 ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 RH. SERVICE BULLETIN THE MODIFICATION FOR RIGHT WING (REQUIRED MINIMUM FOR SAFETY) MOS - (s) SB 737-57A1314 TABLE TORQUE CHECK WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE SUPERSEDED 2.1 TUBE ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 RI). SERVICE BULLETIN (RECOMMENDED ECONOMIC INSPECTION) MOS - Is) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks %Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 181 Of 748 @ Camp Systems EFTA00618472

C O MP Atiant.fran Meowed lip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-57A1314 TABLE ACCOMPLISH WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE SUPERSEDED 2.2 ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 R1). SERVICE BULLETIN THE MODIFICATION FOR LEFT WING (RECOMMENDED ECONOMIC INSPECTION) MOS - Is) SB 737-57A1314 TABLE ACCOMPLISH WINGS - TRAILING EDGE FLAPS - INBOARD FLAP ASSEMBLY - INBOARD CARRIAGE TO TORQUE TUBE SUPERSEDED 2.4 ATTACHMENT - INSPECTION AND MODIFICATION (SUPERSEDED BY SB 737-57A1314 R1). SERVICE BULLETIN THE MODIFICATION FOR RIGHT WING (RECOMMENDED ECONOMIC INSPECTION) MOS - (s) SB 737-71-1422 21 -JUN-I999 CONVERSION OF CFM56-76 TO 7827433. SERVICE BULLETIN MOS 7-OCT-2000 - (s) RECOMMENDED COMPUED WITH - CM SB 737-71-1422 RI CONVERSION OF CFM56-76 TO 7827433. SERVICE BULLETIN RECOMMENDED MOS 02-NOV-2000 - (s) SB 737-71-1422 R2 CONVERSION OF CFM56-76 TO 7827433. SERVICE BULLETIN RECOMMENDED MOS IS-FEB-2001 - (s) SB 737-71-1422 R3 CONVERSION OF CFM56-76 TO 7827/83. SERVICE BULLETIN MOS 12-FEB-2002 - (s) SB 737-71-1464 DRAIN TUBE REPLACEMENT. ENGINE FUEL PUMP PAD. SERVICE BULLETIN RECOMMENDED MOS 02-OCT-2003 SB 737-71-1551 RI POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-76 SINGLE ANNULAR SUPERSEDED COMBUSTOR (SACy3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES (SUPERSEDED BY SB 737-71-1551 R2). SERVICE BULLETIN MOS SB 737-71-1582 POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-7B SINGLE ANNULAR SUPERSEDED COMBUSTOR (SAC) ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-7B SAC/3 TECHNOLOGY INSERTION PROGRAM BASE ENGINES (SUPERSEDED BY SB 737-71-1582 R1). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 182 Of 748 @ Camp Systems EFTA00618473

C O MP A.m." vgnie• Megnsind AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71-1582 RI 58 737-71-1582 R2 13-JAN-2012 58 737-71-1588 02-AUG-2007 POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-78 SINGLE ANNULAR SUPERSEDED COMBUSTOR (SAC) ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-7B SAC/3 TECHNOLOGY INSERTION PROGRAM BASE ENGINES (SUPERSEDED BY SB 737-71-1582 R2). SERVICE BULLETIN MOS POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-7B SINGLE ANNULAR RECOMMENDED COMBUSTOR (SAC) ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-7B SACf3 TECHNOLOGY INSERTION PROGRAM BASE ENGINES. SERVICE BULLETIN MOS POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-7B SINGLE ANNULAR COMBUSTOR (SAC)/3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56- 78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES. SERVICE BULLETIN MOS SB 737-71-1588 RI POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC)/3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56- 78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES. SERVICE BULLETIN I5-AUG-2007 SB 737-71-1588 R2 I 7-DEC-2007 SB 737-71-1588 R3 24-DEC-2007 58 737-71-1588 R4 18-JUL-2008 MOS POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-76 SINGLE ANNULAR COMBUSTOR (SAC)/3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES. SERVICE BULLETIN MOS POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-76 SINGLE ANNULAR COMBUSTOR (SACO TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES. SERVICE BULLETIN MOS INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC)/3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 183 Of 748 @ Camp Systems EFTA00618474

C O MP A.m." vgnie• Megnundop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71-1588 RS 58 737-71-1588 R6 07-DEC-2011 58 737-71-1603 S8 737-71-1603 RI SB 737-71-1603 R2 S8 737-71-1603 R3 S8 737-71-1603 R4 58 737-71-1608 02-OCT-2009 INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFMS6-78 SINGLE ANNULAR COMBUSTOR (SAC)/3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFM56-78 SAC BASE ENGINES (SUPERSEDED BY S8 737-71-1588 R6). SERVICE BULLETIN MOS SUPERSEDED POWER PLANT - GENERAL - INTERMIX ONE OR SUBSTITUTE ANY COMBINATION OF CFM56-7B SINGLE ANNULAR RECOMMENDED COMBUSTOR (SACy3 TECHNOLOGY INSERTION PROGRAM ENGINES OR CFM56-78 HIGH PRESSURE COMPRESSOR AND/OR HIGH PRESSURE TURBINE TECHNOLOGY INSERTION KIT ENGINES FOR THE TWO CFMS6-78 SAC BASE ENGINES. SERVICE BULLETIN MOS POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF THE CFMS6-78 SAC/3 (TECH SUPERSEDED INSERTION) ENGINES FROM 7826/3 TO 782773 BUMP AND RETURN TO 7826/3 (SUPERSEDED BY SB 737-71-1603 RI). SERVICE BULLETIN MOS POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF THE CFM56-78 SAC/3 (TECH SUPERSEDED INSERTION) ENGINES FROM 7826/3 TO 7827/3 BUMP AND RETURN TO 7826/3 (SUPERSEDED BY SB 737-71-1603 R2). SERVICE BULLETIN MOS POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF THE CFMS6-78 SAM (TECH SUPERSEDED INSERTION) ENGINES FROM 7826/3 TO 782773 BUMP AND RETURN TO 7826/3 (SUPERSEDED BY SB 737-71-1603 R3). SERVICE BULLETIN MOS POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF THE CFM56-78 SAC/3 (TECH SUPERSEDED INSERTION) ENGINES FROM 7826/3 TO 7827/3 BUMP AND RETURN TO 7826/3 (SUPERSEDED BY S8 737-71-1603 R4). SERVICE BULLETIN MOS POWER PLANT -POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF THE CFM56-78 SAC/3 (TECH SUPERSEDED INSERTION) ENGINES FROM 7826/3 TO 782773 BUMP AND RETURN TO 7826/3 (SUPERSEDED BY S8 737-71-1603 RS). SERVICE BULLETIN MOS INSPECTION AND REPAIR OF THE ENGINE BUILD UP BRACKETS TO PREVENT DAMAGE TO THE ENGINE FAN CASE. SERVICE BULLETIN MOS RECOMMENDED 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 184 Of 748 @ Camp Systems EFTA00618475

C O MP A.m." vgnie• Megnund AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71-1625 POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF CFM56-78 ENGINES FROM CFM56-7824 TO CFM56-7826/B2 THRUST RATING OR FROM CFM56-7824/3 TO CFM56-7826/382 OR CFM56-7826/382F THRUST RATING. SERVICE BULLETIN MOS RECOMMENDED 28-JUL-2010 SB 737-71-1634 POWER PLANT - GENERAL - CHANGE THE OPERATIONAL THRUST RATING OF CFM56-78 SACJ3 (TECH INSERTION) SUPERSEDED ENGINES FROM 7827/3 TO 7B24/3 OR 7826/3. OR FROM 7826/3 TO 7824/3 (SUPERSEDED BY SB 737-71-1634 RI). SERVICE BULLETIN MOS S8 737-71-1634 RI POWER PLANT - GENERAL - CHANGE THE OPERATIONAL THRUST RATING OF CFM56-78 SACJ3 (TECH INSERTION) SUPERSEDED ENGINES FROM 7827/3 TO 7824/3 OR 7826/3. OR FROM 7826/3 TO 7824/3 (SUPERSEDED BY S8 737-71-1634 R2). SERVICE BULLETIN MOS SB 737-71-1634 R2 POWER PLANT - GENERAL - CHANGE THE OPERATIONAL THRUST RATING OF CFM56-78 SAC/3 (TECH INSERTION) RECOMMENDED ENGINES FROM 7827/3 TO 7824/3 OR 7826/3. OR FROM 7626/3 TO 7824/3, SERVICE BULLETIN MOS 15-DEC-2010 SB 737-71-1658 POWER PLANT - CHANGE ONE OR TWO CFM56-78E ENGINES FOR ONE OR ANY COMBINATION OF TWO CFM56-78 SUPERSEDED SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56-78/3 SAC ENGINES (SUPERSEDED BY S8 737-71-1658 RI). SERVICE BULLETIN MOS SB 737-71-1658 RI POWER PLANT - CHANGE ONE OR TWO CFM56-78E ENGINES FOR ONE OR ANY COMBINATION OF TWO CFM56-78 SUPERSEDED SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56-78/3 SAC ENGINES (SUPERSEDED BY S8 737-71-1658 R2). SERVICE BULLETIN MOS SB 737-71-1658 R2 POWER PLANT - CHANGE ONE OR TWO CFM56-78E ENGINES FOR ONE OR ANY COMBINATION OF TWO CFM56-78 RECOMMENDED SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56-78/3 SAC ENGINES. SERVICE BULLETIN MOS 08-DEC-2011 SB 737-71-1673 POWER PLANT - CHANGE ONE OR ANY COMBINATION OF TWO CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC) SUPERSEDED ENGINES OR CFM56-78/3 SAC ENGINES FOR ONE OR TWO CFM56-78E ENGINES (SUPERSEDED BY SB 737-71-1673 R1). SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 185 Of 748 @ Camp Systems EFTA00618476

CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71-1673 RI 08-DEC-2011 SB 737-71-1674 SB 737-71-1674 RI SB 737-71-1674 R2 08-DEC-2011 POWER PLANT - CHANGE ONE OR ANY COMBINATION OF TWO CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56.78:3 SAC ENGINES FOR ONE OR TWO CFM56-7BE ENGINES. SERVICE BULLETIN MOS POWER PLANT - CHANGE ONE OR ANY COMBINATION OF TWO CFP.I56-78 SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56.78:3 SAC ENGINES FOR ONE OR TWO CFM56-7BE ENGINES (SUPERSEDED BY SB 737-71-1674 RI). SERVICE BULLETIN MOS POWER PLANT - CHANGE ONE OR ANY COMBINATION OF TWO CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56.78:3 SAC ENGINES FOR ONE OR TWO CFM56-7BE ENGINES (SUPERSEDED BY SB 737-71-1674 R2). SERVICE BULLETIN MOS POWER PLANT - CHANGE ONE OR ANY COMBINATION OF TWO CFM56-78 SINGLE ANNULAR COMBUSTOR (SAC) ENGINES OR CFM56.78:3 SAC ENGINES FOR ONE OR TWO CFM56-7BE ENGINES. SERVICE BULLETIN MOS RECOMMENDED SUPERSEDED SUPERSEDED RECOMMENDED SB 737-71-1675 POWER PLANT - CHANGE TWO CFM56-78x2 DUAL ANNULAR COMBUSTOR (DAC) ENGINES FOR TWO CFM56-7BE SUPERSEDED ENGINES (SUPERSEDED BY S8 737-71-1675 RI). SERVICE BULLETIN MOS SB 737-71-1675 RI POWER PLANT - CHANGE TWO CFM56-78x2 DUAL ANNULAR COMBUSTOR (DAC) ENGINES FOR TWO CFM56-7BE RECOMMENDED 16-DEC-201I ENGINES. SERVICE BULLETIN MOS SB 737-71-1682 POWER PLANT - POWER PLANT - B1 FLANGE INSPECTION (SUPERSEDED BY S8 737-71-1682 R1). SERVICE BULLETIN SUPERSEDED MOS SB 737-71-1682 RI POWER PLANT - POWER PLANT - B1 FLANGE INSPECTION (SUPERSEDED BY S8 737-71-1682 R2). SERVICE BULLETIN SUPERSEDED MOS SB 737-71-1682 R2 POWER PLANT - POWER PLANT - B1 FLANGE INSPECTION (SUPERSEDED BY S8 737-71-1682 R3). SERVICE BULLETIN SUPERSEDED MOS SB 737-71-1682 R3 POWER PLANT - POWER PLANT - B1 FLANGE INSPECTION. SERVICE BULLETIN RECOMMENDED 07-MAR-2014 MOS ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 186 Of 748 Camp Systems EFTA00618477

CAMAsiont.P inn• Megnsind•fs' AD/SI Status Report 737-72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS. 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: OS-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71-1705 21-DEC-2010 POWER PLANT - POWER PLANT - CHANGE OPERATIONAL THRUST RATING OF CFM5G-7B ENGINES FROM 7822 TO RECOMMENDED 7824 AND RETURN TO 7822. SERVICE BULLETIN MOS SB 737-71-1709 POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OF TWO CFM56-78 ENGINES FROM RECOMMENDED 7826 TO 7827 AND RETURN TO 7826. SERVICE BULLETIN MOS 12-JAN-2011 • SB 737-71-1717 POWER PLANT - ENGINE COWLING - HEAT RESISTANT ALUMINIZED PRIMER INSTALLATION TO THE LIPSKIN OF THE RECOMMENDED ENGINE INLET COWL. SERVICE BULLETIN MOS 12-SEP-2013 SB 737-71-1725 POWER PLANT - POWER PLANT - INSTALLATION OF ENGINE OWNERSHIP PLACARD. SERVICE BULLETIN RECOMMENDED MOS 23-NOV-2011 • SB 737-71A1462 AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION. SERVICE BULLETIN 29-AUG-2C02 SB 737-71A1462 Fti POWER PLANT-ENGINE MOUNTS-AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION. SERVICE BULLETIN DAYS CO (5) DAYS 90 (5) 29-AUG-2C02 SB 737-71A1462 R2 AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. SERVICE RECOMMENDED BULLETIN MOS 29-MAY-2C03 SB 737-71A1462 R2 PART INSPECT AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. RECOMMENDED SERVICE BULLETIN FOR CORRECT INSTALLATION MOS 29-MAY-2C03 SB 737-71A1462 R2 PART APPLY AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. RECOMMENDED 2 SERVICE BULLETIN PERMANENT MARKINGS MOS 29-MAY-2C03 (51 ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CIW (EBT)-Estimated Base Time 187 Of 748 1, Camp Systems EFTA00618478

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-71A1462 R3 AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. SERVICE BULLETIN 20-MAY-2004 MOS 26-OCT-2011 3573:06 AFL 872 SB 737-71A1462 R3 PART INSPECT AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. 1 SERVICE BULLETIN FOR CORRECT INSTALLATION 20-MAY-2004 MOS 26-OCT-2011 3573:06 AFL 872 SB 737-71A1462 R3 PART INSTALL AFT ENGINE MOUNT. CENTER LINK ASSEMBLY INSTALLATION INSPECTION AND IDENTIFICATION OF PARTS. 2 SERVICE BULLETIN PERMANENTLY MARKED MOUNT 20-MAY-2004 MOS 26-OCT-2011 3573:06 AFL 872 COMPUED WITH - PERFORMED UNDER WO GVBBJ206 COMPUED WITH - PERFORMED UNDER WO GVBBJ206 COMPUED WITH - PERFORMED UNDER WO GVBBJ206 SB 737-73-1014 Of -JUL-7999 ELECTRONIC ENGINE CONTROL. SERVICE BULLETIN MOS I3-SEP-1999 - (s) RECOMMENDED COMPUED WITH-CM SB 737-73-1014 RI ELECTRONIC ENGINE CONTROL. SERVICE BULLETIN RECOMMENDED MOS 27-JUL-2000 - (s) SB 737-73A-026 . SERVICE BULLETIN MOS I3-SEP-1999 - (s) SB 737-73A1011 ENGINE FUEL SUPPLY HOSE (SUPERSEDED BY SB 737-73A1011 R1). SERVICE BULLETIN SUPERSEDED MOS - (s) SB 737-73A1011 RI ENGINE FUEL SUPPLY HOSE (SUPERSEDED BY SB 737-73A1011 R2). SERVICE BULLETIN SUPERSEDED MOS - (s) SB 737-73A1011 R2 ENGINE FUEL SUPPLY HOSE. SERVICE BULLETIN RECOMMENDED MOS I9-APR-2002 73-JUL-2000 988:36 AFL 250 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 188 Of 748 @ Camp Systems EFTA00618479

COMP Moan Aim thernand up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-73A1016 ELECTRONIC ENGINE CONTROL SOFTWARE CHANGE. SERVICE BULLETIN 20-FEB-2003 SB 737-73A1016 RI 08-MAY-2003 SB 737-77-1056 I6-AUG-2001 SB 737-77-1069 R2 10-DEC-2008 MOS 6 (s) 22-AUG-2003 1342 AFL 351 ELECTRONIC ENGINE CONTROL-SOFTWARE CHANGE. SERVICE BULLETIN MOS 22-AUG-2003 1342 AFL 351 AIRBORNE VIBRATION MONITORING SYSTEM UNIVERSAL SIGNAL CONDITIONER INSTALLATION, SERVICE BULLETIN RECOMMENDED MOS - (s) AIRBORNE VIBRATION MONITORING (AVM) SYSTEM - REPLACE CONDITIONER UNIT FOR CFM56-7B ENGINES. SERVICE BULLETIN MOS SB 737-78-1063 R2 EXHAUST- THRUST REVERSER - INNER WALL BLANKET INSULATION CHANGE. SERVICE BULLETIN MOS 28-MAR-2014 07-OCT-1999 SB 737-78-1067 THRUST REVERSER, SERVICE BULLETIN MOS 10-AUG-2000 3000 (s) 44 AFL 2100 38 RECOMMENDED COMPUED WITH COMPUED WITH NOT APPLICABLE - BY EFFECTIVITY SB 737-78-1069 28-FEB-2002 EXHAUST- THRUST REVERSER- INSULATION BLANKET MODIFICATION. SERVICE BULLETIN MOS - (s) SB 737-78-1069 RI EXHAUST - THRUST REVERSER - INSULATION BLANKET MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS I3-JUN-2002 SB 737-78-1069 R2 INSULATION BLANKET MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 06-FEB-2003 SB 737-78-1069 R3 INSULATION BLANKET MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 05-AUG-2004 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 189 Of 748 @ Camp Systems EFTA00618480

COMP Moan Aim thernand up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1069 R4 16-JUN-2005 SB 737-78-1071 06-DEC-2001 SB 737-78-1071 RI 09-MAY-2002 SB 737-78-1072 28-MAR-2002 SB 737-78-1073 EXHAUST - THRUST REVERSER - INSULATION BLANKET MODIFICATION. SERVICE BULLETIN MOS REPLACE THRUST REVERSER EXHAUST FASTNERS FOR TRACKING SEALS. SERVICE BULLETIN MOS - RECOMMENDED THRUST REVERSER - REPLACE FASTNERS FOR TRACK FAIRING SEALS. SERVICE BULLETIN RECOMMENDED MOS - (s) EXHAUST - THRUST REVERSER - INSPECT/CHANGE CASCADE SUPPORT RING TO CORRECTLY INSTALL BARREL RECOMMENDED NUTS. SERVICE BULLETIN MOS - (s) INSPECTION AND MODIFICATION OR REPLACEMNT OF BUSHINGS IN THE ATTACH FITTING ASSEMBLIES FOR THE RECOMMENDED COMPLIED WITH DRAG LINKS. SERVICE BULLETIN 09-DEC-2004 MOS 07-SEP-2005 2202:21 AFL 541 SB 737-78-1073 RI EXHAUST - THRUST REVERSER - BLOCKED DOORS - INSPECTION AND MODIFICATION OR REPLACEMENT OF RECOMMENDED BUSHINGS IN THE ATTACH FITTING ASSEMBUES FOR THE DRAG LINKS. SERVICE BULLETIN MOS 21-APR-2005 SB 737-78-1073 R2 EXHAUST - THRUST REVERSER - BLOCKERS DOORS - INSPECTION AND MODIFICATION OR REPLACEMENT OF BUSHINGS IN THE ATTACH FITTING ASSEMBUES FOR THE DRAG LINKS. SERVICE BULLETIN MOS 12-JAN-2006 SB 737-78-1073 R3 EXHAUST - THRUST REVERSER - BLOCKER DOORS - INSPECTION AND MODIFICATION OR REPLACEMENT OF BUSHINGS IN THE ATTACH FITTING ASSEMBUES FOR THE DRAG LINKS. SERVICE BULLETIN MOS 20-JUL-2006 SB 737-78-1073 R4 EXHAUST - THRUST REVERSER - BLOCKER DOORS - INSPECTION AND MODIFICATION OR REPLACEMENT OF BUSHINGS IN THE ATTACH FITTING ASSEMBUES FOR THE DRAG LINKS. SERVICE BULLETIN MOS 16-NOV-2006 SB 737-78-1074 EXHAUST - THRUST REVERSER - BLOCKER DOOR AERO/FIRE SEAL REPLACEMENT. SERVICE BULLETIN MOS 24 (s) 07-APR-2005 AFL 4000 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 190 Of 748 @ Camp Systems EFTA00618481

COMP Moan. Aim thernand up' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1074 RI EXHAUST - THRUST REVERSER - BLOCKER DOOR AEROIFI RE SEAL REPLACEMENT. SERVICE BULLETIN MOS 60 (s) 15-SEP-2005 AFL 8200 SB 737-78-1075 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND REPLACEMENT OF THE FIRE SEAL ON EACH THRUST SUPERSEDED REVERSER HALF (SUPERSEDED BY SB 737-78-1075 RI). SERVICE BULLETIN MOS SB 737-78-1075 RI EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND REPLACEMENT OF THE FIRE SEAL ON EACH THRUST SUPERSEDED REVERSER HALF (REPLACED BY 737-78-1086 R2). SERVICE BULLETIN MOS SB 737-78-1076 RI EXHAUST - THRUST REVERSER SYSTEM - REPLACEMENT OF CASCADE ASSEMBLIES. SERVICE BULLETIN RECOMMENDED MOS 12-MAR-2010 SB 737-78-1078 EXHAUST - THRUST REVERSER INDICATING SYSTEM - ADDITION OF A RESISTOR TO THE THRUST REVERSER SYNC LOCK TIME DELAY CIRCUIT. SERVICE BULLETIN SB 17-AUG-2006 737-78-1078 RI 30-MAY-2007 MOS EXHAUST - THRUST REVERSER INDICATING SYSTEM - ADDITION OF A RESISTOR TO THE THRUST REVERSER SYNC LOCK TIME DELAY CIRCUIT. SERVICE BULLETIN MOS SB 737-78-1078 R2 EXHAUST - THRUST REVERSER INDICATING SYSTEM - ADDITION OF A RESISTOR TO THE THRUST REVERSER SYNC LOCK TIME DELAY CIRCUIT. SERVICE BULLETIN MOS 19-FEB-2008 SB 737-78-1078 R3 THRUST REVERSER INDICATING SYSTEM - ADDITION OF A RESISTOR TO THE THRUST RECOMMENDED REVERSER SYNC LOCK TIME DELAY CIRCUIT. SERVICE BULLETIN MOS 16-OCT-2009 SB 737-78-1079 EXHAUST - THRUST REVERSER - THRUST REVERSER INNER WALL INSPECTION. REPAIR. AND COOLING HOLE MODIFICATION. SERVICE BULLETIN MOS 06-AUG-2007 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 191 Of 748 @ Camp Systems EFTA00618482

C O MP Atiant.fran Ad-own/lop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1079 RI 17-DEC-2007 SB 737-78-1079 R2 SB 737-78-1079 R3 SB 737-78-1082 SB 737-78-1082 RI 10-MAY-2012 SB 737-78-1083 SB 737-78-1083 RI SB 737-78-1083 RI TABLE 1 01-JAN-2000 EXHAUST - THRUST REVERSER - THRUST REVERSER INNER WALL INSPECTION. REPAIR. AND COOLING HOLE MODIFICATION 9SUPERSEDED BY 737-78-1079 R2). SERVICE BULLETIN MOS SUPERSEDED EXHAUST - THRUST REVERSER- THRUST REVERSER INNER WALL INSPECTION. REPAIR. AND COOLING HOLE SUPERSEDED MODIFICATION (SUPERSEDED BY SB 737-78-1079 R3). SERVICE BULLETIN MOS EXHAUST - THRUST REVERSER - THRUST REVERSER INNER WALL INSPECTION. REPAIR. AND COOLING HOLE MODIFICATION. SERVICE BULLETIN MOS EXHAUST - THRUST REVERSER - INSTALLATION OF A COOLING HOLE AND BUSHING. APPLY SEALANT AND INSTALL SUPERSEDED COMPLIED WITH - LAW. AD 2012-05-02 PARA (G) FLANGE INSULATION ASSEMBLIES ON THE THRUST REVERSERS (SUPERSEDED BY SB 737-78-1082 R1). SERVICE - FOUND SATISFACTORY - TOP KIT RETROFIT BULLETIN THR / 002A0004-16 MOS 12-FEB-2014 - (s) 3743:34 AFL 917 EXHAUST - THRUST REVERSER - INSTALLATION OF A COOLING HOLE AND BUSHING. APPLY SEALANT AND INSTALL FLANGE INSULATION ASSEMBLIES ON THE THRUST REVERSERS. SERVICE BULLETIN MOS 12-FEB-2014 - (s) 3743:34 RECOMMENDED DECLINED - NO MORE WORK IS NECESSARY ON THE AIRPLANE(S) CHANGED IN ACCORDANCE WITH THE ORIGINAL ISSUE OF THIS SERVICE BULLETIN. AFL 917 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST SUPERSEDED REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS (SUPERSEDED BY SB 737-78-1083 R1). SERVICE BULLETIN MOS - (s) EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST SUPERSEDED REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS (SUPERSEDED BY SB 737-78-1083 R2). SERVICE BULLETIN MOS DEATILED INSPECTION EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT SUPERSEDED OF THE THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS (SUPERSEDED BY SB 737-78-1083 R2). SERVICE BULLETIN OF THE THRUST REVERSER HYDRAULIC ACTUATOR ROD ENDS AND ACTUATOR ATTACH FITTINGS MOS - (s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 192 Of 748 @ Camp Systems EFTA00618483

C O MP Atiant.fran Ad-own/lop' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1083 R2 13-JUN-2014 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN MOS RECOMMENDED SB 737-78-1083 R2 TBL DETAILED INSPECTION EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT RECOMMENDED 1.01 OF THE THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN FOR DAMAGE ON THE HYDRAULIC ACTUATOR ROD END ASSEMBLIES AND A DETAILED INSPECTION FOR DAMAGE ON THE ACTUATOR ATTACH FITTINGS (FOR ALL AIRPLANES) (GROUP 1 - 2. CNF 2) MOS 30-JUN-2010 7500 (s) SB 737-78-1083 R2 TBL DO EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 1.03 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN DETAILED INSPECTIONS FOR DAMAGE ON THE HYDRAULIC ACTUATOR ROD END ASSEMBLIES (IF ANY DAMAGE FOUND ON THE HYDRAULIC ACTUATOR ROD END ASSEMBLIES) (GROUP 1 - 2. CNF 2) MOS 13-JUN-2014 BFIF SB 737-78-1083 R2 TBL REPAIR EXHAUST - THRUST REVERSER SYSTEM- INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 1.04 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN OR REPLACE THE HYDRAULIC ACTUATOR ROD END BODY (IF ANY DAMAGE FOUND ON HYDRAULIC ACTUATOR ROD END BODY AND THE DAMAGE IS LESS THAN OR EQUAL TO THE REPAIR LIMITS) (GROUP 1 - 2. CNF 2) MOS 13-JUN-2014 BF/F SB 737-78-1083 R2 TBL REPLACE EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE RECOMMENDED 1.05 THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN HYDRAULIC ACTUATOR ROD END ASSEMBLY (IF ANY DAMAGE FOUND ON HYDRAULIC ACTUATOR ROD END BODY AND THE DAMAGE IS GREATER THAN THE REPAIR LIMITS) (GROUP 1 - 2. CNF 2) MOS 13-JUN-2014 BFIF SB 737-78-1083 R2 TBL EXHAUST- THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 1.06 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN RETURN SPHERICAL BEARING TO SERVICE (IF WEAR LESS THAN OR EQUAL TO SERVICEABLE LIMITS FOUND ON SPHERICAL BEARING ON THE HYDRAULIC ACTUATOR ROD END) (GROUP 1 - 2. CNF 2) MOS 13-JUN-2014 BFIF SB 737-78-1083 R2 TBL REPLACE EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE RECOMMENDED 1.07 THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN THE SPHERICAL BEARING (IF WEAR GREATER THAN SERVICEABLE LIMITS FOUND ON SPHERICAL BEARING ON THE HYDRAULIC ACTUATOR ROD END) (GROUP 1 - 2. CNF 2) MOS 13-JUN-2014 BF/F 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 193 Of 748 @ Camp Systems EFTA00618484

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1083 R2 TBL 1.08 13-JUN-20I1 INSTALL EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN SPACER (IF NO DAMAGE FOUND ON AN ACTUATOR ATTACH FITTING) (GROUP 1 - 2. CNF 2) MOS BFIF RECOMMENDED 58 737-78-1083 R2 TBL REPAIR EXHAUST - THRUST REVERSER SYSTEM- INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 1.09 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN FITTING AND INSTALL SPACER (IF ANY DAMAGE FOUND ON ACTUATOR ATTACH FITTING AND THE DAMAGE IS LESS THAN OR EQUAL TO 0.020 INCH IN DEPTH) (GROUP 1- 2. CNF 2) MOS 13-JUN-2014 BFIF 58 737-78-1083 R2 TBL REPLACE EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE RECOMMENDED 1.10 THRUST REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN FITTING (IF ANY DAMAGE FOUND ON ACTUATOR ATTACH FITTING AND THE DAMAGE IS GREATER THAN 0.020 INCH IN DEPTH) (GROUP 1 - 2. CNF 2) MOS I3-JUN-2014 BFIF 58 737-78-1083 R2 TBL EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 1.11 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN CHANGE THE SCHEDULED MAINTENANCE PROGRAM (FOR AIRPLANES WITH WEAR SPACERS INSTALLED ON THE ACTUATOR ATTACH FITTINGS) (GROUP 1 - 2. CNF 2) MOS 20000 (s) 58 737-78-1083 R2 TBL EXHAUST - THRUST REVERSER SYSTEM - INSPECTION AND CHANGE TO OR REPLACEMENT OF THE THRUST RECOMMENDED 2.1 REVERSER ACTUATOR ATTACH FITTING AND ACTUATOR ROD ENDS. SERVICE BULLETIN CHANGE THE SCHEDULED MAINTENANCE PROGRAM (FOR ALL AIRPLANES WITH WEAR SPACERS INSTALLED ON THE ACTUATOR ATTACH FITTINGS) (GROUP 1 - 2. CNF 1) MOS 12 (s) 13-JUN-2014 SS 737-78-1085 EXHAUST - THRUST REVERSER SYSTEM - CHANGE TO THE INSULATION BLANKETS ON THE THRUST REVERSERS SUPERSEDED (SUPERSEDED BY SS 737-78-1085 RI). SERVICE BULLETIN MOS SS 737-78-1085 RI EXHAUST - THRUST REVERSER SYSTEM - CHANGE TO THE INSULATION BLANKETS ON THE THRUST REVERSERS. RECOMMENDED SERVICE BULLETIN MOS 16-DEC-2011 SS 737-78-1086 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION OF THE FIRE SEAL AND INSTALLATION OF A NEW FIRE SEAL SUPERSEDED BRACKET ON THE THRUST REVERSER (SUPERSEDED BY SB 737-78-1086 R1). SERVICE BULLETIN 1/10S - Is) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 194 Of 748 @ Camp Systems EFTA00618485

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB 737-78-1086 RI EXHAUST - THRUST REVERSER SYSTEM - INSPECTION OF THE FIRE SEAL AND INSTALLATION OF A NEW FIRE SEAL SUPERSEDED BRACKET ON THE THRUST REVERSER (SUPERSEDED BY SB 737-78-1086 R2). SERVICE BULLETIN MOS - (s) SB 737-78-1086 R2 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION OF THE FIRE SEAL AND INSTALLATION OF A NEW FIRE SEAL BRACKET ON THE THRUST REVERSER . SERVICE BULLETIN MOS SB 737-78-1087 REPLACEMENT OF THE LOCKOUT HANDLE ASSEMBLY ON THE THRUST REVERSER ACTUATORS (SUPERSEDED BY SUPERSEDED SB 737-78-1087 R1). SERVICE BULLETIN MOS SB 737-78-1087 RI EXHAUST - THRUST REVERSER SYSTEM - REPLACEMENT OF THE LOCKOUT HANDLE ASSEMBLY ON THE THRUST RECOMMENDED REVERSER ACTUATORS. SERVICE BULLETIN MOS 29-MAY-20 1 3 SB 737-78-1088 EXHAUST - THRUST REVERSER - THRUST REVERSER INNER WALL INSPECTION AND REPAIR (SUPERSEDED BY SB SUPERSEDED 737-78-1088 R1). SERVICE BULLETIN MOS - (s) SB 737-78-1088 RI EXHAUST- THRUST REVERSER - THRUST REVERSER INNER WALL INSPECTION AND REPAIR. SERVICE BULLETIN MOS SB 737-78-1089 EXHAUST - ENGINE PRIMARY EXHAUST NOZZLE AND PLUG ASSEMBLY INSTALLATION (SUPERSEDED BY SB SUPERSEDED 737-78-1089 R1). SERVICE BULLETIN MOS SB 737-78-1089 RI EXHAUST- ENGINE PRIMARY EXHAUST NOZZLE AND PLUG ASSEMBLY INSTALLATION. SERVICE BULLETIN RECOMMENDED MOS 25-OCT-2013 SB 737-78-1090 EXHAUST - THRUST REVERSER SYSTEM - INSPECTION FOR AND REMOVAL OF THE THRUST REVERSER INNER WALL COOLING HOLE BLOCKAGE. SERVICE BULLETIN MOS 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 195 Of 748 @ Camp Systems EFTA00618486

C O MP Atiant.fran Meowed up AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 737-78-1092 EXHAUST - TURBINE EXHAUST SYSTEM - REWORK OF INTERFERENCE CONDITION AT EXHAUST NOZZLE FORWARD RECOMMENDED LABYRINTH. SERVICE BULLETIN MOS 22-JAN-2013 SB 737-SL-21-056 RAM AIR INLET DUCT CLIP ASSEMBLY REPLACEMENT. SERVICE BULLETIN RECOMMENDED MOS 25-OCT-2002 -(5) SB 737-SL-28-044 AIRCRAFT USE OF DYED FUELS (SUPERSEDED BY SL 737-SL-28-044 REV. A). SERVICE BULLETIN SUPERSEDED SB 737-SL-30-020 OI -MAR-2006 SB 737-SL-31-034 MOS WINDOW HEAT CONTROL UNIT MODIFICATION TO CORRECT A4 CIRCUIT BOARD CORROSION. SERVICE BULLETIN MOS TAKEOFF CONFIGURATION WARNING- ALTERNATE METHOD OF COMPLIANCE A.D., SERVICE BULLETIN MOS SB 737-SL-32-129 REV. A NOSE GEAR LOCK VALVE MANIFOLD DUPLICATE SERIAL NUMBERS. SERVICE BULLETIN MOS I0-JUL-2006 SB 737-SL-32-134 REV. A NLG SHOCK STRUT ALTERNATE DYNAMIC SEAL. SERVICE BULLETIN MOS 10-JUL-2006 OPTIONAL SB 737-SL-32-154 MAIN LANDING GEAR ACTUATOR BARREL CRACKS RECOMMENDED FOLLOWING REPAIR PER SERVICE BULLETIN. SERVICE BULLETIN MOS 09-FEB-2009 AFL 500(s) SB 737-SL-34-187 LOSS OF RELIABLE AIR DATA DUE TO ICING OF STATIC PORTS - SRP 34-0111. SERVICE BULLETIN MOS 04-JUN-2007 SB 737-SL-52-046 AUXILIARY POWER UNIT (APU) ACCESS DOOR SKIN LATCH RECOMMENDED CUTOUTS. SERVICE BULLETIN MOS I4-APR-2009 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 196 Of 748 @ Camp Systems EFTA00618487

COMP Astant.fran Aetna/4pp AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC S8 920-34-25 ROCKWELL COLLINS - SB 25 - GLU-920 GLOBAL LANDING UNIT (CPN 822-1152-0011002/003) GNSS RECEIVER CIRCUIT CARD A8 (CPN 828-2940-302) REDUCE OCCURRENCE OF INCORRECT GPS DATE. SERVICE BULLETIN COMPLIED WITH 03-OCT-2008 MOS 23-FEB-2009 3353:18 AFL 804 SB 964-0452-23-39 COMMUNICATION - XK516D HF RADIO SYSTEM - UNIT MODIFICATION (MOD) 48 TO XK516D1 HF TRANSCEIVER (HF RECOMMENDED TRANSCEIVER). PN 964-0452-012. -042. OR -052: INSPECTION AND REPLACEMENT OF HIGH FREOUENCY (HF) MODEM NON-CONFORMING INTEGRATED CIRCUIT (VOICE BAND ANALOG INTERFACE). SERVICE BULLETIN MOS 05-N0V-2013 SB 965-0976-0XXX-34-38 . SERVICE BULLETIN R1 MOS - (s) SB A001-25-96 . SERVICE BULLETIN - IPECO SEATS MOS 13-SEP-1999 - (s) SB Bill 28-136 INSTALLATION OF COMPONENT IDENTIFICATIONS PLACARDS. SERVICE BULLETIN MOS - (s) SB BBJ-25-34 REMOVAL OF CARGO COMPARTMENT LOWER BILGE INSULATION BLANKETS. SERVICE BULLETIN MOS - (s) SB BB.J-28-001-K ST00936NY-D-28-SB-001- K SFAR 88 AFS INTERNAL FUEL CELL MODIFICATION AND VALVE PLATE ASSEMBLY. COMPLIED WITH SERVICE BULLETIN MOS 28-SEP-2009 3378:04 AFL 812 SB BBJ-28-02 MODIFICATION OF THE FORWARD HALF TANK, INBOARD SUPPORT RAIL. SERVICE BULLETIN MOS 17-AUG-1999 - (s) SB BBJ-28-021-K ST00936NY-D-28-SB-021-_K SFAR88 {AND FAR 25.981 (A) (8) (C1) (AMENDMENT 102)} AUXILIARY FUEL SYSTEM UPGRADE FOR PATS MODIFIED AIRCRAFT SERVICE BULLETIN, SERVICE BULLETIN MOS 28-SEP-2009 3378:04 AFL 812 RECOMMENDED COMPLIED WITH 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 197 Of 748 @ Camp Systems EFTA00618488

COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB BBJ-28-02A 17-AUG-1999 SB Bill-28-02B 15-OCT-1999 SB BBJ-28-02C 28-NOV-1999 SB BBJ-28-03 10-JUN-1999 SB BBJ-28-04 SB BBJ-28-04A 12-AUG-1999 SB BBJ-28-048 14-APR-2000 SB BEJ-28-05 10-JUN-1999 SB BBJ-28-06 MODIFICATION OF THE FORWARD HALF TANK. INBOARD SUPPORT RAIL. SERVICE BULLETIN MOS - Is) MODIFICATION OF THE FORWARD HALF TANK. INBOARD SUPPORT RAIL. SERVICE BULLETIN MOS - Is) MODIFICATION OF THE FORWARD HALF TANK. INBOARD SUPPORT RAIL. SERVICE BULLETIN MOS - (s) MODIFICATION OF THE AUXILIARY FUEL ELECTRICAL SYSTEM. SERVICE BULLETIN MOS - (s) MODIFICATION OF THE AUXILIARY FUEL SYSTEM PRESSURE SWITCH, SERVICE BULLETIN MOS - Is) MODIFICATION OF THE AUXILIARY FUEL SYSTEM PRESSURE SWITCH, SERVICE BULLETIN MOS - (s) MODIFICATION OF THE AUXILIARY FUEL SYSTEM PRESSURE SWITCH, SERVICE BULLETIN MOS - (s) INSTALLATIONOF AUXILIARY FUEL SHROUD DRAIN SYSTEM FLOW RESTRICTOR. SERVICE BULLETIN MOS - Is) MODIFICATION TO ADDED ELECTRONICS RACK FOR INCREASED LOAD CAPACITY. SERVICE BULLETIN MOS - (s) SB BBJ-28-09 CONVERSION FROM AN EXISTING NINE (4FWD. 5 AFT) AFS CONFIGURATION 2-G TO AN EIGHT CELL (3 FWD. 5 AFT) AFS. CONFIGURATION 2-F. SERVICE BULLETIN SB BBJ-28-098 MOS RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED CONVERSION FROM AN EXISTING NINE (4FWD. 5 AFT) AFS CONFIGURATION 2-G TO AN EIGHT CELL (3 FWD. 5 AFT) RECOMMENDED AFS. CONFIGURATION 2-F. SERVICE BULLETIN MOS 23-AUG-1999 -(s) 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 198 Of 748 @ Camp Systems EFTA00618489

CAMP fin. thermiewlqi AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB BBJ-28-09F 29-OCT-2001 CONVERSION FROM AN EXISTING NINE (4FWD. S AFT) AFS CONFIGURATION 2-G TO AN EIGHT CELL (3 FWD. S AFT) RECOMMENDED AFS. CONFIGURATION 2-F. SERVICE BULLETIN MOS - (s) SB BB.J-28-10 RELOCATION OF HOSE SHROUD CHECK VALVES. SERVICE BULLETIN RECOMMENDED MOS 10-JUN-1999 - (s) SB BBJ-28-108-A AUXILIARY FUEL SYSTEM (AFS) CONVERSION FROM AN EXISTING (2M) 1 FWD 5 AFT CELL CONFIGURATION TO A (3A) RECOMMENDED 0 FWD 3 AFT CELL CONFIGURATION, SERVICE BULLETIN MOS 08-MAR-2004 SB BBJ-28-11 INSTALLATION OF CARGO NET ATTACH PROVISIONS (FORWARD). SERVICE BULLETIN MOS - (s) SB BBJ-28-13 INSTALLATION: COMPONENT IDENTIFICATION PLACARDS. SERVICE BULLETIN MOS SB BBJ-28-13 . SERVICE BULLETIN - (s) MOS I3-SEP-1999 - (s) SB BBJ-28-13A INSTALLATION: COMPONENT IDENTIFICATION PLACARDS. SERVICE BULLETIN RECOMMENDED MOS 09-AUG-1999 - (s) SB BBJ-28-138 INSTALLATION OF COMPONENT IDENTIFICATIONS PLACARDS. SERVICE BULLETIN MOS - (s) SB BBJ-28-16 MODIFICATION OF THE AUX FUEL HALF TAW INBOARD SUPPORT RAIL. SERVICE BULLETIN MOS SB BBJ-28-16A 31-AUG-1999 - (s) MOUNTING OF THE AFT HALF FUEL CELL INBOARD SUPPORT RAIL AND THE ADDITION OF THE FASTENERS IN THE RECOMMENDED FLOOR BEAM REINFORCEMENT STRAPS. SERVICE BULLETIN MOS - PATS SB 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 199 Of 748 @ Camp Systems EFTA00618490

COMP Atant.fre• therrnewhip' AD/SI Status Report 737.72UBJ REVISION 21 SIN 29273 (YG006) (VP-BBJ): 3753:19HRS, 922 AFL as of 30-Jun-2014 AIRCRAFT Service Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SB BBJ-28-18 31-AUG-1999 SB BBJ-28-19 INSPECTION/MODIFICATION OF FASTENERS ON RAIL AND FLOOR. SERVICE BULLETIN MOS - Is) MODIFICATION OF THE WIRING OF THE AUX FUEL PROCESSING UNIT. SERVICE BULLETIN MOS - SB BBJ-28-19A MODIFICATION OF THE WIRING OF THE AUX FUEL PROCESSING UNIT. SERVICE BULLETIN 06-JUL-2001 MOS - (s) SB BBJ-28-21 FUEL MIGRATION PREVENTION. SERVICE BULLETIN MOS - (s) SB BBJ-28-21A SB Bill-28-21B SB Bill-28-21C FUEL MIGRATION PREVENTION.. SERVICE BULLETIN MOS - FUEL MIGRATION PREVENTION.. SERVICE BULLETIN MOS - FUEL MIGRATION PREVENTION.. SERVICE BULLETIN MOS - Is) SB BBJ-28-210 FUEL MIGRATION PREVENTION. SERVICE BULLETIN MOS 28-AUG-2009 07-SEP-2000 - (s) 3378:04 AFL 812 SB BBJ-28-23 MODIFICATION TO PREVENT BATTERY DRAINING. SERVICE BULLETIN MOS 01-JAN-2000 - (s) RECOMMENDED RECOMMENDED RECOMMENDED COMPLIED WITH SB BBJ-28-23A MODIFICATION TO PREVENT BATTERY DRAIN. SERVICE BULLETIN RECOMMENDED MOS 21-DEC-1999 - (s) SB BBJ-28-24 THE INSTALLATION OF A CLIP ASSEMBLY IN THE FORWARD CARGO COMPARTMENT TO ALLOW FOR THE PROPER RECOMMENDED REINSTALLATION OF THE FORWARD MOST CARGO NET AT THE CARGO BAY DOOR.. SERVICE BULLETIN MOS 14-JAN-2000 - 7-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 200 Of 748 @ Camp Systems EFTA00618491