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 BBJ-28-25 I9-JAN-2000 INSTALLATION OF A PLATE & CHANNEL IN THE FORWARD CARGO COMPARTMENT TO ALLOW FOR THE PROPER RECOMMENDED REINSTALLATION OF THE AFT MOST CARGO NET AT THE CARGO BAY DOOR. SERVICE BULLETIN MOS - (s) SB BBJ-28-26A CONVERSION: FROM (2 WD 5 Fl) TO el FWD 5 AFT) 6 TANK.. SERVICE BULLETIN MOS - (s) SB BBJ-28-268 CONVERSION: FROM (2 WD 5 Fl) TO el FWD 5 AFT) 6 TANK.. SERVICE BULLETIN MOS - (s) SB BBJ-28-26C CONVERSION: FROM A 7 TANK (2 WD 5 FT) TO A 6 TANK. ( FWD 5 AFT). SERVICE BULLETIN RECOMMENDED MOS 30-JUN-2060 - (s) SB BBJ-28-30 CONVERSION OF A SEVEN TANK FUEL SYSTEM TO A SIXTANK FUEL SYSTEM. SERVICE BULLETIN MOS - (s) SB BBJ-28-39E EIGHT CELL TO SEVEN CELL CONVERSION. SERVICE BULLETIN RECOMMENDED MOS 77-JUL-2001 - (s) SB BBJ-28-39F CONVERSION FROM AN EXISTING 8 TANK (3 FWD. 5 AFT) TO A 7 TANK (2 FWD. 5 AFT) AFS. CONFIGURATION. RECOMMENDED SERVICE BULLETIN 04-OCT-2001 SB BBJ-28-00A MOS - (s) SB BB-I-28-00B MODIFICATION TO FORWARD BLEED AIR. SERVICE BULLETIN RECOMMENDED MOS 29-SEP-2000 - (s) SB Bal-28-038 FUEL LINE BRACKET MODIFICATION. SERVICE BULLETIN RECOMMENDED MOS 29-SEP-2000 - (s) SB BBJ-28-45A RELOCATION OF CHECK VALVE IN MIX BAY. SERVICE BULLETIN RECOMMENDED MOS I8-SEP-2000 - (s) MOS MODIFICATION TO FWD BLEED AIR.. SERVICE BULLETIN 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 201 Of 748 @ Camp Systems EFTA00618492

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-28-458 I2-JUL-2001 SB BBJ-28-47F CONVERSION FROM 5 TANK(1 FWD 4 AFT) TO A4 TANK (0 FWD 4AFT) CONFIGURATION. SERVICE BULLETIN RECOMMENDED I6-AUG-2001 SB BBJ-28-56 REPLACEMENT OF THE BBJ FUELING PLACARDS. SERVICE BULLETIN SB BBJ-28-58 05-JUL-2001 SB BBJ-28-61 RELOCATION OF CHECK VALVE IN MIX BAY. SERVICE BULLETIN MOS MOS MOS - Is) - (s) - Is) REPLACEMENT OF THE BBJ CARGO LOADING PLACARDS. SERVICE BULLETIN MOS - (s) RECOMMENDED RECOMMENDED CONVERSION FROM AN EXISTING EIGHT CELL (3 FWD 5AFT) AFS. CONFIGURATION 2-F TO A SIX CELL (1 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 24.1. SERVICE BULLETIN MOS I7-APR-2001 -Is) SB BBJ-28-63C 09-NOV-2001 CONVERSION FROM AN EXISTING SIX CELL (2 FWD. 4 AFT) AFS. CONFIGURATION 2-D TO A EIGHT CELL (3 FWD. 5 AFT) RECOMMENDED AFS. CONFIGURATION 2-F WITH AFT STRUCTURAL PROVISIONS PREVIOUSLY INSTALLED. SERVICE BULLETIN MOS SB BBJ-28-67 CONVERSION FROM AN EXISTING SIX CELL (1 FWD 5 AFT) AFS. CONFIGURATION 2-M TO A SEVEN CELL (2 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 2-E.. SERVICE BULLETIN 05-DEC-2001 SB BBJ-28-6A 02-SEP-1999 SB BBJ-28-70 16-JAN-2002 SB BBJ-28-73A MOS - Is) MODIFICATION TO ADDED ELECTRONICS RACK FOR INCREASED LOAD CAPACITY. SERVICE BULLETIN MOS - (s) MODIFICATION OF THE EQUIPMENT EQUIPMENT RACK INSTALLED IN THE FORWARD CARGO COMPARTMENT. SERVICE BULLETIN MOS RELOCATION OF THE ATOP INSTALLED ON THE ELECTRICAL EQUIPMENT RACK IN THE FORWARD CARGO COMPARTMENT. SERVICE BULLETIN MOS 28-MAY-2002 - (s) 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 202 Of 748 @ Camp Systems EFTA00618493

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-28-78-D SB BBJ-28-78A 05-JUN-2002 SB BBJ-28-788 13-NOV-2002 SB BBJ-28-84A CONVERSION UPDATE TO SOFTWARE 2.1. SERVICE BULLETIN MOS 28-SEP-2009 3378:04 AFL 812 AIRCRAFT CONVERSION TO UPDATE TO SOFTWARE 2.1 (STC: ST00936NY). SERVICE BULLETIN MOS - (s) AIRCRAFT CONVERSION TO UPDATE TO SOFTWARE 2.1 (AFCU/AFDU). SERVICE BULLETIN MOS - (s) INSTALLATION OF PRESSURE EQUALIZATION PANELS INTO EXISTING AUXILIARY FUEL SYSTEM (AFS) CONFIGURATIONS WITH ONE TANK FORWARD AND/OR TWO. THREE AND FOUR TANKS AFT.. SERVICE BULLETIN MOS 08-OCT-2002 - (s) SB BBJ-28-84B INSTALLATION OF PRESSURE EQUALIZATION PANELS. SERVICE BULLETIN MOS 31-DEC-2003 - (s) RECOMMENDED RECOMMENDED RECOMMENDED SB BBJ-28-84C INSTALLATION OF PRESSURE EQUALIZATION PANELS INTO EXISTING AUXILIARY FUEL SYSTEM (AFS) RECOMMENDED CONFIGURATION WITH ONE TANK FORWARD AN/OR TWO. THREE. AND FOUR TANKS AFT. SERVICE BULLETIN MOS 27-FEB-2003 SB BBJ-28-86 CONVERSION FROM AN EXISTING SIX CELL (1FWD 5 AFT). CONFIGURATION 244 TO A NINE CELL (4 FWD 5 AFT) AFS. RECOMMENDED CONFIGURATION 2-G WITH STRUCTURAL PROVISIONS PREVIOUSLY INSTALLED. (STC: ST00936NY AMENDED JUNE 17. 2002). SERVICE BULLETIN MOS 28-AUG-2002 - (s) SB BBJ-28-86A CONVERSION FROM AN EXISTING SIX CELL (1 FWD 5 AFT), CONFIGURATION 3-M TO A NINE CELL (4 FWD 5 AFT) AFS. RECOMMENDED CONFIGURATION 3-G WITH STRUCTURAL PROVISIONS PREVIOUSLY INSTALLED.. SERVICE BULLETIN MOS 30-SEP-2002 - (s) SB BRJ-28-890 ADDING ADDITIONAL PROVISIONS ONLY TO AN EXISITING THREE CELL (0 FWD 3 AFT) AFS. CONFIGURATION 3-A. FOR RECOMMENDED FUTURE INSTALLATION OF 2 FWD TANKS FOR A FIVE CELL (2 FWD 3 AFT) AFS. CPNFIGURATION 3-C. SERVICE BULLETIN MOS 15-JAN-2003 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 203 Of 748 @ Camp Systems EFTA00618494

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 88J-28-89E 14-FEB-2003 SB 88J-28-89F I7-APR-2003 SB 88J-28-90 07-NOV-2002 SB 88J-28-90A 05-DEC-2002 SB 88J-28-92 22-NOV-2002 ADDING ADDITIONAL PROVISIONS ONLY TO AN EXISITING THREE CELL (0 FWD 3 AFT) AFS. CONFIGURATION 3-A. FOR RECOMMENDED FUTURE INSTALLATION OF 2 FWD TANKS FOR A FIVE CELL (2 FWD 3 AFT) AFS. CPNFIGURATION 3-C. SERVICE BULLETIN MOS CONVERSION OF EXISTING CONFIGURATION 3-A A THREE CELL (0 FWD 3 AFT) AFS PER STC ST00936NY TO A RECOMMENDED CONFIGURATION 3-C A FIVE CELL (2 FWD 3 AFT) AFS ALSO PER STC ST00936NY.. SERVICE BULLETIN MOS CONVERSION TO CONFIGURATION TO A FIVE CELL. SERVICE BULLETIN MOS RECOMMENDED CONVERSION FROM AN EXISTING SEVEN CELL (2 FWD. 5 AFT) AFS. CONFIGURATION 2-E TO A FIVE CELL (1 FWD. 4 RECOMMENDED AFT) AFS. CONFIGURATION 3-K. SERVICE BULLETIN MOS CONVERSION FROM AN EXISTING SIX CELL (1 FWD. 5 AFT) AFS. CONFIGURATION 2-M TO A SEVEN CELL (2 FWD. 5 RECOMMENDED AFT) AFS. CONFIGURATION 3-E. SERVICE BULLETIN MOS SB 88J-28-928 CONVERSION FROM AN EXISTING SIX CELL (1 FWD 5 AFT) AFS. CONFIGURATION 3-M TO A SEVEN CELL (2 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 3-E.. SERVICE BULLETIN MOS 20-NOV-2003 SB 88J-28-92C CONVERSION FROM AN EXISTING SIX CELL (1 FWD 5 AFT) AFS. CONFIGURATION 3-M TO A SEVEN CELL (2 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 3-E.. SERVICE BULLETIN MOS 02-DEC-2003 SB 88J-28-93 1S-JAN-2003 IN AUX FUEL MODIFIED AIRPLANES. TO RELOCATE EXPOSED TEST PLUG IN THE AFT CARGO COMPARTMENT 8. RECOMMENDED STOW THE FUEL CONNECTOR PLUG IN THE FWD CARGO TO A PROTECTED AREA. SERVICE BULLETIN MOS SB 88J-28-94A CONVERSION OF PREVIOUS CONFIGURATION: FROM AN EXISTING SIX CELL (1 FWD 5 AFT) AFS. CONFIGURATION RECOMMENDED 2-M TO A EIGHT CELL (3 FWD 5 AFT) AFS. CONFIGURATION 3-F. SERVICE BULLETIN MOS 17-APR-2003 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 204 Of 748 @ Camp Systems EFTA00618495

COMP Jm. thernanditfi 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 88J-28-95 CHANGE THE FUEL QUANTITY INDICATING SYSTEM FROM KILOGRAMS TO POUNDS STC: ST00936NY AMENDED JUNE RECOMMENDED 17. 2002. SERVICE BULLETIN MOS I0-MAR-2003 SB 88J-33-37A DE-ACTIVATIONIREACTIVATION OF CARGO LIGHTING ABOVE AUX FUEL TANKS. SERVICE BULLETIN MOS - (s) SB 88J-33-37B DE-ACTIVATION! REACTIVATION OF CARGO LIGHTING ABOVE AUX FUEL TANKS.. SERVICE BULLETIN RECOMMENDED MOS I3-NOV-2000 - (s) SB 88J-34-79 REMOVAL OF EXISTING ARINC 740 MILTOPE COCKPIT PRINTER AND AND REPLACE WITH ALLIED SIGNAL PRIMER. RECOMMENDED SERVICE BULLETIN MOS I4-MAR-2003 SB 88J-53-38A IMPROVED MIX BAY ACCESS.. SERVICE BULLETIN RECOMMENDED MOS 06-JUL-2001 - (s) SB BB-Q-28-08A AIRCRAFT CONVERSION TO UPDATE TO SOFTWARE 2.1 (STC SA01384NY). SERVICE BULLETIN RECOMMENDED MOS 05-JUN-2002 - (s) SB 88J2-28-11A CONVERSION FROM AN EXISTING SEVEN CELL (2 FWD 5 AFT) AFS. CONFIGURATION 1-G TOA SIX CELL (1 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 1-0. SERVICE BULLETIN MOS 08-JAN-2003 SB 88J2-28-118 15-APR-2003 CONVERSION FROM AN EXISTING SEVEN CELL (2 FWD 5 AFT) AFS. CONFIGURATION 1-G TOA SIX CELL (1 FWD 5 AFT) RECOMMENDED AFS. CONFIGURATION 1 -D. SERVICE BULLETIN MOS SB 88J2-28-15 CONVERSION FROM AN EXISITNG SIX CELL (2 FWD 4 AFT) AFS. CONFIGURATION 1-F TO A FIVE CELL (1 FWD 4 AFT) RECOMMENDED AFS. CONFIGURATION 1-C. SERVICE BULLETIN MOS 12-FEB-2003 SB 88J2-28-17A CHANGE FUEL OUANITY INDICATING SYSTEM. SERVICE BULLETIN RECOMMENDED MOS 21-FEB-2003 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 205 Of 748 @ Camp Systems EFTA00618496

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 BBJ2-28-9 IA CHANGE FUEL OUANITY INDICATING SYSTEM. SERVICE BULLETIN MOS SB CFM56-78S880-005 . SERVICE BULLETIN COMPUED WITH-CM SB CFMI-S872-168 . SERVICE BULLETIN MOS - (s) 10-AUG-2000 SB S-0380-34-02 . SERVICE BULLETIN MOS - (s) 17-OCT-2000 SB S-0380-34-03 . SERVICE BULLETIN MOS - (s) SB S8-17 . SERVICE BULLETIN MOS - (s) MOS - (s) SB TPR-901-34-10R2 ROCKWELL COLLINS- ELIMINATE OCCURANCE OF ERRANT MODE A CODE (0607) AND IMPROVE DESENDE RECOVERY TIMING. SERVICE BULLETIN MOS 20-DEC-2006 2785:43 AFL 661 SIL 920-08-1 ROCKWELL COLLINS - GLU-920 GLOBAL LANDING UNIT COMPUED WITH (CPN 822-1152-001/002=31220) GPS DATE CODE - 08-1. SERVICE INFORMATION LETTER MOS 23-FEB-2009 26-AUG-2008 3353:18 AFL 804 SIL D200808000008 R5 HONEYWELL HAS ISSUED A SPECIAL PRICE FOR THE PARTS NECESSARY FOR THE ATA 36 UPGRADES FOR 737. SERVICE INFORMATION LETTER MOS 07-AUG-20I3 SIL D201103000023 R1 INTRODUCTION OF WHEEL HUB ULTRASONIC INSPECTION KIT. PN 7416886. SERVICE INFORMATION LETTER RECOMMENDED MOS 27-NOV-20I3 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 206 Of 748 @ Camp Systems EFTA00618497

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 SIL D201104000050 R2 RE-INTRODUCTION OF VACUUM BLOWER. PN 606802-2. IN PLACE OF VACUUM BLOWER. PN 645172-1. -2. SERVICE OPERATORS 28-JUN-2013 INFORMATION LETTER MOS DISCRETION SIL D201311000043 POSSIBLE INCORRECT PACK DISCHARGE OVERHEAT SWITCH INSTALLED ON CERTAIN BOEING MODEL SUPERSEDED 737-800/-900/-900ER AIRCRAFT (SUPERSEDED BY SIL D201311000043 R1), SERVICE INFORMATION LETTER MOS SIL D201311000043 RI POSSIBLE INCORRECT PACK DISCHARGE OVERHEAT SWITCH INSTALLED ON CERTAIN BOEING MODEL RECOMMENDED 15-JAN-2011 737-800/-900/-900ER AIRCRAFT. SERVICE INFORMATION LETTER MOS SIL D201312000067 MK V ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS). PN 965-0976-003-XXX-XXX. PN RECOMMENDED 965-0976-020-XXX-XXX. PN 965-0976-040-XXX-XXX. PN 965-0976-060-XXX-XXX. PN 965-1676-00X. AND PN 965-1690-05X: 20-DEC-2013 END OF PRODUCTION ANNOUNCEMENT DUE TO PARTS OBSOLESCENCE. SERVICE INFORMATION LETTER MOS SIL D201401000052 BOEING 737 UGHT EMITTING DIODE (LED) WINGLET AND COLLISION LIGHT SYSTEM - WINGLET STROBE NOT RECOMMENDED 13-MAR-2011 FLASHING. SERVICE INFORMATION LETTER MOS SIL D201402000030 INSPECTION OF THE LEVER. PN 3177656-1 OR PN 63000974-1. AND ADAPTER ASSEMBLY. PN 3177635-2 OR -3. ON THE RECOMMENDED 26-FEB-2014 PRECOOLER CONTROL VALVE (PCCV). PN 3289562-6.-7. SERVICE INFORMATION LETTER MOS SL 737-SL-00-014 REV. A LOADABLE SOFTWARE MEDIA BINDERS. SERVICE LETTER INFORMATIONAL 19-SEP-2001 MOS - (s) SL 737-SL-00-015 FLIGHT DECK FAULT INDICATIONS AND NUISANCES MESSAGES. SERVICE LETTER INFORMATIONAL 29-JUN-1999 MOS - (s) SL 737-SL-00-016 SOFTWARE STORAGE ON DISKETTE SET. OTHER MEDIA SET. AND MASS STORAGE DEVICES. SERVICE LETTER INFORMATIONAL 20-SEP-1999 MOS - (s) SI. 737-SL-00-017 AVAILABILITY OF BOEING DISKETTE COPY PROCESS AND TOOL SET. (SUPERSEDED BY SL 737-SL-00-017 REV. A). SUPERSEDED SERVICE LETTER 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 207 Of 748 @ Camp Systems EFTA00618498

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 SL 737-SL-00-017 REV. A AVAILABILITY OF BOEING DISKETTE COPY PROCESS AND TOOL SET. SERVICE LETTER RECOMMENDED MOS 17-OCT-2012 SL 737-SL-00-019 SUSPECT DISCREPANCY REPORT PROCESS (SUPERSEDED BY SL 737-SL-00-019 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-00-019 REV. A SUSPECT DISCREPANCY REPORT PROCESS. SERVICE LETTER RECOMMENDED MOS I3-NOV-2012 SL 737-SL-00-020 PROCEDURES FOR SEEKING ALTERNATE METHOD OF COMPLIANCE APPROVAL. SERVICE LETTER MOS 24-JAN-2007 SL 737-SL-00-022 BOEING REVIEW PROCESS OF REQUESTS FOR AIRPLANE SYSTEMS AND FLIGHT OPERATIONS NO TECHNICAL OBJECTION (NTO). ACCEPTABLE. AND APPROVED (8100-9) DATA. SERVICE LETTER MOS 10-JAN-2008 SL 737-SL-00-022 REV. A BOEING REVIEW PROCESS OF REQUESTS FOR AIRPLANE SYSTEMS AND FLIGHT OPERATIONS NO TECHNICAL OBJECTION (NTO). ACCEPTABLE. AND APPROVED (8100-9) DATA. SERVICE LETTER MOS 12-MAR-2008 SI. 737-SL-00-022 REV. 8 BOEING REVIEW PROCESS OF REQUESTS FOR AIRPLANE SYSTEMS AND FLIGHT OPERATIONS NO TECHNICAL OBJECTION (NTO). ACCEPTABLE. AND APPROVED (8100-9) DATA (SUPERSEDED BY SL 737-SL-00-022 REV. C). SERVICE LETTER MOS INFORMATIONAL INFORMATIONAL INFORMATIONAL SUPERSEDED SL 737-SL-00-022 REV. C BOEING REVIEW PROCESS OF REQUESTS FOR AIRPLANE SYSTEMS AND FLIGHT OPERATIONS NO TECHNICAL SUPERSEDED OBJECTIONS. FAA 8100-9 FORMS. AND REPAIR AND DEVIATION RECORDS (SUPERSEDED BY SL 737-SL-00-022 REV. D), SERVICE LETTER MOS SL 737-SL-00-022 REV. D BOEING REVIEW PROCESS OF REQUESTS FOR AIRPLANE SYSTEMS AND FLIGHT OPERATIONS NO TECHNICAL RECOMMENDED OBJECTIONS. FAA 8100-9 FORMS. AND REPAIR AND DEVIATION RECORDS. SERVICE LETTER MOS I6-JUL-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 208 Of 748 @ Camp Systems EFTA00618499

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 SL 737-SL-00-023 SMOKE AND BURNING ODOR (SBO) EVENT SUMMARY. SERVICE LETTER INFORMATIONAL MOS 22-FEB-2008 • SL 737-SL-00-023 REV. A SMOKE AND BURNING ODOR (SBO) EVENT SUMMARY. SERVICE LETTER INFORMATIONAL MOS 24-NOv-2008 SL 737-SL-00-023 REV. B SMOKE AND BURNING ODOR (SBO) EVENT SUMMARY. SERVICE LETTER INFORMATIONAL MOS 17-DEC-2009 SL 737-SL-00-024 BOEING TECHNICAL COMMUNICATIONS (SUPERSEDED BY SL 737-SL-00-024 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-00-024 REV. A BOEING TECHNICAL COMMUNICATIONS. SERVICE LETTER RECOMMENDED MOS 11-APR-2011 SL 737-SL-00-025 DISCONTINUED USE OF 3.5 INCH FLOPPY DISKETTES FOR ONBOARD LOADABLE LRLI'S (SUPERSEDED BY SL SUPERSEDED 737-SL-00-025 REV. A). SERVICE LETTER MOS SL 737-SL-00-025 REV. A DISCONTINUED USE OF 3 5 INCH FLOPPY DISKETTES FOR ONBOARD LOADABLE LRUS (SUPERSEDED BY SL SUPERSEDED 737-SL-00-025 REV B). SERVICE LETTER MOS SL 737-SL-00-025 REV. B DISCONTINUED USE OF 3.5 INCH FLOPPY DISKETTES FOR ON BOARD LOADABLE LRUS (SUPERSEDED BY SL 737-SL-00-025 REV. C). SERVICE LETTER MOS SL 737-SL-00-025 REV. C DISCONTINUED USE OF 3 5 INCH FLOPPY DISKETTES FOR ONBOARD LOADABLE LRU.S. SERVICE LETTER MOS 23-JUL-2014 SL 737-SL-00-026 OPERATOR CORRECTION OF ERRORS IN THE LIFE LIMITED PART LIST AND AIRCRAFT READINESS LOG. SERVICE LETTER MOS 17-JAN.2014 SUPERSEDED RECOMMENDED RECOMMENDED ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time 209 Of 748 11 Camp Systems EFTA00618500

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 SL 737-SL-02-002 IN-FIGHT AIRFRAME VIBRATION. SERVICE LETTER INFORMATIONAL MOS 28-JUL-1987 - Is) St 737-SL-02-002 REV. A IN-FIGHT AIRFRAME VIBRATION. SERVICE LETTER INFORMATIONAL MOS 09-AUG-1995 - (s) St 737-SL-02-002 REV. B IN-FIGHT AIRFRAME VIBRATION. SERVICE LETTER INFORMATIONAL MOS I I -SEP-1996 - Is) St 737-SL-02-002 REV. C IN-FIGHT AIRFRAME VIBRATION. SERVICE LETTER INFORMATIONAL MOS 28-APR-1999 - Is) St 737-SL-02-002 REV. D IN FLIGHT AIRFRAME VIBRATION.. SERVICE LETTER INFORMATIONAL MOS 03-JUL-2001 - (s) St 737-SL-02-008 PASSENGER CARRY ON ELECTRONIC DEVICES (SUPERSEDED BY SL 737-SL-02-058 REV. A). SERVICE LETTER SUPERSEDED MOS 04-JUL-I 993 - (s) St 737-SL-02-008 REV. A PASSENGER CARRY ON ELECTRONIC DEVICES (SUPERSEDED BY SL 737-SL-02-058 REV. B). SERVICE LETTER SUPERSEDED MOS - (s) St 737-SL-02-008 REV. B PASSENGER CARRY ON ELECTRONIC DEVICES (SUPERSEDED BY SL 737-SL-02-058 REV. C), SERVICE LETTER SUPERSEDED MOS - St 737-SL-02-008 REV. C PASSENGER CARRY ON ELECTRONIC DEVICES (SUPERSEDED BY SL 737-SL-02-058 REV. D), SERVICE LETTER SUPERSEDED MOS - Is) St 737-SL-02-008 REV. D PASSENGER CARRY-ON ELECTRONIC DEVICES (SUPERSEDED BY 51 737-SL-02-008 REV. E), SERVICE LETTER SUPERSEDED MOS St 737-SL-02-008 REV. E PASSENGER CARRY-ON ELECTRONIC DEVICES (SUPERSEDED BY St 737-SL-02-008 REV. F). SERVICE LETTER SUPERSEDED 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 210 Of 748 @ Camp Systems EFTA00618501

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 SL 737-SL-02-008 REV. F PASSENGER CARRY-ON ELECTRONIC DEVICES. SERVICE LETTER 31 -JUL-2014 SL 737-SL-02-017 REDUCED VERTICAL SEPERATION MINIMUM (RVSM) QUALIFICATION.. SERVICE LETTER 10-FEB-1998 MOS MOS - (s) RECOMMENDED INFORMATIONAL SL 737-SL-02-017 REV. A REDUCED VERTICAL SEPERATION MINIMUM (RVSM) QUALIFICATION.. SERVICE LETTER INFORMATIONAL 25-SEP-1998 MOS - Is) SL 737-SL-02-017 REV. B REDUCED VERTICAL SEPERATION MINIMUM (RVSM) QUALIFICATION.. SERVICE LETTER INFORMATIONAL MOS 23-SEP-1998 - (s) SL 737-SL-02-017 REV. C REDUCED VERTICAL SEPERATION MINIMUM (RVSM) QUALIFICATION.. SERVICE LETTER INFORMATIONAL - INFORMATION COMPLIED WITH RVSM QUALIFICATION RENEWAL. CONTINUE IN REV.G MOS 27-JAN-2006 21-MAR-2001 2484:18 AFL 596 SL 737-SL-02-017 REV. 0 REDUCED VERTICAL SEPARATION MINIMUM (RVSM) QUALIFICATION. SERVICE LETTER INFORMATIONAL MOS 06-OCT-2003 SL 737-SL-02-017 REV. G REDUCED VERTICAL SEPARATION MINIMUM (RVSM) QUALIFICATION. SERVICE LETTER INFORMATIONAL COMPLIED WITH - FOUND NC ALREADY RVSM CERTIFIED MOS 24-AUG-2007 02-JUL-2004 2968:28 AFL 699 SL 737-SL-02-018 COMPLIANCE GUIDANCE TO EUROPEAN JOINT AVIATION AUTHORITY REQUIREMENTS FOR OPERATIONS. (JAR-OPS INFORMATIONAL I EUROPEAN). SERVICE LETTER MOS 26-MAR-1998 - Is) SL 737-SL-02-019 EXTENDED RANGE OPERATIONS WITH ETOPS NP CONFIGURATION CMP DOC, SERVICE LETTER INFORMATIONAL MOS 20-JAN-1999 - (s) SL 737-SL-02-020 BASIC AND PRECISION AREA NAVIGATION. SERVICE LETTER INFORMATIONAL MOS 04-JUN-2003 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 211 Of 748 @ Camp Systems EFTA00618502

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 SL 737-SL-02-020 REV. A BASIC AND PRECISION AREA NAVIGATION. SERVICE LETTER 03-NOV-2005 SL 737-SL-02-020 REV. 8 BASIC AND PRECISION AREA NAVIGATION. SERVICE LETTER I I -SEP-2006 SL 737-SL-02-020 REV. C BASIC AND PRECISION AREA NAVIGATION. SERVICE LETTER I2-FEB-2007 MOS MOS MOS SL 737-SL-02-021 UPDATE 10.5 INCORPORATION OF 2005 MAGNETIC VARIATION DATA. SERVICE LETTER MOS 23-MAR-2004 SL 737-SL-02-022 STATEMENT OF AIRCRAFT CAPABILITY IN REFERENCE TO TERMINAL AND EN-ROUTE AREA NAVIGATION IN UNITED STATES NATIONAL AIRSPACE. SERVICE LETTER MOS 31-AUG-2005 SI. 737-SL-02-022 REV. A STATEMENT OF AIRCRAFT CAPABILITY IN REFERENCE TO TERMINAL AND EN-ROUTE NAVIGATION IN UNITED STATES NATIONAL AIRSPACE. SERVICE LETTER MOS 22-SEP-2005 SI. 737-SL-02-022 REV. 8 STATEMENT OF AIRCRAFT CAPABILITY IN REFERENCE TO TERMINAL AND EN-ROUTE AREA NAVIGATION IN UNITED STATES NATIONAL AIRSPACE SERVICE LETTER MOS 29-JUN-2006 INFORMATIONAL INFORMATIONAL SL 737-SL-02-022 REV. C STATEMENT OF AIRCRAFT CAPABILITY IN REFERENCE TO TERMINAL AND EN-ROUTE AREA NAVIGATION IN UNITED SUPERSEDED STATES NATIONAL AIRSPACE (SUPERSEDED BY 737-SL-02-022 REV.D). SERVICE LETTER MOS 7-JUL-2007 SL 737-SL-02-022 REV. D STATEMENT OF AIRCRAFT CAPABILITY IN REFERENCE TO TERMINAL AND EN-ROUTE AREA NAVIGATION IN UNITED RECOMMENDED STATES NATIONAL AIRSPACE SERVICE LETTER MOS 08-FEB-20I2 SL 737-SL-02-023 TRANSPORT OF LIQUID CARGO. SERVICE LETTER RECOMMENDED MOS 15-DEC-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 212 Of 748 @ Camp Systems EFTA00618503

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 SL 737-SL-02-024 LITHIUM BATTERY FIRE FIGHTING RECOMMENDATIONS (SUPERSEDED BY SL 737-SL-02-024 REV. A). SERVICE LETTER MOS 51 737-SL-02-024 REV. A LITHIUM BATTERY FIRE FIGHTING RECOMMENDATIONS. SERVICE LETTER 28-APR-20I4 MOS 51 737-SL-03-004 AVIOD USE OF DRY CHEMICAL FIRE EXTINGUISHERS ON AIRPLANES. SERVICE LETTER MOS 16-AUG-2005 St 737-SL-03-004 REV. A AVOID USE OF DRY CHEMICAL FIRE EXTINGUISHERS ON AIRPLANES (SUPERSEDED BY SL 737-SL-03-004 REV. 8). SERVICE LETTER MOS SUPERSEDED RECOMMENDED SUPERSEDED SL 737-SL-03-004 REV. 8 AVOID USE OF DRY CHEMICAL FIRE EXTINGUISHERS ON AIRPLANES. SERVICE LETTER RECOMMENDED MOS 13-JUL-2011 SL 737-SL-03-004 REV. C AVOID USE OF DRY CHEMICAL FIRE EXTINGUISHERS ON AIRPLANES (SUPERSEDED BY SL 737-SL-03-004 REV. 0). SUPERSEDED SERVICE LETTER MOS SL 737-SL-03-004 REV. 0 AVOID USE OF DRY CHEMICAL FIRE EXTINGUISHERS ON AIRPLANES (SUPERSEDED BY SL 737-SL-03-004 REV. E). SUPERSEDED SERVICE LETTER MOS SL 737-SL-03-004 REV. E AVOID USE OF DRY CHEMICAL FIRE EXTINGUISHERS ON RECOMMENDED AIRPLANES. SERVICE LETTER MOS I8-FEB-2014 SL 737-SL-05-011 REPORTING PARTS DEPARTING AIRPLANE. SERVICE LETTER RECOMMENDED MOS 31 -JUL-2009 SL 737-SL-05-012 CONTROL AND ELIMINATION OF CIMICIDAE (BED BUGS) ON AIRPLANES. SERVICE LETTER RECOMMENDED MOS 24-MAY-2011 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 213 Of 748 @ Camp Systems EFTA00618504

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 SL 737-SL-05-013 I3-MAR-2014 SL 737-SL-05-014 CONTROL AND ELIMINATION OF RODENTS ON AIRPLANES. SERVICE LETTER 20-JAN-2014 St 737-SL-09-002 TOWBARLESS TOWING (SUPERSEDED BY a 737-SL-09-002 REV. A). SERVICE LETTER MOS REPORTING FUEL IMBALANCE EXCEEDANCES TO BOEING. SERVICE LETTER MOS MOS St 737-SL-09-002 REV. A TOWBARLESS TOWING (SUPERSEDED BY a 737-SL-09-002 REV. B). SERVICE LETTER MOS St 737-SL-09-002 REV. B TOWBARLESS TOWING (SUPERSEDED BY a 737-SL-09-002 REV. C), SERVICE LETTER MOS St 737-SL-09-002 REV. C TOWBARLESS TOWING (SUPERSEDED BY a 737-SL-09-002 REV. 0). SERVICE LETTER MOS St 737-SL-09-002 REV. 0 TOWBARLESS TOWING (SUPERSEDED BY a 737-SL-09-002 REV. E). SERVICE LETTER MOS St 737-SL-09-002 REV. E TOWBARLESS TOWING (SUPERSEDED BY a 737-SL-09-002 REV. F). SERVICE LETTER MOS I6-OCT-2009 St 737-SL-09-002 REV. F TOWBARLESS TOWING, SERVICE LETTER MOS I8-DEC-2013 St 737-SL-09-003 737 NOSE GEAR COLLAPSE POTENTIAL DURING TOWING4PUSHBACK SERVICE LETTER MOS I2-JUL-2007 St 737-SL-09-003 REV. A 737 NOSE GEAR COLLAPSE POTENTIAL DURING TOWING/PUSHBACK SERVICE LETTER MOS 17-JAN-2008 RECOMMENDED RECOMMENDED SUPERSEDED SUPERSEDED SUPERSEDED SUPERSEDED SUPERSEDED 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 214 Of 748 @ Camp Systems EFTA00618505

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 SL 737-SL-11-005 II -MAR-1998 -(s) 51 737-SL-11-005 REV. A RED CROSS PLACARDS. SERVICE LETTER 06-MAY-1998 -(s) 51 737-SL-11-005 REV. 8 RED CROSS PLACARDS. SERVICE LETTER 04-AUG-1998 SL 737-SL-11-007 PASSENGER ENTRY DOOR HANDLE ARROW PLACARD MODIFICATION.. SERVICE LETTER 08-OCT-1999 51 737-SL-11-009 EXTERNAL POWER PANEL-INCORRECT VOLTAGE MARKING. SERVICE LETTER 31-MAY-2000 -(s) 51 737-SL-11-010 LOWER CARGO COMPARTMENT LINER AND FLOOR PANEL REPLACEMENT.. SERVICE LETTER OI -JUN-2001 51 737-SL-11-010 REV. A EXTERIOR PLACARDS PEELING FROM AIRPLANE. SERVICE LETTER I5-APR-2003 51 737-SL-11-011 REV. A OWNER NAMEPLATE-INSPECTION AND REWORK. SERVICE LETTER 10-FEB-2004 51 737-SL-11-013 P18-2 CIRCUIT BREAKER MARKER WITH INCORRECT NOMENCLATURE. SERVICE LETTER MOS 26-SEP-2008 RED CROSS PLACARDS. SERVICE LETTER MOS MOS MOS MOS MOS MOS MOS MOS - (s) - (s) - (s) SI. 737-SL-11-013 REV. A P18-2 CIRCUIT BREAKER MARKER WITH INCORRECT NOMENCLATURE. SERVICE LETTER MOS I5-JUL-2009 INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL 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 215 Of 748 @ Camp Systems EFTA00618506

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 SL 737-SL-11-013 REV. 8 21-AUG-2009 P18-2 CIRCUIT BREAKER MARKER WITH INCORRECT NOMENCLATURE. SERVICE LETTER MOS 51 737-SL-11-014 E/E BAY ACCESS DOOR STENCILS. SERVICE LETTER RECOMMENDED 23-AUG-2013 MOS 51 737-SL-11-015 FORWARD AND AFT DOOR SILL DRAIN SYSTEM STENCIL REPLACEMENTS (SUPERSEDED BY SL 737-SL-11-015 REV. SUPERSEDED A). SERVICE LETTER MOS 51 737-SL-11-015 REV. A FORWARD AND AFT DOOR SILL DRAIN SYSTEM STENCIL REPLACEMENTS. SERVICE LETTER RECOMMENDED 02-JUN-2014 MOS - (s) 51 737-SL-12-011 AIRPLANE HIGH PRESSURE WASHING VIDEO. SERVICE LETTER INFORMATIONAL 25-JUN-1993 MOS - (s) 51 737-SL-12-011 REV. A AIRPLANE HIGH PRESSURE WASHING VIDEO. SERVICE LETTER INFORMATIONAL 02-APR-1999 MOS - 51 737-SL-12-011 REV. 8 AIRPLANE HIGH PRESSURE WASHING VIDEO (SUPERSEDED BY 737-SL-12-011 REV. C). SERVICE LETTER SUPERSEDED 18-MAY-1999 MOS -(s) SL 737-SL-12-011 REV. C AIRPLANE HIGH PRESSURE WASHING VIDEO, SERVICE LETTER RECOMMENDED 08-JUL-2010 MOS 51 737-SL-12-014 DEICING/ANTI-ICING FLUID RESIDUE REHYDRATION AND FREEZING.. SERVICE LETTER INFORMATIONAL MOS 11-JAN-2000 - (s) 51 737-SL-12-015 RECOMMENDED INTERVALS FOR TIRE PRESSURE CHECKS. SERVICE LETTER INFORMATIONAL MOS 13-JUL-2001 - (s) 51 737-SL-12-015 REV. A RECOMMENDED INTERVALS FOR TIRE PRESSURE CHECKS. SERVICE LETTER MOS 17-JUL-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 216 Of 748 @ Camp Systems EFTA00618507

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 SL 737-SL-12-01S REV. B RECOMMENDED INTERVALS FOR TIRE PRESSURE CHECKS. SERVICE LETTER 26-SEP-2007 SL 737-SL-12-016 09-OCT-2001 SI. 737-SL-12-017 CLEANING OF DEICING/ANTI-ICING FLUID RESIDUE FROM ELEVATOR BALANCE PANEL CAVITY AREA. SERVICE INFORMATIONAL LETTER MOS 10-APR-2002 - (s) MOS INTRODUCTION OF RE-BRANDED NAMES FOR APPROVED OILS. SERVICE LETTER MOS - Is) INFORMATIONAL SI. 737-SL-12-017 REV. A CLEANING OF DEICING/ANIT-ICI NG FLUID RESIDUE FROM ELEVATOR BALANCE PANEL CAVITY AREA. SERVICE INFORMATIONAL LETTER MOS 23-MAY-2002 - (s) SI. 737-SL-12-018 LANDING GEAR MAINTENANCE DURING COLD WEATHER OPERATION. SERVICE LETTER MOS 73-OCT-2006 SL 737-SL-12-018 REV. A LANDING GEAR MAINTENANCE DURING COLD WEATHER OPERATION. SERVICE LETTER MOS 18-MAR-2013 SL 737-SL-12-019 DEICING/ANTI-ICING FLUID RESIDUES CAUSING FLIGHT CONTROL RESTRICTIONS. SERVICE LETTER MOS 14-NOV-2006 SL 737-SL-12-019 REV. A DEICING/ANTI-ICING FLUID RESIDUES CAUSING FLIGHT CONTROL RESTRICTIONS. SERVICE LETTER MOS 28-AUG-2007 SL 737-SL-12-020 RECOMMENDED LANDING GEAR WASHING AND CLEANING PRACTICES (SUPERSEDED BY SL 737-SL-12-020 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-12-020 REV. A LANDING GEAR WASHING AND CLEANING PRACTICES. SERVICE LETTER RECOMMENDED MOS C6-JUN-2014 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 217 Of 748 @ Camp Systems EFTA00618508

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 SL 737-SL-12-022 20-JAN-2011 SL 737-SL-12-022 REV. A IATA GUIDANCE MATERIAL ON STANDARD INTO-PLANE FUEUNG PROCEDURES. SERVICE LETTER 27-JAN-2011 SL 737-SL-156-A UNPROTECTED WIRE BUNDLES IN P88 P9 PANELS, SERVICE LETTER MOS SL 737-SL-20-005 IATA GUIDANCE MATERIAL ON STANDARD INTO-PLANE FUEUNG PROCEDURES. SERVICE LETTER MOS MOS - (s) APPROVAL OF VENDOR MATERIALS FOR USE IN GENERAL AIRCRAFT MAINTENANCE (SUPERSEDED 8Y St 737-SL-20-005 REV. A). SERVICE LETTER MOS SL 737-SL-20-005 REV. A APPROVAL OF VENDOR MATERIALS FOR USE IN GENERAL AIRCRAFT MAINTENANCE (SUPERSEDED 8Y St 737-SL-20-005 REV. 8). SERVICE LETTER MOS St 737-SL-20-005 REV. 8 APPROVAL OF VENDOR MATERIALS FOR USE IN GENERAL AIRCRAFT MAINTENANCE (SUPERSEDED 8Y St 737-SL-20-005 REV. C). SERVICE LETTER MOS SL 737-SL-20-005 REV. C APPROVAL OF VENDOR MATERIALS FOR USE IN GENERAL AIRCRAFT MAINTENANCE (SUPERSEDED BY SL 737-SL-20-005 REV. D). SERVICE LETTER MOS SL 737-SL-20-005 REV. D APPROVAL OF VENDOR MATERIALS FOR USE IN GENERAL AIRCRAFT MAINTENANCE. SERVICE LETTER MOS I4-JAN-2014 SL 737-SL-20-012 QUICK REPAIR FUEL TANK SEALANT.. SERVICE LETTER MOS I -MAR-1987 - (s) SL 737-SL-20-012 REV. A QUICK REPAIR FUEL TANK SEALANT.. SERVICE LETTER MOS 04-MAY-1987 RECOMMENDED RECOMMENDED SUPERSEDED SUPERSEDED SUPERSEDED SUPERSEDED RECOMMENDED INFORMATIONAL INFORMATIONAL 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 218 Of 748 @ Camp Systems EFTA00618509

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 SL 737-SL-20-012 REV. 8 QUICK REPAIR FUEL TANK SEALANT.. SERVICE LETTER 31-MAR-1992 MOS - Is) SL 737-SL-20-012 REV. C QUICK REPAIR FUEL TANK SEALANT.. SERVICE LETTER MOS 05-FEB-2001 SL 737-SL-20-014 REV. 8 CONTROL CABLE CHANGE TO IMPROVE TENSION STABILITY. SERVICE LETTER MOS 20-OCT-2008 SL 737-SL-20-025 REV. A EVALUATION OF GENERAL PURPOSE GREASES FOR ROUTINE RELUBRICATION DURING AIRPLANE MAINTENANCE. SERVICE LETTER MOS 26-K1AR-2009 SL 737-SL-20-027 REV. C SUMMARY OF MOST COMMONLY USED GREASES ON BOEING AIRCRAFT. SERVICE LETTER MOS I6-NOV-2001 - (4) SL 737-SL-20-027 REV. D SUMMARY OF MOST COMMONLY USED GREASES ON BOEING AIRPLANES (SUPERSEDED BY SL 737-SL-20-027 REV. E). SERVICE LETTER MOS C6-AUG-2008 INFORMATIONAL INFORMATIONAL RECOMMENDED SI. 737-SL-20-027 REV. E SUMMARY OF MOST COMMONLY USED GREASES ON BOEING AIRPLANES (SUPERSEDED BY 737-SL-20-027 REV. F). SUPERSEDED SERVICE LETTER MOS SL 737-SL-20-027 REV. F SUMMARY OF MOST COMMONLY USED GREASES ON BOEING AIRPLANES. SERVICE LETTER RECOMMENDED MOS 26-JUN-20I3 SL 737-SL-20-029 REV. A AIRPLANE STATIC/ELECTRICAL GROUNDING RECOMMENDATIONS. SERVICE LETTER INFORMATIONAL MOS 20-MAY-2003 SL 737-SL-20-029 REV. B AIRPLANE STATIC/ELECTRICAL GROUNDING RECOMMENDATIONS. SERVICE LETTER INFORMATIONAL MOS 24-JUL-2003 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 219 Of 748 @ Camp Systems EFTA00618510

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 SL 737-SL-20-029 REV. C AIRPLANE STATIC/ELECTRICAL GROUNDING RECOMMENDATIONS. SERVICE LETTER O1-MAR-2005 SL 737-SL-20-032 REV. A BMS 3-33 GENERAL PURPOSE AIRCRAFT GREASE. SERVICE LETTER MOS I4-AUG-2001 - (s) SL 737-SL-20-032 REV. 8 BMS 3-33 GENERAL PURPOSE AIRCRAFT GREASE. SERVICE LETTER MOS 26-MAR-2009 SL 737-SL-20-034 CONTROL CABLE TENSION INSPECTION. SERVICE LETTER MOS MOS 03-MAY-1991 -144 SL 737-SL-20-034 REV. A WIRE BUNDLE/COAXIAL CABLE ORDERING/FABRICATING PROCEDURE SERVICE LETTER MOS I6-JUN-1997 - (s) SL 737-SL-20-034 REV. 8 WIRE BUNDLE/COAXIAL CABLE ORDERING/FABRICATING PROCEDURE SERVICE LETTER MOS I6-JUL-1999 - (s) SL 737-SL-20-035 AS HOSE INTERCHANGEABILIN FOR POTABLE AND GREY WATER. SERVICE LETTER MOS 20-JUL-1998 - (s) SL 737-SL-20-036 NAS1611. NAS1612. NAS1613SEAL AND SEAL MATERIAL CHANGES. SERVICE LETTER MOS 04-JUN-1999 - (s) SL 737-SL-20-037 LOW BREAKAWAY TORQUE ON KAYNAR NAS 1805-5L.. SERVICE LETTER MOS 30-MAY-2000 -(s) SL 737-SL-20-038 CONTROL CABLE TENSION INSPECTION. SERVICE LETTER MOS 31-OCT-2000 SL 737-SL-20-038 REV. A CONTROL CABLE TENSION INSPECTION. SERVICE LETTER 22-OCT-2002 - MOS INFORMATIONAL RECOMMENDED INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL 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 220 Of 748 @ Camp Systems EFTA00618511

C 4 11 Megnand 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 SL 737-SL-20-038 REV. 8 CONTROL CABLE TENSION INSPECTION. SERVICE LETTER I 7-JUL-2003 SL 737-SL-20-040 PART MARKING., SERVICE LETTER 30-MAY-2001 SL 737-SL-20-041 OVERHAUL OF HIGH STRENGTH STEEL COMPONENTS - CADMIUM STRIP REQUIRED. SERVICE LETTER 22-MAR-2002 MOS MOS MOS - (s) SL 737-SL-20-042 REV. A MATERIAL REVIEW BOARD ACTION ON TILEFLEX STANDARD HOSES SHIPPED AS SPARES. SERVICE LETTER MOS 28-JAN-2003 SL 737-SL-20-043 DEFERRED APPLICATION OF AERO-SEALANT, SERVICE LETTER MOS 16-AUG-2002 SL 737-SL-20-043 REV. A DEFERRED APPLICATION OF AERO-SEALANT IN ANTENNA INSTALLATIONS. SERVICE LETTER MOS 02-MAY-2003 SL 737-SL-20-043 REV. 8 DEFERRED APPLICATION OF AERO-SEALANT IN ANTENNA INSTALLATIONS. SERVICE LETTER MOS 13-NOV-2003 SL 737-SL-20-043 REV. C DEFERRED APPLICATION OF AERO-SEALANT IN ANTENNA INSTALLATIONS. SERVICE LETTER MOS I I -JUN-2007 INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL SL 737-SL-20-044 ESCAPEMENT OF NONCONFORMING FIELD EFFECT TRANSISTOR (FET) P/N S182-10802-5 (SUPERSEDED BY SL SUPERSEDED 737-SL-20-044 REV. A). SERVICE LETTER MOS St 737-SL-20-044 REV. A ESCAPEMENT OF NONCONFORMING FIELD EFFECT TRANSISTOR (FET) P/N S182-10802-5 (SUPERSEDED BY SUPERSEDED 737-SL-20-044 REV. 8). SERVICE LETTER MOS SL 737-SL-20-044 REV. 8 ESCAPEMENT OF NONCONFORMING FIELD EFFECT TRANSISTOR (FET) P/N S182-10802-5. SERVICE LETTER RECOMMENDED MOS I4-JUN-20 I 1 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 221 Of 748 @Camp Systems EFTA00618512

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 SL 737-SL-20-045 07-AUG-2003 SI. 737-SL-20-045 REV. A USE OF GASKET IN LIEU OF SEALANT FOR THE FOLLOWING ANTENNA INSTALLATION (SUPERSEDED BY SL SUPERSEDED 737-SL-20-045 REV. 8). SERVICE LETTER MOS GASKET IN LIEU OF SEALANT FOR ANTENNA INSTALLATIONS. SERVICE LETTER MOS INFORMATIONAL SL 737-SL-20-045 REV. 8 USE OF GASKET IN LIEU OF SEALANT FOR THE FOLLOWING ANTENNA INSTALLATIONS: AIR TRAFFIC CONTROL (ATC). RECOMMENDED DISTANCE MEASURING EQUIPMENT (DME). LOW RANGE RADIO ALTIMETER (LRRA). MARKER BEACON (MB). TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS). AND VERY HIGH FREQUENCY (VHF) COMMUNICATION ANTENNAS. SERVICE LETTER 19-NOV-20I3 SL 737-SL-20-047 07-JAN-2005 SL 737-SL-20-048 19-DEC-2005 MOS CIRCUIT BREAKER RELIABILITY. SERVICE LETTER MOS NAS1611-XXXA CODE O-RING STATIC SEALS - HYDRULIC FLUID EXTERNAL LEAKAGE LOW TEMPERATURES. SERVICE LETTER MOS SL 737-SL-20-048 REV. A NAS1611-XXXA CODE O-RING STATIC SEALS - HYDRAULIC FLUID EXTERNAL LEAKAGE AT LOW TEMPERATURES. SERVICE LETTER MOS 21-MAR-2006 SL 737-SL-20-048 REV. 8 NAS1611-XXXA CODE O-RING STATIC SEALS - HYDRAULIC FLUID EXTERNAL LEAKAGE AT LOW TEMPERATURES. SERVICE LETTER MOS 22-SEP-2006 SL 737-SL-20-048 REV. C NAS1611-XXXA CODE O-RING STATIC SEALS - HYDRAULIC FLUID EXTERNAL LEAKAGE AT LOW TEMPERATURES. SERVICE LETTER MOS 29-JUN-2007 SL 737-SL-20-048 REV. D NAS16114COCA CODE O-RING STATIC SEALS - HYDRAULIC FLUID EXTERNAL LEAKAGE AT LOW TEMPERATURES. SERVICE LETTER MOS 09-APR-2008 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 222 Of 748 @ Camp Systems EFTA00618513

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 SL 737-SL-20-049 I4-NOV-2006 SL 737-SL-20-049 REV. A BACC1OKB( ) CONNECTOR BACKSHELL CHAFE. SERVICE LETTER 21-NOV-2007 SI. 737-SL-20-050 REPAINTING AIRPLANES THAT EXHIBIT FUSELAGE DECORATIVE PAINT PEELING FROM RIVET HEADS - -RIVET RASH'. SERVICE LETTER IS-FEB-2007 BACC1OKB( ) CONNECTOR BACKSHELL CHAFE. SERVICE LETTER MOS MOS MOS SL 737-SL-20-05I POSSIBLE INCORRECT WIRING BRACKET LOCATION. SERVICE LETTER RECOMMENDED MOS IS-JUL-2009 SL 737-SL-20-05I REV. A POSSIBLE INCORRECT WIRING BRACKET LOCATION (SUPERSEDED BY SL 737-SL-20-051 REV. B). SERVICE LETTER SUPERSEDED MOS SL 737-SL-20-051 REV. B POSSIBLE INCORRECT WIRING BRACKET LOCATION. SERVICE LETTER MOS IS-JUL-2010 SL 737-SL-20-052 WIRE BUNDLE SUPPORT BRACKETS IN NOSE GEAR E/E BAY RECOMMENDED INCORRECTLY INSTALLED. SERVICE LETTER MOS 13-AUG-2009 SL 737-SL-20-052 REV. A WIRE BUNDLE SUPPORT BRACKETS IN NOSE GEAR E/E BAY RECOMMENDED INCORRECTLY INSTALLED. SERVICE LETTER MOS 02-OCT-2009 SL 737-SL-20-053 ELECTRICAL CONNECTOR CORROSION IN UNPRESSURIZED RECOMMENDED AREAS. SERVICE LETTER MOS 04-N0V-2009 SL 737-SL-20-054 SEVEN CONNECTORS WITH POTENTIALLY INCORRECT PLATING (SUPERSEDED BY SL 737-SL-20-054 REV. A). SUPERSEDED SERVICE LETTER 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 223 Of 748 @ Camp Systems EFTA00618514

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 SL 737-SL-20-054 REV. A SEVEN CONNECTORS WITH POTENTIALLY INCORRECT PLATING. SERVICE LETTER 30-SEP-2010 SL 737-SL-20-055 GROUND BLOCK CORROSION. SERVICE LETTER MOS 10-JAN-2012 SL 737-SL-20-056 28-MAR-2011 MOS RECOMMENDED RECOMMENDED INSPECTION FOR CORRECT LABELING OF THE TERMINAL BLOCKS IN THE .138 JUNCTION BOX. SERVICE LETTER RECOMMENDED MOS SL 737-SL-20-057 SAFETY WIRE (LOCKWIRE) MATERIAL SELECTION AND USAGE INTERCHANGEABILITY. SERVICE LETTER RECOMMENDED MOS 04-SEP-2013 SL 737-SL-21-033 REV. D RECOMMENDED ALLOWABLE DRY ICE CARRIAGE LIMITS. SERVICE LETTER MOS 28-MAY-2008 SL 737-SL-21-033 REV. E RECOMMENDED ALLOWABLE DRY ICE CARRIAGE LIMITS. SERVICE LETTER MOS 0I-AUG-2008 SL 737-SL-21-033 REV. F RECOMMENDED ALLOWABLE DRY ICE CARRIAGE LIMITS (SUPERSEDED BY SL 737-SL-21-033 REV. G). SERVICE SUPERSEDED LETTER MOS SL 737-SL-21-033 REV. G RECOMMENDED ALLOWABLE DRY ICE CARRIAGE LIMITS (SUPERSEDED BY SL 737-SL-21-033 REV. H). SERVICE SUPERSEDED LETTER MOS SL 737-SL-21-033 REV. H RECOMMENDED ALLOWABLE DRY ICE CARRIAGE LIMITS (SUPERSEDED BY SL 737-SL-21-033 REV. I). SERVICE SUPERSEDED LETTER MOS SL 737-SL-21-033 REV. I RECOMMENDED ALLOWABLE DRY ICE CARRIAGE LIMITS (SUPERSEDED BY SL 737-SL-21-033 REV. J). SERVICE SUPERSEDED LETTER 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 224 Of 748 @ Camp Systems EFTA00618515

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 SL 737-SL-21-033 REV. J RECOMMENDED ALLOWABLE DRY ICE CARRIAGE LIMITS. SERVICE LETTER 28-MAY-20I4 SL 737-SL-21-044 DIGITAL CABIN PRESSURE SYSTEM - CABIN PRESSURE EXCURSION DUE TO EMI (SUPERSEDED BY SL 737-SL-21-044 SUPERSEDED REV. A). SERVICE LETTER MOS MOS RECOMMENDED SL 737-SL-21-044 REV. A DIGITAL CABIN PRESSURE SYSTEM - CABIN PRESSURE EXCURSION DUE TO EMI (SUPERSEDED BY SL 737-SL-21-044 SUPERSEDED REV. B). SERVICE LETTER MOS SL 737-SL-21-044 REV. 8 DIGITAL CABIN PRESSURE SYSTEM -CABIN PRESSURE EXCURSION DUE TO EMI (SUPERSEDED BY SL 737-SL-21-044 SUPERSEDED REV. C). SERVICE LETTER MOS SL 737-SL-21-044 REV. C DIGITAL CABIN PRESSURE SYSTEM-CABIN PRESSURE EXCURSIONS DUE TO EMI (SUPERSEDED BY SL 737-SL-21-044 SUPERSEDED REV. D). SERVICE LETTER MOS SL 737-SL-21-044 REV. D DIGITAL CABIN PRESSURE SYSTEM -CABIN PRESSURE EXCURSION DUE TO EMI. SERVICE LETTER MOS 78-JUL-2011 SL 737-SL-21-045 SINGLE PACK DISPATCHABILITY CONFIDENCE CHECK. SERVICE LETTER MOS -SEP-1998 - (s) SL 737-SL-21-045 REV. A SINGLE PACK DISPATCHABILITY CONFIDENCE CHECK. SERVICE LETTER MOS 19-APR-1999 - (s) SL 737-SL-21-045 REV. 8 SINGLE PACK DISPATCHABILITY CONFIDENCE CHECK. SERVICE LETTER MOS 04-OCT-1999 - (s) SL 737-SL-21-045 REV. C SINGLE PACK DISPATCHABILITY CONFIDENCE (DISCO) CHECK. SERVICE LETTER MOS 03-JUN-2003 RECOMMENDED INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL 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 225 Of 748 @ Camp Systems EFTA00618516

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 SL 737-SL-21-045 REV. D SINGLE PACK DISPATCHABILITY CONFIDENCE (DISCO) CHECK. SERVICE LETTER 04-AUG-2CO3 SL 737-SL-21-045 REV. E SINGLE PACK DISPATCHABILITY CONFIDENCE (DISCO) CHECK. SERVICE LETTER 22-AUG-2007 MOS MOS SL 737-SL-21-045 REV. F SINGLE PACK DISPATCHABILITY CONFIDENCE (DISCO) CHECK. SERVICE LETTER MOS 02-JUN-2008 SL 737-SL-21-045 REV. G SINGLE PACK DISPATCHABILITY CONFIDENCE (DISCO) CHECK. SERVICE LETTER MOS 27-OCT-2009 INFORMATIONAL RECOMMENDED SL 737-SL-21-046 PASSENGER CABIN TEMPERATURE SENSOR INSTALLATION. SERVICE LETTER INFORMATIONAL 20-OCT-1998 MOS - Is) SL 737-SL-21-050 MODIFICATION OF THE AFT CABIN ZONE TEMPERATURE INDICATION SYSTEM WIRING.. SERVICE LETTER INFORMATIONAL 29-OCT-1999 MOS - Is) SL 737-SL-21-051 DIGITAL CABIN PRESSURE CONTROLLER-SOFTWARE UPGRADE. SERVICE LETTER INFORMATIONAL 29-OCT-1999 MOS - (s) SL 737-SL-21-052 AIR CYCLE MACHINE FAN DESIGN IMPROVEMENT.. SERVICE LETTER INFORMATIONAL 02-FEB-2000 MOS - Is) SL 737-SL-21-053 USE OF GROUND SOURCE CONDITIONED MR IN LIEU OF AIRPLANES ECS AIR CONDITIONING PACKS (SUPERSEDED SUPERSEDED BY SL 737-SL-21-053 REV. A). SERVICE LETTER MOS - (s) SL 737-SL-21-053 REV. A USE OF GROUND SOURCE CONDITIONED MR IN LIEU OF AIRPLANE ECS AIR CONDITIONING PACKS. SERVICE LETTER RECOMMENDED MOS I 7-OCT-2011 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 226 Of 748 @ Camp Systems EFTA00618517

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 SL 737-SL-21-055 02-JAN-2003 NEW RECIRCULATION AIR FILTER. SERVICE LETTER MOS SL 737-SL-21-056 REV. A RAM AIR INLET DUCT CLIP ASSEMBLY REPLACEMENT. SERVICE LETTER MOS 11-MAY-2004 • SL 737-SL-21-056 REV. C RAM AIR INLET DUCT CLIP ASSEMBLY REPLACEMENT. SERVICE LETTER MOS 02-DEC-2005 • SL 737-SL-21-056 REV. D RAM AIR INLET DUCT CLIP ASSEMBLY REPLACEMENT. SERVICE LETTER MOS 30-MAR-2006 • SL 737-SL-21-056 REV. E RAM AIR INLET DUCT CLIP ASSEMBLY REPLACEMENT. SERVICE LETTER MOS 23-MAR-2007 • SL 737-SL-21-056 REV. F RAM AIR INLET DUCT CLIP ASSEMBLY REPLACEMENT. SERVICE LETTER MOS 10-JUL-2007 SL 737-SL-21-058 SIDEWALL RISER DUCTS SEPARATE FROM THE DISTRIBUTION MANIFOLD. SERVICE LETTER MOS 21-JUL-2003 SL 737-SL-21-058 REV. B SIDEWALL RISER DUCTS SEPARATE FROM THE DISTRIBUTION MANIFOLD. SERVICE LETTER MOS 09-JUN-200,1 SL 737-SL-21-058 REV. C SIDEWALL RISER DUCTS SEPARATE FROM THE DISTRIBUTION MANIFOLD. SERVICE LETTER MOS 03-APR-2007 INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL SL 737-SL-21-059 AIR-CONDITIONING HIGH PRESSURE WATER SEPERATOR DRAM MANIFOLD INSPECTION. SERVICE LETTER MOS 18-JUL-2003 • SL 737-SL-21-060 RECOMMENDED CLEANING INTERVALS AND PROCEDURES FOR IN-FLIGHT ENTERTAINMENT (IFE) SYSTEM INFORMATIONAL COMPONENTS. SERVICE LETTER MOS 25-SEP-2003 9-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CNV (EBT)-Estimated Base Time 227 Of 748 1' Camp Systems EFTA00618518

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 SL 737-SL-21-060 REV. A CLEAN RECOMMENDED CLEANING INTERVALS AND PROCEDURES FOR IN-FLIGHT ENTERTAINMENT (IFE) SYSTEM RECOMMENDED COMPONENTS. SERVICE LETTER COOLING SYSTEM MOS 25-SEP-2003 SL 737-SL-21-060 REV. B INSPECT RECOMMENDED CLEANING INTERVALS AND PROCEDURES FOR IN-FLIGHT ENTERTAINMENT (IFE) SYSTEM RECOMMENDED COMPONENTS. SERVICE LETTER IFE EQUIPMENT MOS 25-SEP-2003 800 (s) SL 737-SL-21-062 REV. B OPTIONAL PART FOR RIGHT AIR CYCLE MACHINE (ACM) SENSE LINE. SERVICE LETTER MOS I6-APR-2007 SL 737-SL-21-062 REV. C AIR CYCLE MACHINE (ACM) SENSE LINES. SERVICE LETTER MOS I6-JAN-2009 SI. 737-SL-21-063 NUISANCE PACK/ZONE TEMP LIGHT ILLUMINATION ON RECALL THAT RESETS - CONTROLLER INPROVEMENT. NOT APPLICABLE - BY EFFECTIVITY - SERVICE LETTER MOS 30-SEP-2004 SL 737-SL-21-064 OUTFLOW VALVE SOFTWARE UPGRADE AND EMI ENHANCEMENT. SERVICE LETTER MOS 04-NOV-2004 SL 737-SL-21-065 AIR CONDITIONING FLEX HOSE SEPARATION AT THE OVERHEAD DISTRIBUTION TAPED JOINTS. SERVICE LETTER MOS 15-K4AR-2005 SL 737-SL-21-065 REV. A AIR CONDITIONING FLEX HOSE SEPARATION AT THE OVERHEAD DISTRIBUTION TAPED JOINTS. SERVICE LETTER MOS 23-AUG-2007 SL 737-SL-21-066 I9-JUL-2005 SL 737-SL-21-067 07-DEC-2005 COOLING PACK MR CYCLE MACHINE TURBINE TORUS EROSION. SERVICE LETTER MOS FLIGHT DECK MUFFLER REPLACEMENT. SERVICE LETTER 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 228 Of 748 @ Camp Systems EFTA00618519

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 SL 737-SL-21-068 AIRPLANE PRESSURIZATION - GUIDANCE TO UNDERSTANDING. SERVICE LETTER MOS 20-MAR-2006 51 737-SL-21-070 OUTFLOW VALVE MODIFICATION. SERVICE LETTER MOS I3-DEC-2006 51 737-SL-21-071 MISSING BOND JUMPER CABLE ON NC PACK. SERVICE LETTER MOS 30-NOV-2006 51 737-SL-21-071 REV. A MISSING BOND JUMPER CABLE ON NC PACK, SERVICE LETTER MOS 08-FEB-2007 51 737-SL-21-071 REV. B MISSING BOND JUMPER CABLE ON NC PACK, SERVICE LETTER MOS 09-APR-2007 51 737-SL-21-072 DIGITAL CABIN PRESSURE CONTROL SYSTEM - CONTROLLER SOFTWARE UPDATE. SERVICE LETTER MOS 23-FEB-2007 51 737-SL-21-072 REV. A DIGITAL CABIN PRESSURE CONTROL SYSTEM - CONTROLLER SOFTWARE UPDATE. SERVICE LETTER MOS 02-MAR-2007 51 737-SL-21-073 PRESSURIZATION TROUBLESHOOTING GUIDANCE. SERVICE LETTER MOS 24-JAN-2007 51 737-SL-21-074 COMPONENT INTERCHANGEABILITY - DIGITAL CABIN PRESSURIZATION SYSTEM (SUPERSEDED BY SL 737-SL-21-074 REV. A). SERVICE LETTER MOS 20-APR-2007 SL 737-SL-21-074 REV. A COMPONENT INTERCHANGEABILITY - DIGITAL CABIN PRESSURIZATION SYSTEM (SUPERSEDED BY SL 737-SL-21-074 REV. B). SERVICE LETTER MOS 23-DEC-2008 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 229 Of 748 @ Camp Systems EFTA00618520

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 SL 737-SL-21-074 REV. 8 COMPONENT INTERCHANGEABILITY - DIGITAL CABIN PRESSURIZATION SYSTEM (SUPERSEDED BY SL 737-SL-21-074 REV. C). SERVICE LETTER MOS SUPERSEDED SL 737-SL-21-074 REV. C COMPONENT INTERCHANGEABILITY - DIGITAL CABIN PRESSURIZATION SYSTEM (SUPERSEDED BY SL 737-SL-21-074 SUPERSEDED REV. 0). SERVICE LETTER MOS SL 737-SL-21-074 REV. D COMPONENT INTERCHANGEABILITY - DIGITAL CABIN PRESSURIZATION SYSTEM. SERVICE LETTER RECOMMENDED 24-JAN-2014 MOS SL 737-SL-21-075 DIAGNOSTIC CHECK OF THE MR CONDITIONING PACK. SERVICE LETTER MOS 01-MAY-2007 SL 737-SL-21-075 REV. A DIAGNOSTIC CHECK OF THE MR CONDITIONING PACK. SERVICE LETTER MOS 09-NOV-2007 SL 737-SL-21-075 REV. B DIAGNOSTIC CHECK OF THE MR CONDITIONING PACK. SERVICE LETTER MOS 30-APR-2008 SL 737-SL-21-077 AIR-CONDITIONING HIGH PRESSURE WATER SEPARATOR DRAIN MANIFOLD PLUG (SUPERSEDED BY SL 737-SL-21-077 REV. A). SERVICE LETTER MOS SUPERSEDED SL 737-SL-21-077 REV. A AIR-CONDITIONING HIGH PRESSURE WATER SEPARATOR RECOMMENDED DRAIN MANIFOLD PLUG. SERVICE LETTER MOS 24-JUN-20I4 SL 737-SL-21-078 FORWARD DOOR HEAT SYSTEM DUCT KINKING. SERVICE LETTER MOS 20-FEB-2008 SL 737-SL-21-078 REV. A FORWARD DOOR HEAT SYSTEM FLEXIBLE DUCT KINKING, SERVICE LETTER MOS 37 -JUL-2008 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 230 Of 748 @ Camp Systems EFTA00618521

C 4 11 Megnand 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 SL 737-SL-21-078 REV. B 02-APR-2009 FORWARD DOOR HEAT SYSTEM FLEXIBLE DUCT KINKING. SERVICE LETTER MOS RECOMMENDED SI. 737-SL-21-079 EÆ COOLING IN PS PANEL - POTENTIAL WIRE CHAFING RECOMMENDED AGAINST HOSE CLAMP. SERVICE LETTER MOS I2-MAY-2009 SL 737-SL-21-080 AIR-CONDITIONING DUCT CLAMP ASSEMBLY TORQUE. SERVICE LETTER RECOMMENDED MOS 23-JAN-2009 SL 737-SL-21-080 REV. A AIR-CONDITIONING DUCT CLAMP ASSEMBLY TORQUE. SERVICE LETTER RECOMMENDED MOS 31-MAR-2009 SL 737-SL-21-081 CABIN ALTITUDE AND DIFFERENTIAL PRESSURE INDICATOR RECOMMENDED 24-APR-2009 INSPECTION. SERVICE LETTER DAYS 90 (s) SL 737-SL-21-082 CABIN ALTITUDE AND DIFFERENTIAL PRESSURE INDICATOR RECOMMENDED I2-MAY-2009 REPLACEMENT. SERVICE LETTER MOS SL 737-SL-21-083 PROTECTIVE CAPS NOT REMOVED FROM MIX MANIFOLD RECOMMENDED 08-OCT-2009 TEMPERATURE SENSORS. SERVICE LETTER MOS SL 737-SL-21-084 TRANSPORTATION OF CRYOGENIC LIQUIDS (SUPERSEDED BY SL 737-SL-21-084 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-21-084 REV. A TRANSPORTATION OF CRYOGENIC LIQUIDS (SUPERSEDED BY SL 737-SL-21-084 REV. B). SERVICE LETTER SUPERSEDED MOS SL 737-SL-21-084 REV. B TRANSPORTATION OF CRYOGENIC LIQUIDS. SERVICE LETTER RECOMMENDED MOS I8-JUL-2011 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 231 Of 748 @Camp Systems EFTA00618522

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 SL 737-SL-21-086 DIGITAL CABIN SELECTOR PANEL - VALVE POSITION RECOMMENDED INDICATION REPLACEMENT. SERVICE LETTER MOS 23-DEC-2009 SL 737-SL-21-087 DIGITAL CABIN PRESSURE CONTROLLER - P/N 7121-19971-01XX ON-WING SERVICE LIFE. SERVICE LETTER RECOMMENDED MOS 15-FEB-2010 SL 737-SL-21-088 DIGITAL CABIN PRESSURE CONTROLLER - SOFTWARE FOR DOWNLOAD AND ANALYSIS OF NON-VOLATILE MEMORY. RECOMMENDED SERVICE LETTER MOS 20-JUL-2010 SL 737-SL-21-089 OUTFLOW VALVE: ATTACHMENT CLAMP:BOLT-INTERFERENCE CONDITION (SUPERSEDED BY SL 737-SL-21-089 REV. RECOMMENDED A). SERVICE LETTER MOS 26-JUL-2011 SL 737-SL-21-089 REV. A OUTFLOW VALVE: ATTACHMENT CLAMP:BOLT-INTERFERENCE CONDITION. SERVICE LETTER RECOMMENDED MOS 19-MAR-2013 SL 737-SL-21-091 AIR CONDITIONING TEMPERATURE CONTROL VALVE IMPROVEMENT (SUPERSEDED BY SL 737-SL-21-091 REV. A). SUPERSEDED SERVICE LETTER MOS SL 737-SL-21-091 REV. A AIR CONDITIONING TEMPERATURE CONTROL VALVE IMPROVEMENT. SERVICE LETTER RECOMMENDED MOS 04-SEP-2013 SL 737-SL-21-092 CABIN ENVIRONMENTAL QUALITY - INFECTION CONTROL GUIDELINES. SERVICE LETTER RECOMMENDED MOS 10-DEC-2012 SI. 737-SL-21-094 CABIN PRESSURE CONTROLLER. ADDITIONAL LAYER OF TAPE (ALOP) FOR COPPER TAPE PROTECTION. SERVICE RECOMMENDED LETTER MOS 30-MAY-2013 SI. 737-SL-21-095 ACMS 'USER GUIDE FOR ENHANCED PRESSURIZATION SYSTEM TROUBLESHOOTING AND HEALTH MANAGEMENT. RECOMMENDED SERVICE LETTER MOS 02-APR-2014 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 232 Of 748 @ Camp Systems EFTA00618523

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 SL 737-SL-21-096 PACK DISCHARGE OVERHEAT SWITCH - POSSIBLE WRONG PART NUMBER INSTALLED. SERVICE LETTER MOS 17-OCT-2013 RECOMMENDED SL 737-SL-21-097 POSSIBLE UNDER-TORQUE OF THE GROUNDING JUMPER TO THE RAM AIR INLET ACTUATOR. SERVICE LETTER RECOMMENDED MOS 03-MAR-2014 SI. 737-SL-21-099 SMART RAM AIR DOOR ACTUATOR (SRADA) - RAM AIR DOOR STATUS LIGHT ILLUMINATION - SUSPECT CONNECTOR SUPERSEDED BUILD (SUPERSEDED 8Y SI. 737-SL-21-099 REV. A). SERVICE LETTER MOS SI. 737-SL-21-099 REV. A SMART RAM AIR DOOR ACTUATOR (SRADA) - RAM AIR DOOR STATUS LIGHT ILLUMINATION - SUSPECT CONNECTOR RECOMMENDED BUILD. SERVICE LETTER MOS I4-JUL-2014 SL 737-SL-22-040 AUTOPILOT FLIGHT CONTROL COMPUTER IMPROVEMENTS. SERVICE LETTER MOS 21 -JAN-1999 - (s) SL 737-SL-22-040 REV. A AUTOPILOT FLIGHT CONTROL COMPUTER IMPROVEMENTS. SERVICE LETTER MOS I8-FEB-1999 - (s) SL 737-SL-22-040 REV. B AUTOPILOT FLIGHT CONTROL COMPUTER IMPROVEMENTS.. SERVICE LETTER MOS I0-FEB-2000 - (s) SL 737-SL-22-043 737 AUTO THROTTLE COMPUTER. SERVICE LETTER MOS 08-MAR-2000 - (s) SL 737-SL-22-044 FCC SOFTWARE UPDATE (-705), SERVICE LETTER MOS 31-MAY-2000 -(s) SL 737-SL-22-045 AUTOTHROTTLE COMPUTER MODIFICATION. SERVICE LETTER MOS 08-SEP-2000 - (s) SL 737-SL-22-046 FCC HARDWARE UPDATE (PM 10-62038-8).. SERVICE LETTER MOS I3-NOV-2000 - (s) INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL 74nsufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 233 Of 748 @ Camp Systems EFTA00618524

flP Megnand 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 SL 737-SL-22-046 REV. A FCC HARDWARE UPDATE (PM 10-62038-8) (SUPERSEDED BY SL 737-SL-22-046 REV. B). SERVICE LETTER MOS SL 737-SL-22-046 REV. 8 21-OCT-2011 SL 737-SL-22-047 I3-JUL-2001 SL 737-SL-22-048 06-MAR-2002 SL 737-SL-22-051 I I -JUN-2002 SL 737-SL-22-052 REV. 8 FCC HARDWARE UPDATE (P/N 10-62038-8). SERVICE LETTER MOS FCC SOFTWARE UPDATE (-708). SERVICE LETTER MOS - (s) SUPERSEDED RECOMMENDED INFORMATIONAL AUTO THROTTLE COMPUTER MODIFICATION (-54), SERVICE LETTER INFORMATIONAL MOS - INFORMATIONAL FCC SOFTWARE UPDATE(-709). SERVICE LETTER MOS COLLINS ENHANCED DIGITAL FLIGHT CONTROL SYSTEM (SUPERSEDED BY 51 737-SL-22-052 REV. C). SERVICE SUPERSEDED LETTER MOS SL 737-SL-22-052 REV. C COLLINS ENHANCED DIGITAL FLIGHT CONTROL SYSTEM, SERVICE LETTER RECOMMENDED MOS 29-JUL-2010 SL 737-SL-22-053 09-FEB-2004 COLLINS FCC SOFTWARE UPDATE (-120). SERVICE LETTER MOS INFORMATIONAL SL 737-SL-22-054 POTENTIAL CHAFFING OF W3397 WIRE BUNDLE TO M1020 ELEVATOR CONTROL'. SERVICE LETTER INFORMATIONAL MOS I 7-JUN-2004 SL 737-SL-22-054 REV. A POTENTIAL CHAFFING OF W3397 WIRE BUNDLE TO M1020 ELEVATOR CONTROL'. SERVICE LETTER INFORMATIONAL MOS 02-JUL-2004 SL 737-SL-22-054 REV. B POTENTIAL CHAFFING OF W3397 WIRE BUNDLE TO M1020 ELEVATOR CONTROL 'A", SERVICE LETTER INFORMATIONAL MOS 03-NOV-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 234 Of 748 @Camp Systems EFTA00618525

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 SL 737-SL-22-056 REV. A COLLINS FCC SOFTWARE UPDATE (-130). SERVICE LETTER I8-APR-2005 51 737-SL-22-056 REV. 8 COLLINS FCC SOFTWARE UPDATE (-130). SERVICE LETTER 21 -SEP-2005 MOS MOS INFORMATIONAL SL 737-SL-22-057 04-AUG-2006 COLLINS FCC SOFTWARE UPDATE (-100). SERVICE LETTER MOS SL 737-SL-22-058 HONEYWELL FCC SOFTWARE UPDATE (-710), SERVICE LETTER COMPUED WITH MOS 22-AUG-2008 09-AUG-2007 3260:48 AFL 782 SL 737-SL-22-059 COLLINS FCC SOFTWARE UPDATE (P5.0), SERVICE LETTER MOS 29-JUN-2007 SL 737-SL-22-060 CAT IIIB AUTOPILOT ROLLOUT RUDDER POSITION TRANSMITTER - MISSING LOCKWIRE. SERVICE LETTER MOS I9-FEB-2008 SL 737-SL-22-061 FIRST OFFICERS PITCH CONTROL WHEEL STEERING FORCE TRANSDUCER WIRE CONTACTING NEARBY WIRE RECOMMENDED BUNDLE CLAMP HARDWARE. SERVICE LETTER MOS 04-MAY-2011 SL 737-SL-22-062 COLLINS FCC SOFTWARE UPDATE (P7.0) (SUPERSEDED BY SL 737-SL-22-062 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-22-062 REV. A COLLINS FCC SOFTWARE UPDATE (P7.0), SERVICE LETTER RECOMMENDED MOS 17-OCT-2012 SL 737-SL-22-063 ROCKWELL COLLINS FCC HARDWARE UPDATE- PIN'S 822-1600-102 AND -152. SERVICE LETTER RECOMMENDED MOS 05-FEB-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 235 Of 748 @ Camp Systems EFTA00618526

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 SL 737-SL-22-064 AUTOTHROTTLE COMPUTER MODIFICATION (P/N 10-62017-55) (SUPERSEDED BY 737-SL-22-064 REV. A). SERVICE SUPERSEDED 51 737-SL-22-064 REV. A LETTER MOS AUTOTHROTTLE COMPUTER MODIFICATION (P/N 10-62017-55). SERVICE LETTER 51 737-SL-23-01 MOS PASSENGER ADDRESS AMPLIFIER MODIFICATION I6-MAY-1990 . SERVICE LETTER MOS 51 737-SL-23-020 VHF 8.33 I0-IZ CHANNEL SPACING, SERVICE LETTER INFORMATIONAL 16-SEP-1997 MOS -(s) 51 737-SL-23-020 REV. A VHF 8.33 I0-IZ CHANNEL SPACING. SERVICE LETTER INFORMATIONAL 16-DEC-1997 MOS -(s) 51 737-SL-23-020 REV. 8 VHF 8.33 KHZ CHANNEL SPACING. SERVICE LETTER INFORMATIONAL 28-MAY-1998 MOS -(s) 51 737-SL-23-020 REV. C VHF 8.33 I0-IZ CHANNEL SPACING. SERVICE LETTER INFORMATIONAL 28-MAY-1998 MOS -(s) 51 737-SL-23-021 HF ANTENNA COUPLER RELIABILITY. SERVICE LETTER INFORMATIONAL 18-MAR-1998 MOS - (s) 51 737-SL-23-021 REV. A HF ANTENNA COUPLER RELIABILITY. SERVICE LETTER INFORMATIONAL 09-APR-1998 MOS -(s) 51 737-SL-23-021 REV. 8 HF ANTENNA COUPLER RELIABILITY. SERVICE LETTER INFORMATIONAL 02-NOV-1998 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 236 Of 748 @ Camp Systems EFTA00618527

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 SL 737-SL-23-023 22-DEC-1998 RADIO COMMUNICATION COMPLIANT PINS. SERVICE LETTER MOS - Is) INFORMATIONAL 51 737-SL-23-024 COMMUNICATIONS-HF AUDIO DISTORTION ON OPPOSITE HF. SERVICE LETTER INFORMATIONAL 08-MAR-1999 MOS - (s) 51 737-SL-23-024 REV. A COMMUNICATIONS-HF AUDIO DISTORTION ON OPPOSITE HF. SERVICE LETTER INFORMATIONAL 27-MAY-1999 51OS - (s) 51 737-SL-23-025 COMMANDED FREQUENCY CHANGE. SERVICE LETTER INFORMATIONAL 23-APR-200O MOS - Is) 51 737-SL-23-025 REV. A COMMANDED FREQUENCY CHANGE.. SERVICE LETTER INFORMATIONAL 23-JAN-2001 MOS - (s) 51 737-SL-23-026 LOSS OF ESSENTIAL LEVELS VHF COMMUNICATIONS. SERVICE LETTER INFORMATIONAL 23-APR-1999 MOS - (s) 51 737-SL-23-026 REV. A LOSS OF ESSENTIAL LEVELS VHF COMMUNICATIONS. SERVICE LETTER INFORMATIONAL 27-MAY-1999 MOS - Is) 51 737-SL-23-026 REV. 8 LOSS OF ESSENTIAL LEVELS VHF COMMUNICATIONS. SERVICE LETTER INFORMATIONAL 26-AUG-1999 MOS - (s) 51 737-SL-23-027 SEAT ELECTRONICS BOX (SEB) MODIFICATION. SERVICE LETTER INFORMATIONAL C6-AUG-1999 MOS - SL 737-SL-23-028 VHF ANTENNA CONNECTION CHANGE. SERVICE LETTER INFORMATIONAL 13-JUL-2001 MOS - 51 737-SL-23-028 REV. A VHF ANTENNA CONNECTION CHANGE. SERVICE LETTER INFORMATIONAL 13-JUL-2001 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 237 Of 748 @ Camp Systems EFTA00618528

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 SL 737-SL-23-029 INTERPHONE SYSTEM - REMOTE ELECTRONICS UNIT MODIFICATION. SERVICE LETTER INFORMATIONAL 15-AUG-2000 MOS - Is) St 737-SL-23-030 BOEING RADIO COMMUNICATIONS PANEL UPGRADE TO P/N 285U0037-61X. SERVICE LETTER INFORMATIONAL MOS 27 -SEP-2000 -(s) SL 737-SL-23-030 REV. 8 COMMUNICATIONS - BOEING RADIO COMMUNICATIONS PANEL (RCP) UPGRADE TO P/N 2850003761X. SERVICE INFORMATIONAL LETTER MOS IO-AUG-2001 - Is) St 737-SL-23-031 CABIN ATTENDANT HANDSET/FLIGHT DECK HANDSET, P/14 285W0024. SHELL REPLACEMENT.. SERVICE LETTER INFORMATIONAL MOS 04-DEC-2000 - (s) St 737-SL-23-031 REV. A CABIN ATTENDANT HANDSET/FLIGHT DECK HANDSET, PIN 285W0024. SHELL REPLACEMENT.. SERVICE LETTER INFORMATIONAL MOS 04-APR-2001 - Is) St 737-SL-23-032 REV. A AUDIO - REMOTE ELECTRONICS UNIT (REU) PIN 10-62090-121 (AVTECH PM 5340-1-1). SERVICE LETTER INFORMATIONAL MOS I9-OCT-2001 -(s) St 737-SL-23-032 REV. 8 AUDIO-REMOTE ELECTRONICS UNIT PM 10-62090-121 (AVTECH PIN 5340-1-1). SERVICE LETTER INFORMATIONAL MOS 27-NOV-2002 St 737-SL-23-032 REV. C AUDIO-REMOTE ELECTRONICS UNIT PM 10-62090-121 (AVTECH FIN 5340-1-1). SERVICE LETTER INFORMATIONAL MOS I5-OCT-2003 St 737-SL-23-033 AUDIO CONTROL PANEL. P5-15. INTERFERENCE WITH SCREW. SERVICE LETTER INFORMATIONAL MOS OI -APR-2002 - (s) St 737-SL-23-033 REV. A AUDIO CONTROL PANEL. P5-15. INTERFERENCE WITH SCREW. SERVICE LETTER INFORMATIONAL MOS 26-NOV-2002 St 737-SL-23-035 HIGH FREQUENCY TRANSCEIVER. SERVICE LETTER INFORMATIONAL MOS I6-JUL-2002 - (s) 7-Insufficient Information +-Task exists in Inspection Manual (0-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 238 Of 748 @ Camp Systems EFTA00618529

C 4 11 Megnand 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 SL 737-SL-23-036 19-SEP-2003 SL 737-SL-23-037 GABLES NEW RADIO TUNING PANEL (RTP) PM G7404-12X. SERVICE LETTER 15-OCT-2003 SL 737-SL-23-037 REV. B GABLES NEW RADIO TUNING PANEL (RTP) PM G7404-12X. SERVICE LETTER 09-JAN-2009 SL 737-SL-23-038 ARINC EUROPEAN VHF REOUENCY CHANGE. SERVICE LETTER 10-SEP-2004 SL 737-SL-23-038 REV. A ARINC EUROPEAN VHF FREQUENCY CHANGE. SERVICE LETTER 10-MAY-2005 SL 737-SL-23-038 REV. B 13-AUG-2009 SL 737-SL-23-039 03-NOV-2004 SL 737-SL-23-040 28-FEB-2005 SL 737-SL-23-041 II -OCT-2006 SI. 737-SL-23-042 27 -SEP-2007 MULTI-INPUT INTERACTIVE DISPLAY UNIT (MIDU) PIN 964-0443-002/-003 MODIFICATION. SERVICE LETTER MOS MOS MOS MOS MOS 28-APR-2006 2606:18 AFL 626 ARINC EUROPEAN VHF FREQUENCY CHANGE. SERVICE LETTER MOS UNCOMMANDED CHANGE OF VHF COMMUNICATIONS FREQUENCY, SERVICE LETTER MOS PASSENGER ADDRESS (PA) POPPING/CRACKLING SOUND. SERVICE LETTER MOS VHF NUMBER TWO ANTENNA CONNECTORS DISCONNECTING. SERVICE LETTER MOS VHF-2100 COM TRANSCEIVER - KEY EVENT SIGNAL LEVEL CORRECTION. SERVICE LETTER MOS INFORMATIONAL INFORMATIONAL INFORMATIONAL RECOMMENDED INFORMATIONAL 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 239 Of 748 @Camp Systems EFTA00618530

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 SL 737-SL-23-043 12-JAN-2009 VHF-920 DATA RADIO (822-1250-002) - MODE LOCK-UP CONDITION. SERVICE LETTER MOS SL 737-SL-23-043 REV. A VHF-920 DATA RADIO (822-1250-002) - MODE LOCK-UP CONDITION. SERVICE LETTER MOS 09-JUL-2009 SL 737-SL-23-044 NOISE ON SERVICE INTERPHONE. SERVICE LETTER MOS I9-JAN-2010 SL 737-SL-23-044 REV. A NOISE ON SERVICE INTERPHONE (SUPERSEDED BY 737-SL-23-044-B). SERVICE LETTER MOS 26-JAN-2010 SL 737-SL-23-044 REV. B NOISE ON SERVICE INTERPHONE. SERVICE LETTER MOS I3-MAY-2010 RECOMMENDED RECOMMENDED SUPERSEDED SL 737-SL-23-045 MISWIRING OF TERMINAL BLOCKS IN CVR SELF-TEST WIRING. SERVICE LETTER RECOMMENDED MOS 22-DEC-2010 SI. 737-SL-23-046 BOEING SKY INTERIOR ATTENDANT CONTROL PANEL SOFTWARE IMPROVEMENTS-LOCK UPS AND UN-COMMANDED SUPERSEDED UGHT CHANGES (SUPERSEDED BY SL 737-SL-23-046 REV. A). SERVICE LETTER MOS SI. 737-SL-23-046 REV. A BOEING SKY INTERIOR ATTENDANT CONTROL PANEL SOFTWARE IMPROVEMENTS-LOCK UPS AND UN-COMMANDED RECOMMENDED UGHT CHANGES. SERVICE LETTER MOS 18-OCT-2011 SL 737-SL-23-047 INTERPHONE (INT) SYSTEM NOISE. SERVICE LETTER RECOMMENDED MOS I7-JUL-2013 SL 737-SL-23-048 POSSIBLE INCORRECT ORIENTATION OF GROUND CREW CALL HORN. SERVICE LETTER RECOMMENDED MOS 28-MAY-20I4 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 240 Of 748 @ Camp Systems EFTA00618531

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 SL 737-SL-24-111 REV. A MAIN WHEEL WELL JUNCTION BOX. SERVICE LETTER INFORMATIONAL 08-SEP-2000 MOS - (s) 51 737-SL-24-111 REV. B MAIN WHEEL WELL JUNCTION BOX WIRE CHAFING, SERVICE LETTER INFORMATIONAL I6-JAN-2001 MOS - (s) 51 737-SL-24-111 REV. C MAIN WHEEL WELL JUNCTION BOX WIRE CHAFING, SERVICE LETTER INFORMATIONAL 22-AUG-2001 MOS - (s) 51 737-SL-24-111 REV. D MAIN WHEEL WELL JUNCTION BOX WIRE CHAFING, SERVICE LETTER INFORMATIONAL 28-NOV-2001 MOS - (s) 51 737-SL-24-111 REV. E MAIN WHEEL WELL JUNCTION BOX WIRE CHAFING (SUPERSEDED BY SI. 737-SL-24-111 REV. F). SERVICE LETTER SUPERSEDED MOS SL 737-SL-24-111 REV. F MAIN WHEEL WELL JUNCTION BOX WIRE CHAFING. SERVICE LETTER MOS 21 -AUG-20I 2 RECOMMENDED SL 737-SL-24-125 CHECK SCREWS ATTACHING FEEDER TERMINALS TO RIGID BUS IN POWER DISTRIBUTION PANELS. SERVICE LETTER INFORMATIONAL MOS 05-NOV-1998 - (s) SL 737-SL-24-125 REV. A CHECK SCREWS ATTACHING FEEDER TERMINALS TO RIGID BUS IN POWER DISTRIBUTION PANELS. SERVICE LETTER INFORMATIONAL MOS C6-JAN-1999 - (s) SL 737-SL-24-133 FUELING VALVE WIRE CHAFING, SERVICE LETTER INFORMATIONAL MOS 23-FEB-1999 - (s) SL 737-SL-24-136 REV. A INSPECTION FOR WIRE CHAFING CONDITION IN P5 PANEL, SERVICE LETTER INFORMATIONAL MOS 30-AUG-1999 -(s) SL 737-SL-24-136 REV. B P-5 PANEL WIRE CHAFING INSPECTION/PROTECTION. SERVICE LETTER INFORMATIONAL MOS 17-NOV-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 241 Of 748 @ Camp Systems EFTA00618532

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 SL 737-SL-24-136 REV. C INSPECTION FOR WIRE CHAFING CONDITION IN PS PANEL. SERVICE LETTER INFORMATIONAL I9-JUN-2001 MOS - (s) 51 737-SL-24-137 WIRE BUNDLE RIDING FLAP CONTROL CABLE.. SERVICE LETTER INFORMATIONAL MOS 26-APR-1999 - (s) 51 737-SL-24-139 BATTERY CHARGER MODIFICATION. SERVICE LETTER INFORMATIONAL MOS 24-MAY-1999 - Is) SL 737-SL-24-140 SPARE CONNECTOR CAVITIES NOT SEALED. SERVICE LETTER INFORMATIONAL MOS Of -JUN-1999 - (s) SL 737-SL-24-141 POWER FEEDER WIRE BUNDLE CHAFED AGAINST FILTER ON ENGINE. SERVICE LETTER INFORMATIONAL MOS Of -JUN-1999 - SL 737-SL-24-141 REV. A POWER FEEDER WIRE BUNDLE CHAFED AGAINST FILTER ON ENGINE. SERVICE LETTER INFORMATIONAL MOS 20-OCT-1999 - (s) SL 737-SL-24-142 STANDOFF NOT INSTALLED IN MAIN WHEEL WELL. SERVICE LETTER INFORMATIONAL MOS II -JUN-1999 - (s) SL 737-SL-24-143 . SERVICE LETTER INFORMATIONAL MOS II -JUN-1999 - 51 737-SL-24-143 REV. A .SERVICE LETTER INFORMATIONAL MOS 03-SEP-1999 - 51 737-SL-24-143 REV. B WIRE BUNDLE RIDING IN LEFT WING STINT. SERVICE LETTER INFORMATIONAL MOS IO-DEC-1999 -(s) SL 737-SL-24-144 DUAL BATTERY AND STATIC INVERTER REMOTE CONTROLLED CIRCUIT BREAKER INSTALLATION ERRORS. SERVICE INFORMATIONAL LETTER MOS 29-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 242 Of 748 @ Camp Systems EFTA00618533

COMP Astant.fran Attn./whip' 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 SL 737-SL-24-145 WIRE BUNDLE RIDESACOUSTIC FIBER. SERVICE LETTER INFORMATIONAL 27-AUG-1999 MOS - (s) SL 737-SL-24-146 POWER DISTRIBUTION PANEL. P92. INSPECTION & MODIFICATION OF RIGID BUS ASSEMBLY. SERVICE LETTER INFORMATIONAL 07-SEP-1999 MOS - (s) SL 737-SL-24-146 REV. A POWER DISTRIBUTION PANEL. P92. INSPECTION & MODIFICATION OF RIGID BUS ASSEMBLY. SERVICE LETTER INFORMATIONAL 23-SEP-1999 MOS - (s) SI. 737-SL-24-147 BPCU MODIFICATION TO PREVENT POTENTIAL LOSS OF POWER TO A TRANSFER BUS WHEN CONNECTING GROUND INFORMATIONAL POWER. SERVICE LETTER MOS 23-SEP-1999 - (s) SI. 737-SL-24-147 REV. A BUS POWER CONTROL UNIT (3PCLI) MODIFICATION TO PREVENT POTENTIAL LOSS OF POWER TO A TRANSFER BUS INFORMATIONAL WHEN CONNECTING GROUND POWER. SERVICE LETTER MOS Of -JUL-2002 - (s) SL 737-SL-24-149 DUAL BATTERY ('API F LENGTH. SERVICE LETTER INFORMATIONAL MOS 08-OCT-1999 - (s) SL 737-SL-24-150 WIRE BUNDLES RIDING P15 REFUELING PANEL. SERVICE LETTER INFORMATIONAL MOS 08-OCT-1999 - (8) SL 737-SL-24-152 RIDING CONDITION OF THE COAXIAL CABLE ON THE KEEL BEAM STRUCTURE. SERVICE LETTER INFORMATIONAL MOS 15-NOV-1999 - (s) SL 737-SL-24-153 FUEL SHUTOFF VALVE WIRE CHAFING AGAINST THE RIGHT HYDRAULIC ACOUSTIC FILTER BRACKET BOLT IN THE INFORMATIONAL WHEEL WELL.. SERVICE LETTER MOS 16-NOV-1999 - (s) SL 737-SL-24-153 REV. A FUEL SHUTOFF VALVE WIRE CHAFING AGAINST THE RIGHT HYDRAULIC ACOUSTIC FILTER BRACKET BOLT IN THE INFORMATIONAL WHEEL WELL.. SERVICE LETTER MOS 29-JAN-2001 - (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 243 Of 748 @ Camp Systems EFTA00618534

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 SL 737-SL-24-154 REV. 8 BATTERY CHARGER INTERCHANGEABILITY. SERVICE LETTER INFORMATIONAL 09-SEP-2002 SL 737-SL-24-156 UNPROTECTED WIRE BUNDLES IN P88 P9 PANELS, SERVICE LETTER INFORMATIONAL MOS 13-DEC-1999 - (s) SL 737-SL-24-156 REV. A UNPROTECTED WIRE BUNDLES IN P88 P9 PANELS, SERVICE LETTER INFORMATIONAL MOS I7-APR-2000 MOS - (s) SL 737-SL-24-157 REV. A WIRE BUNDLES RIDING HYDRAULIC TUBE IN WHEEL WELL. SERVICE LETTER INFORMATIONAL MOS 13-OCT-2000 - (s) SL 737-SL-24-158 LANDING GEAR DOWN LOCK SENSOR- POTENTIAL WIRE CHAFING, SERVICE LETTER INFORMATIONAL 31 -JAN-2000 MOS - (s) SL 737-SL-24-162 POTENTIAL WIRE INTERFERENCE WITH HYDRAULIC LINE IN THE REFUELING PANEL. SERVICE LETTER INFORMATIONAL 31 -JUL-2000 MOS - (s) SL 737-SL-24-163 POTENTIAL WIRE RIDING CONDITION IN NOSE GEAR WHEEL WELL AREA, SERVICE LETTER INFORMATIONAL 14-AUG-2000 MOS - (s) SL 737-SL-24-164 EXTERNAL POWER RECEPTACLE - IMPROVED RETENTION. SERVICE LETTER INFORMATIONAL 31-OCT-2001 MOS -(s) SL 737-SL-24-165 STATIC INVERTER MODIFICATION. SERVICE LETTER INFORMATIONAL MOS 03-OCT-2000 - (s) SL 737-SL-24-165 REV. A STATIC INVERTER MODIFICATION TO REDUCE THE POTENTIAL FOR OVERHEATING. SERVICE LETTER INFORMATIONAL MOS 20-MAY-2003 SL 737-SL-24-165 REV. B STATIC INVERTER MODIFICATION TO REDUCE THE POTENTIAL FOR OVERHEATING (SUPERSEDED BY THE LATEST SUPERSEDED REVISION OF 737-SL-24-183). SERVICE LETTER MOS 03-APR-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 244 Of 748 @ Camp Systems EFTA00618535

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 SL 737-SL-24-167 STANDBY POWER CONTROL UNIT (SPCU) IMPROVEMENTS. SERVICE LETTER INFORMATIONAL 09-APR-2001 MOS - Is) SL 737-SL-24-168 GROUND SERVICE BUS 28VAC TRANSFORMER WIRES-POTENTAL CHAFING ON FRAME. SERVICE LETTER INFORMATIONAL MOS I4-MAY-2001 - (s) SL 737-SL-24-168 REV. A GROUND SERVICE BUS 28VAC TRANSFORMER WIRES- POTENTIAL CHAFING ON FRAME. SERVICE LETTER INFORMATIONAL MOS II -DEC-2001 - (s) SI. 737-SL-24-169 INTEGRATED DRIVE GENERATOR (IDG) RETENTION LANYARDS CHAFING (SUPERSEDED BY SL 737-SL-24-169 REV. A). SUPERSEDED SERVICE LETTER MOS - (s) SL 737-SL-24-169 REV. A INTEGRATED DRIVE GENERATOR (IDG) RETENTION LANYARDS CHAFING. SERVICE LETTER MOS SL 737-SL-24-170 24-SEP-2001 SL 737-SL-24-171 31-OCT-2001 WIRE BUNDLE RIDING AIRSTAIR RAIL. SERVICE LETTER MOS - Is) CORROSION PROTECTION OF ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL. (SUPERSEDED BY 737-SL-24-171 REV. A). SERVICE LETTER MOS - (s) SL 737-SL-24-171 REV. A CORROSION PROTECTION OF ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL (SUPERSEDED BY 737-SL-24-171 REV.B). SERVICE LETTER MOS 21-AUG-2003 - (s) SL 737-SL-24-171 REV. 8 CORROSION PROTECTION OF ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL. SERVICE LETTER MOS 24 (s) 24-JUN-2005 INFORMATIONAL SUPERSEDED SUPERSEDED SL 737-SL-24-175 INTERGRATED DRIVE GENERATOR-MAIN ROTOR. EXCITER ROTOR. CHARGE RELIEF VALVE. AND INPUT SHAFT SEAL INFORMATIONAL IMPROVEMENTS. SERVICE LETTER MOS 04-N0V-2002 - (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 245 Of 748 @ Camp Systems EFTA00618536

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 SL 737-SL-24-176 WINGTIP WIRING CHAFING-INSPECTION. SERVICE LETTER INFORMATIONAL 27-NOV-2002 SL 737-SL-24-176 REV. B WINGTIP WIRING CHAFING - INSPECTION. SERVICE LETTER INFORMATIONAL I 7-DEC-2003 SL 737-SL-24-177 BATTERY RESTORATION REQUIREMENTS. SERVICE LETTER INFORMATIONAL I3-MAY-2003 SL 737-SL-24-178 INSTALLATION MODIFICATION TO PREVENT LANYARD CHAFING. SERVICE LETTER INFORMATIONAL 07-JUL-2003 SL 737-SL-24-178 REV. A INTEGRATED DRIVE GENERATOR - INSTALLATION MODIFICATION TO PREVENT LANYARD CHAFING. SERVICE LETTER INFORMATIONAL MOS 22-JAN-2004 MOS MOS MOS MOS SL 737-SL-24-179 FLIGHT DECK P5 OVERHEAD RUBBER SWITCH TIP P/NS, SERVICE LETTER INFORMATIONAL MOS 08-AUG-2003 SL 737-SL-24-180 INTEGRATED DRIVE GENERATOR-MAIN STATOR SHORT CIRCUIT. SERVICE LETTER INFORMATIONAL MOS 24-OCT-2003 SL 737-SL-24-181 WIRE BUNDLE CHAFING AT STATION 671 AILERON CONTROL QUADRANT. SERVICE LETTER MOS 23-FEB-2004 SL 737-SL-24-181 REV. A WIRE BUNDLE CHAFING AT STATION 671 SPOILER CONTROL QUADRANT. SERVICE LETTER MOS I3-SEP-2004 SL 737-SL-24-182 STANDBY POWER CONTROL UNIT (SPCU) l(1 8 K8 RELAY IMPROVEMENTS. SERVICE LETTER MOS I2-JAN-2006 SL 737-SL-24-183 STATIC INVERTER MODIFICATION TO REDUCE THE POTENTIAL FOR OVERHEATING. SERVICE LETTER MOS 09-DEC-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 246 Of 748 @ Camp Systems EFTA00618537

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 SL 51 737-SL-24-183 REV. A 03-APR-2007 737-SL-24-184 09-FEB-2006 STATIC INVERTER MODIFICATION TO REDUCE THE POTENTIAL FOR OVERHEATING. SERVICE LETTER MOS STATIC INVERTER TRANSISTOR REPLACEMENT. SERVICE LETTER MOS 51 737-SL-24-185 UPGRADE OF MAIN WHEEL WELL ELECTRICAL CONNECTORS. SERVICE LETTER 51 27-MAR-2006 737-SL-24-185 REV. A MOS UPGRADE OF MAIN WHEEL WELL ELECTRICAL CONNECTORS. SERVICE LETTER 51 22-MAY-2006 737-SL-24-185 REV. B MOS UPGRADE OF MAIN WHEEL WELL ELECTRICAL CONNECTORS. SERVICE LETTER 51 I I -SEP-2006 737-SL-24-186 MOS LEACH TIME DELAY RELAY DISCLOSURE. SERVICE LETTER RECOMMENDED 51 09-MAR-2012 737-SL-24-187 MOS CIC NOT APPLIED TO CONNECTOR O46038P. SERVICE LETTER 51 09-JAN-2007 737-SL-24-188 MOS DRAIN MAST HEATER WIRE CHAFING. SERVICE LETTER 51 09-APR-2007 737-SL-24-188 REV. A MOS DRAIN MAST HEATER WIRE CHAFING. SERVICE LETTER COMPLIED WITH I8-MAY-2007 MOS 29-AUG-2011 3533:32 AFL 863 SL 737-SL-24-189 03-DEC-2007 51 737-SL-24-190 77-JAN-2008 INTEGRATED DRIVE GENERATOR - DIFFERENTIAL PRESSURE INDICATOR CHECK - ALTERNATE PROCEDURE. SERVICE LETTER MOS NON-CONFORMING KINGS COAX CONNECTORS. SERVICE LETTER 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 247 Of 748 @ Camp Systems EFTA00618538

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 SL 737-SL-24-190 REV. A NON-CONFORMING KINGS COAX CONNECTORS. SERVICE LETTER I 5-JUL -2008 SI. 737-SL-24-192 W10'22A/V1032 WIRE BUNDLE CHAFING NEAR FLAP TRACK BEAM. SERVICE LETTER 24-JAN-2008 MOS MOS SL 737-SL-24-192 REV. A W10'22AN1032 WIRE BUNDLE CHAFING NEAR FLAP TRACK BEAM. SERVICE LETTER MOS 12-MAY-2009 SL 737-SL-24-193 ELECTRICAL BRACKET ASSEMBLY INSTALLED INCORRECTLY. SERVICE LETTER MOS 28-JAN-2009 RECOMMENDED SL 737-SL-24-194 BACC6513L EXTERNAL POWER RECEPTACLE - CONTACTS SUPERSEDED BREAKING (SUPERSEDED BY SL 737-SL-24-194 REV. A). SERVICE LETTER MOS SL 737-SL-24-194 REV. A BACC8513L EXTERNAL POWER RECEPTACLE - CONTACTS BREAKING. SERVICE LETTER RECOMMENDED MOS I3-SEP-2011 SL 737-SL-24-195 CIRCUIT BREAKER TERMINAL SCREWS INSPECTION AND REPLACEMENT (SUPERSEDED BY 737-SL-24-195-A). SUPERSEDED SERVICE LETTER MOS I5-FEB-2010 SL 737-SL-24-195 REV. A CIRCUIT BREAKER TERMINAL SCREWS INSPECTION AND REPLACEMENT (SUPERSEDED BY SL 737-SL-24-195 REV. B), SUPERSEDED SERVICE LETTER MOS SL 737-SL-24-195 REV. B CIRCUIT BREAKER TERMINAL SCREWS INSPECTION AND REPLACEMENT. SERVICE LETTER MOS I5-JUL-2010 SL 737-SL-24-196 EXTERNAL POWER RECEPTACLE CRACKING (SUPERSEDED BY SL 737-SL-24-196 REV. A). SERVICE LETTER MOS SUPERSEDED 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 248 Of 748 @ Camp Systems EFTA00618539

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 SL 737-SL-24-196 REV. A EXTERNAL POWER RECEPTACLE CRACKING. SERVICE LETTER RECOMMENDED MOS OS-OCT-201 I SL 737-SL-24-197 ELECTRIC MOTOR DRIVEN HYDRAULIC CIRCUIT BREAKER TRIPPING (SUPERSEDED BY SL 737-SL-24-197 REV. A). SUPERSEDED SERVICE LETTER MOS SL 737-SL-24-197 REV. A ELECTRIC MOTOR DRIVEN HYDRAULIC CIRCUIT BREAKER TRIPPING. SERVICE LETTER RECOMMENDED MOS 20-MAR-2012 SI. 737-SL-24-198 POTENTIALLY INCORRECT CIRCUIT BREAKERS INSTALLED FOR STICK SHAKER AND MACH WARNING SYSTEM. RECOMMENDED SERVICE LETTER MOS 28-JAN-2011 SL 737-SL-24-200 FIRE PANEL WIRE INSTALLATION (SUPERSEDED BY SL 737-SL-24-200 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-24-200 REV. A FIRE PANEL WIRE INSTALLATION. SERVICE LETTER RECOMMENDED MOS I3-SEP-2011 SL 737-SL-24-201 POWER DISTRIBUTION PANEL - P91. UNUSED WIRE TERMINAL SLEEVES. SERVICE LETTER RECOMMENDED 08-DEC-2011 MOS SL 737-SL-24-202 GEN DRIVE STANDBY POWER TOGGLE SWITCH GUARD IS FOUND NOT FULLY ENGAGED TO AUTO POSITION. RECOMMENDED 28-MAR-2012 SERVICE LETTER MOS SL 737-SL-24-204 POSSIBLE MISLOCATED WIRE BUNDLE CLAMPS IN MAIN WHEEL WELL (SUPERSEDED BY SL 737-SL-24-204 REV. A). SUPERSEDED SERVICE LETTER MOS SI. 737-SL-24-204 REV. A POSSIBLE MISLOCATED WIRE BUNDLE CLAMPS IN MAIN WHEEL WELL (SUPERSEDED BY SL 737-SL-24-204 REV. B). SUPERSEDED SERVICE LETTER 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 249 Of 748 @ Camp Systems EFTA00618540

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 SL 737-SL-24-204 REV. 8 27-AUG-2013 POSSIBLE MISLOCATED WIRE BUNDLE CLAMPS IN MAIN WHEEL WELL. SERVICE LETTER MOS RECOMMENDED 51 737-SL-24-205 IDG LANYARD ADJUSTMENT TO PREVENT CHAFING ON IDG SERVICING ACCESS DOOR. SERVICE LETTER RECOMMENDED 16-NOV-2012 MOS 51 737-SL-24-206 STANDBY POWER CONTROL UNIT - K1 AND K8 RELAY IMPROVEMENT. SERVICE LETTER RECOMMENDED 26-JUN-2013 MOS SL 737-SL-24-207 ENVIRONMENTAL PROTECTION OF ELECTRICAL COMPONENTS IN WHEEL WELL AND WING. SERVICE LETTER RECOMMENDED 08-JUL-2013 MOS 51 737-SL-24-208 IDG BARE BORE BLOCKS. SERVICE LETTER RECOMMENDED 19-AUG-2013 MOS 51 737-SL-24-209 STATIC INVERTER INSTALLATION - TERMINAL TORQUE, SERVICE LETTER RECOMMENDED 17-MAR-2014 MOS 51 737-SL-25-051 REV. D LOWER CARGO COMPARTMENT LINER REPAIRS. SERVICE LETTER INFORMATIONAL 07-DEC-2001 MOS -(s) 51 737-SL-25-051 REV. E LOWER CARGO COMPARTMENT LINER REPAIRS. SERVICE LETTER INFORMATIONAL 51 28-MAR-2002 737-SL-25-051 REV. F MOS - (s) LOWER CARGO COMPARTMENT LINER REPAIRS. SERVICE LETTER 05-NOV-2004 MOS 51 737-SL-25-073 OVERHEAD STOWAGE BIN SYSTEM CONTENT RETENTION.. SERVICE LETTER INFORMATIONAL 12-MAR-1997 MOS -(s) 51 737-SL-25-073 REV. A OVERHEAD STOWAGE BIN SYSTEM CONTENT RETENTION.. SERVICE LETTER INFORMATIONAL 23-JUN-1997 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 250 Of 748 @ Camp Systems EFTA00618541

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 SL 737-SL-25-073 REV. 8 OVERHEAD STOWAGE BIN SYSTEM CONTENT RETENTION.. SERVICE LETTER INFORMATIONAL 26-MAR-1999 MOS - Is) SL 737-SL-25-076 INSTALLATION OF FELT TO PREVENT WATER DRIPPAGE INTO THE PASSENGER CABIN. SERVICE LETTER INFORMATIONAL MOS I6-JAN-I998 - (s) SL 737-SL-25-077 PREVENTING CONTAMINATION THAT AFFECTS FLAMMABILITY Of INSULATION BLANKETS. SERVICE LETTER INFORMATIONAL MOS 23-MAR-1998 SL 737-SL-25-078 REV. A RESCU 406 EMERGENCY LOCATOR TRANSMITTER (ELT) INSTALLATION. SERVICE LETTER MOS 03-JUN-2008 - (s) SL 737-SL-25-079 GALLEY OVEN MODIFICATION. SERVICE LETTER MOS I4-JUL-I998 - (4) SL 737-SL-25-082 EMI FILTER REPLACEMENT WE AEROSPACE AIR CHILLERS. SERVICE LETTER MOS 21-DEC-1998 - (4) SL 737-SL-25-082 REV. A EMI FILTER REPLACEMENT B/E AEROSPACE AIR CHILLERS. SERVICE LETTER MOS I8-JAN-1999 - (s) SL 737-SL-25-082 REV. B EMI FILTER REPLACEMENT WE AEROSPACE AIR CHILLERS. SERVICE LETTER MOS 06-AUG-1999 - (s) SL 737-SL-25-084 JAMCO GALLEY ELECTRICAL WIRE TERMINAL FASTENERS INSPECTION. SERVICE LETTER MOS 05-MAR-1999 - (s) SL 737-SL-25-085 IMPROVED OVERHEAD STOW BIN LATCH. SERVICE LETTER MOS 27-APR-1999 - (s) SL 737-SL-25-087 FLIGHT CREW SEAT ADJUSTMENT HANDLE. SERVICE LETTER MOS 14-JUL-I 999 - (s) INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL 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 251 Of 748 @ Camp Systems EFTA00618542

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 SL 737-SL-25-088 29-JUL-I999 LAV BI-FOLD DOOR IMPROVEMENTS TO EASE EMERGENCY REMOVAL. SERVICE LETTER MOS - Is) St 737-SL-25-089 AVIO INTERIORS PASSENGER SEAT TRAC REPLACEMENT. SERVICE LETTER 22-MAR-1999 MOS - Is) St 737-SL-25-089 REV. A AVIO INTERIORS PASSENGER SEAT TRAC REPLACEMENT. SERVICE LETTER 10-AUG-1999 MOS - Is) St 737-SL-25-092 REV. A OVERHEAD STOWAGE BIN DOOR STRIKE ASSEMBLY MODIFICATION. SERVICE LETTER I4-JUL-2000 - (s) MOS St 737-SL-25-093 REV. B LAVATORY DOOR LATCH IMPROVEMENTS. SERVICE LETTER MOS 28-AUG-2000 - (s) St 737-SL-25-094 REV. B CARGO NET USE - LOWER LOBE. SERVICE LETTER MOS 27-OCT-2006 St 737-SL-25-094 REV. C CARGO NET USE - LOWER LOBE. SERVICE LETTER MOS 24-JUL-2007 St 737-SL-25-096 LOWER CARGO COMPARTMENT LINER AND FLOOR PANEL REPLACEMENT.. SERVICE LETTER MOS 26-APR-2001 - (s) St 737-SL-25-096 REV. A LOWER CARGO COMPARTMENT LINER AND FLOOR PANEL REPLACEMENT.. SERVICE LETTER MOS C6-JUN-2001 - Is) SL 737-SL-25-096 REV. B LOWER CARGO COMPARTMENT LINER AND FLOOR PANEL REPLACEMENT (SUPERSEDED BY SL 737-SL-25-096 REV. C), SERVICE LETTER MOS SL 737-SL-25-096 REV. C LOWER LOBE CARGO COMPARTMENT LINER AND FLOOR PANEL REPLACEMENT. SERVICE LETTER MOS 10-MAR-201 I INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL SUPERSEDED 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 252 Of 748 @ Camp Systems EFTA00618543

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 SL 737-SL-25-097 22-AUG-2001 SL 737-SL-25-098 27-JUL-2001 St 737-SL-25-099 REMOVAL OF FUSELAGE CARGO COMPARTMENT INSULATION BLANKETS. SERVICE LETTER MOS - Is) FLIGHT DECK SUITCASE RESTRAINT STRAP CLIP INSTALLATION. SERVICE LETTER INFORMATIONAL INFORMATIONAL MOS - FLIGHT DECK NO.2 SLIDING WINDOW UNING ASSEMBLY INTERFERENCE WITH CIRCUIT BREAKER PANEL. SERVICE INFORMATIONAL LETTER MOS 24-AUG-2001 - (s) SL 737-SL-25-100 24-SEP-2001 SL 737-SL-25-100 REV. A FORWARD CARGO LOADINGAJNLOADING PERCAUTIONS. SERVICE LETTER I3-OCT-2003 SL 737-SL-25-100 REV. B FORWARD CARGO LOADINGAJNLOADING PRECAUTIONS. SERVICE LETTER I7-OCT-2003 SL 737-SL-25-100 REV. 0 CARGO LOADING/UNLOADING PRECAUTIONS. SERVICE LETTER 25-SEP-2007 SL 737-SL-25-101 24-SEP-2001 - (s) SL 737-SL-25-103 03-JUN-2002 - SL 737-SL-25-104 29-MAY-2002 SL 737-SL-25-104 REV. A ATTENDANT SEAT MOUNTING BOLT MATERIAL. SERVICE LETTER MOS Of -JUL-2002 - FORWARD CARGO LOADINGAJNLOADING PRECAUTIONS. SERVICE LETTER INFORMATIONAL MOS INFORMATIONAL - Is) MOS MOS MOS ESCAPE ROPE "SHELLING'. SERVICE LETTER MOS SLIDING CARPET LOADING SYSTEM (SCLS) RAMP SEALING. SERVICE LETTER MOS ATTENDANT SEAT MOUNTING BOLT MATERIAL. SERVICE LETTER MOS - INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL 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 253 Of 748 @ Camp Systems EFTA00618544

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 SL 737-SL-25-106 OUTBOARD GLARESHIELD LIGHTSHADE ASSEMBLY BREAKAGE.. SERVICE LETTER INFORMATIONAL MOS 03-OCT-2002 - Is) SL 737-SL-25-107 CLOSE OUT SEAL RETAINER. SERVICE LETTER INFORMATIONAL MOS I0-SEP-2002 SL 737-SL-25-107 REV. A CLOSE OUT SEAL RETAINER REPLACEMENT ON INTERIOR MONUMENTS. SERVICE LETTER INFORMATIONAL MOS 21-OCT-2002 SL 737-SL-25-108 CLOSE OUT SEAL REPLACEMENT BETWEEN OVERHEAD STOWAGE BIN AND FULL HEIGHT MONUMENTS. SERVICE INFORMATIONAL LETTER MOS I7-DEC-2002 SL 737-SL-25-108 REV. A CLOSE OUT SEAL REPLACEMENT BETWEEN OVERHEAD STOWAGE BIN AND FULL HEIGHT MONUMENTS. SERVICE INFORMATIONAL LETTER MOS 08-APR-2003 SL 737-SL-25-109 CABIN SIDEWALL AIR RETURN GRILLE INSTALLATION. SERVICE LETTER INFORMATIONAL MOS I5-MAY-2003 SL 737-SL-25-109 REV. A CABIN SIDEWALL AIR RETURN GRILLE INSTALLATION, SERVICE LETTER INFORMATIONAL MOS 02-JUL-2003 SL 737-SL-25-111 FLIGHT DECK DRIP-SHIELD DRAIN TUBE INTERFERENCE WITH THE NUMBER 2 WINDOW. SERVICE LETTER INFORMATIONAL MOS 27-OCT-2003 SL 737-SL-25-111 REV. A FLIGHT DECK DRIP-SHIELD DRAIN TUBE INTERFERENCE WITH THE NUMBER 2 WINDOW. SERVICE LETTER MOS 0I-FEB-2008 SL 737-SL-25-112 AFT CARGO COMPARTMENT BLOWOUT PANEL REPLACEMENT. SERVICE LETTER INFORMATIONAL MOS 30-MAR-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 254 Of 748 @ Camp Systems EFTA00618545

flP Megnand 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 SL 737-SL-25-114 REV. A ATTENDANT SEAT RUBSTRIPS. SERVICE LETTER INFORMATIONAL 51 31-MAR-2004 737-SL-25-115 REV. 8 MOS CARGO COMPARTMENT LINER TAPE AND FASTENERS. SERVICE LETTER 51 -JUL-2007 737-SL-25-116 REV. A MOS CLOSE OUT SEAL REPLACEMENT BETWEEN OVERHEAD STOWAGE BINS. SERVICE LETTER 51 76-DEC-2005 737-SL-25-116 REV. 8 MOS CLOSE OUT SEAL REPLACEMENT BETWEEN OVERHEAD STOWAGE BINS. SERVICE LETTER 51 30-MAR-2006 737-SL-25-117 REV. A MOS FORWARD CARGO CEILING PANEL PERMANENT REPAIR OPTIONS. SERVICE LETTER 51 04-JAN-2005 737-SL-25-118 MOS AVAILABILITY OF IMPROVED OXYGEN GENERATOR RELEASE PIN. SERVICE LETTER INFORMATIONAL 30-NOV-2004 MOS 51 737-SL-25-119 REV. A OVERHEAD STOWAGE BIN LATCH BEZEL CRACKING. SERVICE LETTER INFORMATIONAL NOT APPLICABLE - - 51 23-MAR-2005 737-SL-25-120 MOS IMPROVED CROWN INSULATION BLANKETS AT ANTENNAJLIGHT PENETRATIONS. SERVICE LETTER 51 29-MAR-2005 737-SL-25-120 REV. B MOS IMPROVED CROWN INSULATION BLANKETS AT ANTENNAJLIGHT PENETRATIONS. SERVICE LETTER 51 07-DEC-2005 737-SL-25-121 MOS OUST CONTAMINATION - LRU CLEANING PROCEDURES. SERVICE LETTER 51 72-JUL-2005 737-SL-25-122 MOS ATTENDANT SEAT FASTENERS. SERVICE LETTER NOT APPLICABLE 23-AUG-2005 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 255 Of 748 @Camp Systems EFTA00618546

1y taM1pM„ Megnand 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 SL 737-SL-25-123 REV. B AIR STAIRS HANDRAIL FITTING ATTACHMENT TO YRC FWD LAVATORY. SERVICE LETTER MOS 24 (s) 13-DEC-2005 SL 737-SL-25-124 NEW FLAMMABILITY REQUIREMENT FOR THERMAUACOUS11C INSULATION MATERIALS. SERVICE LETTER MOS 06-JAN-2006 SL 737-SL-25-124 REV. A NEW FLAMMABILITY REQUIREMENT FOR THERMAUACOUSTIC INSULATION MATERIALS. SERVICE LETTER MOS I3-APR-2006 SL 737-SL-25-125 GALLEY AIR CHILLER RELIABILITY IMPROVEMENTS, SERVICE LETTER MOS 28-APR-2006 SL 737-SL-25-125 REV. A GALLEY AIR CHILLER RELIABILITY IMPROVEMENTS, SERVICE LETTER MOS 30-AUG-2006 SL 737-SL-25-126 IMPROVING GALLEY REFRIGERATION PERFORMANCE AND RELIABILITY BEST PRACTICES. SERVICE LETTER MOS 15-MAR-2007 SL 737-SL-25-127 OVERHEAD STOWAGE BIN DOOR IMPROVEMENTS, SERVICE LETTER MOS Of-OCT-2007 SL 737-SL-25-128 CARGO COMPARTMENT BILGE TFUM, - FUSELAGE SKIN DAMAGE. SERVICE LETTER MOS 27-MAR-2008 SL 737-SL-25-130 CLOSE OUT SEAL REPLACEMENT BETWEEN OVERHEAD STOWAGE AND FULL HEIGHT MONUMENTS. SERVICE LETTER MOS 08-DEC-2008 SL 737-SL-25-130 REV. A CLOSE OUT SEAL REPLACEMENT BETWEEN OVERHEAD RECOMMENDED STOWAGE AND FULL HEIGHT MONUMENTS. SERVICE LETTER MOS 27-FEB-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 256 Of 748 @Camp Systems EFTA00618547

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 SL 737-SL-25-131 POSSIBLE DAMAGE TO E4-1 RACK SHROUD DRAIN TUBE. SERVICE LETTER MOS 24-OCT-2008 SL 737-SL-25-132 GALLEY OVEN MODIFICATION. SERVICE LETTER MOS I9-DEC-2008 SL 737-SL-25-132 REV. A GALLEY OVEN MODIFICATION. SERVICE LETTER MOS I7-FEB-2009 SI. 737-SL-25-133 IMPROVED OXYGEN GENERATOR FITTING FOR 417N3011- SERIES PASSENGER SERVICE UNITS (SUPERSEDED BY SL 737-SL-25-133 REV. A). SERVICE LETTER MOS SUPERSEDED SL 737-SL-25-133 REV. A IMPROVED OXYGEN GENERATOR FITTING FOR 417N3011-SERIES PASSENGER SERVICE UNITS. SERVICE LETTER RECOMMENDED MOS I0-SEP-2010 SL 737-SL-25-134 GOODRICH 2110-SERIES FLIGHT ATTENDANT SEATBACK CRACKING. SERVICE LETTER 21-AUG-2009 SL 737-SL-25-135 31-AUG-2009 MOS INSULATION BLANKET REPAIR PROCEDURES - NEW THERMAL-ACOUSTIC INSULATION BLANKETS FOR FUSELAGE BURNTHROUGH STANDARDS. SERVICE LETTER MOS SL 737-SL-25-135 REV. A INSULATION BLANKET REPAIR PROCEDURES -NEW THERMAL-ACOUSTIC INSULATION BLANKETS FOR FUSELAGE BURNTHROUGH STANDARDS. SERVICE LETTER MOS 06-OCT-2009 RECOMMENDED RECOMMENDED SL 737-SL-25-136 SELL OVEN INTERCHANGEABILITY. SERVICE LETTER RECOMMENDED MOS 23-SEP-2009 SL 737-SL-25-137 FLIGHT DECK SIDE GRILLE MODIFICATION. SERVICE LETTER RECOMMENDED MOS 23-SEP-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 257 Of 748 @ Camp Systems EFTA00618548

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 SL 737-SL-25-137 REV. A 29-SEP-2009 SL 737-SL-25-138 19-OCT-2009 FLIGHT DECK SIDE GRILLE MODIFICATION. SERVICE LETTER MOS RESTRAINT SYSTEM WITH INERTIA REEL - MANUAL LOCK MAY BE INOPERABLE. SERVICE LETTER MOS SL 737-SL-25-138 REV. A RESTRAINT SYSTEM WITH INERTIA REEL - MANUAL LOCK MAY BE INOPERABLE. SERVICE LETTER MOS I I -NOV-2009 SL 737-SL-25-139 27-OCT-2009 SL 737-SL-25-140 23-DEC-2009 SL 737-SL-25-141 30-JUL-2010 SL 737-SL-25-142 SL 737-SL-25-142 REV. A 22-DEC-2010 SL 737-SL-25-143 23-DEC-2010 SL 737-SL-25-144 03-DEC-2010 RECOMMENDED RECOMMENDED RECOMMENDED DRIESSEN 61 GALLEY SHROUD COVER MODIFICATION. SERVICE LETTER RECOMMENDED MOS RESCU 406(5) ELT ANTENNA RADIATION ISSUE. SERVICE LETTER INFORMATIONAL MOS FOLD DOWN TABLE ASSEMBLY MECHANICAL LINKAGE. SERVICE LETTER RECOMMENDED MOS 737NG ESCAPE SLIDE VALISE RELEASE CABLE AND ASPIRATOR (SUPERSEDED BY SL 737-SL-25-142 REV. A). SUPERSEDED SERVICE LETTER MOS 737NG ESCAPE SLIDE VALISE RELEASE CABLE AND ASPIRATOR. SERVICE LETTER RECOMMENDED MOS LRU EQUIPMENT DECALS SWAPPED ON E1-5 SHELF FOR VHF NO.2 TRANSCEIVER AND DME NO.2 INTERROGATOR. RECOMMENDED SERVICE LETTER MOS ATTENDANT SERVICE UNIT - OXYGEN DOOR PANEL ASSEMBLY DESIGN IMPROVEMENT. SERVICE LETTER RECOMMENDED 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 258 Of 748 @ Camp Systems EFTA00618549

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 SL 737-SL-25-145 737 BSI OVERHEAD STOWAGE BIN BUCKET LATCH END ASSEMBLY FASTENERS. SERVICE LETTER RECOMMENDED MOS 12-MAY-2011 SL 737-SL-25-146 RETENTION OF OXYGEN DOOR LATCH ACTUATOR FOR 417N3011-SERIES PASSENGER SERVICE UNITS. SERVICE RECOMMENDED LETTER MOS 08-FEB-2012 SL 737-SL-25-148 EUROPEAN UNION (EU) RESTRICTION ON IMPORT OF CADMIUM IN PLASTICS. SERVICE LETTER RECOMMENDED MOS 19-DEC-2011 SL 737-SL-25-149 BSI PIVOT STOWAGE BIN TORQUE TUBE COVER FASTENERS (SUPERSEDED BY SL 5L737-SL-25-149 REV. A). SERVICE SUPERSEDED LETTER MOS SI. 737-SL-25-149 REV. A BSI PIVOT STOWAGE BIN TORQUE TUBE COVER FASTENERS (SUPERSEDED BY SL 737-SL-25-149 REV. B). SERVICE RECOMMENDED LETTER MOS 18-DEC-2012 SL 737-SL-25-149 REV. B BSI PIVOT STOWAGE BIN TORQUE TUBE COVER FASTENERS. SERVICE LETTER RECOMMENDED MOS 28-MAR-2013 SL 737-SL-25-150 HORIZONTAL BATWING TRIM DIS-BONDING BSI STOW BINS. SERVICE LETTER RECOMMENDED MOS 06-AUG-2012 SL 737-SL-25-152 FLIGHT DECK DRIP-SHIELD DRAIN TUBE INSTALLATION. SERVICE LETTER RECOMMENDED MOS 12-MAR-2013 SL 737-SL-25-153 BOEING SKY INTERIOR (BSI) - SEAT ROW MARKER (SUPERSEDED BY SL 737-SL-25-153 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-25-153 REV. A BOEING SKY INTERIOR (BSI) - SEAT ROW MARKER. SERVICE LETTER RECOMMENDED MOS 22-MAY-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 259 Of 748 @ Camp Systems EFTA00618550

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 SL 737-SL-25-155 06-JUN-2013 SL 737-SL-25-156 YRC (YOKOHAMA RUBBER COMPANY) TOILET DOOR HANDLE MISSING LOCTITE. SERVICE LETTER MOS RECOMMENDED 2ND OBSERVERS SEAT: REPLACEMENT OF THE FWD ATTACH BOLTS AND THE ATTACHMENT SCREWS IN THE FLT SUPERSEDED DECK CLOSET (SUPERSEDED BY 737-SL-25-156 REV. A). SERVICE LETTER MOS SL 737-SL-25-156 REV. A 2ND OBSERVERS SEAT: REPLACEMENT OF THE FWD ATTACH BOLTS AND THE ATTACHMENT SCREWS IN THE FLT RECOMMENDED DECK CLOSET. SERVICE LETTER MOS 30-JAN-2014 SL 737-SL-25-157 CONNECTOR BACKSHELL POTENTIALLY RIDING BSI CEILING PANEL. SERVICE LETTER RECOMMENDED 81OS 02-JUN-2014 - (s) SL 737-SL-25-159 INTRODUCTION OF IMPROVED SIDEWALL WINDOW SHADES (SUPERSEDED BY SL 737-SL-25-159 REV. A). SERVICE SUPERSEDED LETTER 81OS SL 737-SL-25-159 REV. A INTRODUCTION OF IMPROVED SIDEWALL WINDOW SHADES. SERVICE LETTER RECOMMENDED MOS 16-MAY-2014 SL 737-SL-25-160 BOEING SKY INTERIOR (BSI) - PASSENGER WINDOW REVEAL SHARP EDGE. SERVICE LETTER RECOMMENDED MOS 03-MAR-2014 SL 737-SL-26-037 FORWARD ATTENDANT PANEL - LAVATORY SMOKE DETECTOR MODULE IMPROVEMENTS. SERVICE LETTER INFORMATIONAL MOS 09-AUG-2000 - (s) SL 737-SL-26-037 REV. A FORWARD ATTENDANT PANEL- LAVATORY SMOKE DETECTOR MODULE IMPROVEMENTS. SERVICE LETTER RECOMMENDED MOS 07-DEC-2000 - (s) SL 737-SL-26-038 CFM56-78 FIRE DETECTION HARNESS IMPROVEMENT. SERVICE LETTER RECOMMENDED MOS 14-MAR-2001 - (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 260 Of 748 @ Camp Systems EFTA00618551

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 SL 737-SL-26-040 22-APR-2002 PORTABLE WATER FIRE EXTINGUISHERS. SERVICE LETTER MOS - Is) INFORMATIONAL SL 737-SL-26-042 PORTABLE WATER FIRE EXTINGUISHERS MISSING PIERCER. SERVICE LETTER INFORMATIONAL MOS 13-JUN-2002 - (s) SL 737-SL-26-043 RECALL OF KIDDE AEROSPACE PORTABLE HALON 1211 FIRE EXTINGUISHERS-P/N 898052. SERVICE LETTER INFORMATIONAL COMPUED WITH MOS 15-FEB-2004 05-NOV-2002 -Is) 1579:18 AFL 398 SL 737-SL-26-044 INCORRECT INSTALLATION OF ENGINE FIRE EXTINGUISHING HOSE MAY PREVENT AGENT FLOW TO ENGINE. INFORMATIONAL COMPUED WITH SERVICE LETTER MOS 15-FEB-2004 17-DEC-2003 1579:18 AFL 398 SL 737-SL-26-045 CARGO COMPARTMENT FIRE SUPPRESSION BOTTLE REQUIREMENTS. SERVICE LETTER INFORMATIONAL MOS 18-AUG-2004 SL 737-SL-26-046 LAVATORY FIRE EXTINGUISHER EXTINGUISHING AGENT REPLACEMENT. SERVICE LETTER MOS 20-SEP-2006 SL 737-SL-26-046 REV. A LAVATORY FIRE EXTINGUISHER EXTINGUISHING AGENT REPLACEMENT. SERVICE LETTER MOS 27-FEB-2007 SL 737-SL-26-047 ENGINE FIRE LIGHT ILLUMINATION. SERVICE LETTER MOS 27-NOV-2006 SL 737-SL-26-048 CARGO FIRE EXTINGUISHER -METERING ASSEMBLY/DRIER DISC RUPTURE. SERVICE LETTER 09-NOV-2007 SL 737-SL-26-049 14-NOV-2007 MOS IMPROPERLY TORQUED APU LOWER FIRE DETECTOR SENSOR, SERVICE LETTER 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 261 Of 748 @ Camp Systems EFTA00618552

CAMP Asiant.fran Atna: 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 SL 737-SL-26-049 REV. A IMPROPERLY TORQUED APU LOWER FIRE DETECTOR SENSOR. SERVICE LETTER 51 24-JAN-2008 737-SL-26-050 MOS CARD CONTAMINATION IN FIRE DETECTION MODULES. SERVICE LETTER 03-DEC-2008 MOS 51 737-SL-26-051 CONTAMINATED HALON 1211 FIRE EXTINGUISHERS. SERVICE LETTER INFORMATIONAL 23-DEC-2009 MOS 51 737-SL-26-051 REV. A CONTAMINATED HALON 1211 FIRE EXTINGUISHERS. SERVICE LETTER INFORMATIONAL 08-FEB-2010 MOS 51 737-SL-26-052 WASHERS ON APU FIRE DETECTOR CLAMPS INADVERTENTLY OMITTED (SUPERSEDED BY SL SL 737-SL-26-052 REV. SUPERSEDED A). SERVICE LETTER MOS 51 737-SL-26-052 REV. A WASHERS ON APU FIRE DETECTOR CLAMPS INADVERTENTLY OMITTED. SERVICE LETTER RECOMMENDED 10-JAN-2011 MOS 51 737-SL-26-054 POSSIBLE OVERHEAT SENSOR BRACKET DISCREPANCY. SERVICE LETTER RECOMMENDED 14-MAY-2012 MOS 51 737-SL-26-055 WING(BODY OVERHEAT FAULTS DUE TO FENWAL CONNECTORS. SERVICE LETTER RECOMMENDED I9-JUN-2012 MOS 51 737-SL-26-056 APU FIRE DETECTOR PART MARK INCORRECT. SERVICE LETTER RECOMMENDED 23-MAY-20I3 MOS 51 737-SL-27-079 REV. A MACH TRIM FLAPS UP. AND LANDING WARNING SWITCH IMPROVEMENT. SERVICE LETTER INFORMATIONAL 51 10-APR-2003 737-SL-27-079 REV. F MOS NEW S138 LAND WARNING. S245 FLAP POSITION. S290 MACH TRIM WARNING. AND S1051 FLAPS UP SWITCHES. 08-FEB-2005 SERVICE LETTER 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 262 Of 748 @ Camp Systems EFTA00618553

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 SL 737-SL-27-124 STALL MANAGEMENT/ YAW DAMPER MODULE ASSY MODIFICATION. SERVICE LETTER INFORMATIONAL MOS 23-FEB-1999 - Is) SL 737-SL-27-126 REV. A PERIODIC OPERATIONAL VERIFICATION OF THE ELEVATOR TAB CONTROL SYSTEM. SERVICE LETTER RECOMMENDED I3-NOV-2000 MOS - (s) SL 737-SL-27-130 REV. A STABILIZER TRIM ACTUATOR CMR RETROFIT PROCEDURE. SERVICE LETTER INFORMATIONAL MOS 06-AUG-1999 - Is) SL 737-SL-27-131 ELEVATOR TAB ROD HI-LOK INTERFERENCE WITH STRUCTURE. SERVICE LETTER INFORMATIONAL I8-DEC-1998 MOS - SL 737-SL-27-131 REV. A ELEVATOR TAB ROD HI-LOK INTERFERENCE WITH STRUCTURE. SERVICE LETTER INFORMATIONAL MOS I 7-JUN-1999 - 51 737-SL-27-132 INSPECTION OF FLEXIBLE HOSES BETWEEN ELEVATOR FEEL PITOT PROBES AND RIGID METAL TUBING. SERVICE INFORMATIONAL LETTER MOS I8-DEC-1998 - (s) SL 737-SL-27-133 ELEVATOR TAB CONTROL ROD NUT REPLACEMENT. SERVICE LETTER INFORMATIONAL MOS I8-JAN-1999 - (s) SL 737-SL-27-134 REV. A TRAILING EDGE FLAP ALTERNATE DRIVE MOTOR DESIGN IMPROVEMENTS. SERVICE LETTER MOS 27-MAR-2007 SL 737-SL-27-136 ELEVATOR CONTROL CABLE CLEARANCE INSPECTION. SERVICE LETTER INFORMATIONAL MOS 31-MAR-1999 - (s) SL 737-SL-27-137 REV. B ELEVATOR TAB PIVOT BOLT WASHER OMISSION. SERVICE LETTER INFORMATIONAL MOS 03-NOV-2000 - (s) SL 737-SL-27-138 AILERON TAB CONTROL ROD CONNECTING BARREL. SERVICE LETTER INFORMATIONAL MOS 31-MAR-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 263 Of 748 @ Camp Systems EFTA00618554

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: O5-Aug-2O14 Task No. Description Unit Interval Compliance Next Due Disposition MOC SL 737-SL-27-139 ELEVATOR CONTROLS-FORWARD QUADRANT INTERFERENCE. SERVICE LETTER MOS I6-APR-1999 - Is) SL 737-SL-27-140 FLIGHT CONTROLS-ELEVATOR BUSS INSTALLATION-RIVET INTERFERENCE. SERVICE LETTER MOS 13-SEP-1999 23-APR-1999 - SL 737-SL-27-140 REV. A FLIGHT CONTROLS-ELEVATOR BUSS INSTALLATION-RIVET INTERFERENCE. SERVICE LETTER MOS I7-MAY-1999 - (s) SL 737-SL-27-140 REV. B FLIGHT CONTROLS-ELEVATOR BUSS INSTALLATION-RIVET INTERFERENCE. SERVICE LETTER MOS I6-JUN-1999 - SL 737-SL-27-141 AILERON WING CONTROL CABLE ROUTING INSPECTION. SERVICE LETTER MOS 18 (s) 13-SEP-1999 I3-JUL-I 999 AFL 4000 SL 737-SL-27-142 ELEVATOR FEEL COMPUTER DISCREPANT O RINGS, SERVICE LETTER MOS 14-JUL-I 999 - (s) SL 737-SL-27-143 AILERON SPRING CARTRIDGE BOLTINTERFERENCE. SERVICE LETTER MOS 07-SEP-1999 - (s) SL 737-SL-27-147 REV. A RUDDER CONTROL AFT QUADRANT ATTACHMENT FASTENERS UNDERTOROUED.. SERVICE LETTER MOS 08-DEC-1999 - (s) SL 737-SL-27-148 INABILITY TO MOVE WING LEADING EDGE DEVICE. SERVICE LETTER MOS 21-DEC-1999 - (s) SL 737-SL-27-148 REV. A INABILITY TO MOVE WING LEADING EDGE DEVICES, SERVICE LETTER MOS 01-MAR-2005 SL 737-SL-27-149 RUDDER CONTROL AFT QUADRANT ATTACHMENT FASTENERS UNDERTOROUED.. SERVICE LETTER MOS 11 -JUN-2000 - INFORMATIONAL INFORMATIONAL COMPLIED WITH - CM INFORMATIONAL INFORMATIONAL INFORMATIONAL COMPLIED WITH - CM RECOMMENDED RECOMMENDED RECOMMENDED RECOMMENDED INFORMATIONAL 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 264 Of 748 @ Camp Systems EFTA00618555

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 SL 737-SL-27-149 REV. A CONTROLS-AILERON CABLE PULLEY INSTALLATION-INTERFERNCE. SERVICE LETTER 21-FEB-2000 MOS - Is) St 737-SL-27-150 ELEVATOR POWER CONTROL UNIT LINKAGE INSPECTION, SERVICE LETTER MOS I 7-APR-2000 I4-FEB-2000 - (s) St 737-SL-27-150 REV. A ELEVATOR POWER CONTROL UNIT LINKAGE INSPECTION. SERVICE LETTER MOS I4-FEB-2001 - (s) St 737-SL-27-150 REV. B ELEVATOR POWER CONTROL UNIT LINKAGE- INSPECTION.. SERVICE LETTER MOS I2-MAY-2000 -(s) St 737-SL-27-152 STABILIZER TRIM MOTOR IMPROVEMENTS. SERVICE LETTER MOS 27-JUL-2000 - St 737-SL-27-153 TRAILING EDGE FLAP TORQUE TUBE COUPLING AND U-JOINT LUBRICATION. SERVICE LETTER MOS 03-OCT-2000 - (s) St 737-SL-27-154 REPLACEMENT OF ELEVATOR OUTPUT TORQUE TUBE CONTROL CRANK BEARING. SERVICE LETTER MOS I3-OCT-2000 - (s) St 737-SL-27-154 REV. A REPLACEMENT OF ELEVATOR OUTPUT TORQUE TUBE CONTROL CRANK BEARING. SERVICE LETTER MOS I 7-NOV-2000 - (s) St 737-SL-27-154 REV. B REPLACEMENT OF ELEVATOR OUTPUT TORQUE TUBE CONTROL CRANK BEARING. SERVICE LETTER MOS I8-APR-2001 - (s) St 737-SL-27-154 REV. C REPLACEMENT OF ELEVATOR OUTPUT TORQUE TUBE CONTROL CRANK BEARING, SERVICE LETTER MOS 27-APR-2001 - Is) St 737-SL-27-154 REV. D ELEVATOR CONTROL SYSTEM - ELEVATOR OUTPUT TORQUE TUBE CONTROL CRANK BEARING. SERVICE LETTER MOS I6-NOV-2001 - (s) RECOMMENDED RECOMMENDED COMPUED WITH - CM INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL 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 265 Of 748 @ Camp Systems EFTA00618556

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 SL 737-SL-27-154 REV. E ELEVATOR CONTROL SYSTEM - ELEVATOR OUTPUT TOROUE TUBE CONTROL CRANK BEARING. SERVICE LETTER MOS I5-OCT-2007 SL 737-SL-27-154 REV. F ELEVATOR CONTROL SYSTEM - ELEVATOR OUTPUT TORQUE TUBE CONTROL CRANK BEARING. SERVICE LETTER MOS 27-OCT-2009 RECOMMENDED SL 737-SL-27-154 REV. G ELEVATOR CONTROL SYSTEM- ELEVATOR OUTPUT TORQUE SUPERSEDED TUBE CONTROL CRANK BEARING (SUPERSEDED BY SL 737-SL-27-154 REV. H). SERVICE LETTER MOS SL 737-SL-27-154 REV. H ELEVATOR CONTROL SYSTEM - ELEVATOR OUTPUT TORQUE TUBE CONTROL CRANK BEARING, SERVICE LETTER RECOMMENDED MOS I3-JUL-2011 SL 737-SL-27-155 ELEVATOR TAB SOLENOID VALVE REPLACEMENT. SERVICE LETTER INFORMATIONAL MOS I 7-NOV-2000 - (s) SL 737-SL-27-155 REV. A ELEVATOR TAB SOLENOID VALVE REPLACEMENT. SERVICE LETTER INFORMATIONAL MOS I3-APR-2001 - (s) SI. 737-SL-27-156 STABILIZER TRIM CABLE GUARD INTERFERENCE WITH AUTOTHROTTLE MECHANISMMOUNTING FLANGE. SERVICE INFORMATIONAL LETTER MOS 79-DEC-2000 - (s) SL 737-SL-27-159 STANDBY RUDDER PCU REACTION BEARING INCORRECTLY SWAGED. SERVICE LETTER INFORMATIONAL MOS I6-JAN-2001 - (s) SL 737-SL-27-160 AILERON POWER CONTROL SUPPORT ARM INTERFERENCE WITH HYDRAULIC HOSE. SERVICE LETTER INFORMATIONAL MOS 07-MAY-2001 - (s) SL 737-SL-27-162 STALL MANAGEMENT/YAW DAMPER MODULE ASSEMBLY MODIFICATION. M01747 NO.1. 1,401748 NO.2. P/N 285A1010. INFORMATIONAL SERVICE LETTER MOS I9-OCT-2001 -(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 266 Of 748 @ Camp Systems EFTA00618557

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 SL 737-SL-27-162 REV. A STALL MANAGEMENT/ YAW DAMPER MODULE ASSEMBLY MODIFICATION. M01747 NO.1. M01748 NO.2. PIN 285A1010. INFORMATIONAL SERVICE LETTER MOS 12-APR-2002 - Is) SL 737-SL-27-162 REV. B STALL MANAGEMENT/YAW DAMPER MODULE ASSEMBLY MODIFICATION. M01747 NO.1. M01748 NO.2. PIN 285A1010. INACTIVE SERVICE LETTER 08-MAR-2004 MOS SL 737-SL-27-164 INSPECTION FOR BENT CLEVIS ON ELEVATOR FEEL AND CENTERING BRACKET SUPPORT. SERVICE LETTER INFORMATIONAL MOS 02-MAY-2002 - (s) SL 737-SL-27-164 REV. A INSPECTION FOR BENT CLEVIS ON ELEVATOR FEEL AND CENTERING BRACKET SUPPORT. SERVICE LETTER INFORMATIONAL MOS 16-DEC-2004 SL 737-SL-27-165 P2-3 LANDING GEAR PANEL ASSEMBLIES - DISCREPANT FLAP PLACARD SPEEDS. SERVICE LETTER INFORMATIONAL MOS I2-APR-2002 - (s) SL 737-SL-27-167 CONTROL COLUMN NEEDLE BEARING CORROSION. SERVICE LETTER INFORMATIONAL MOS I I -DEC-2002 SL 737-SL-27-169 LUBRICATION OMITTED FROM THE ROD END ASSEMBLY FOR THE FLIGHT SPOILER ACTUATOR. SERVICE LETTER INFORMATIONAL MOS I I -DEC-2002 SL 737-SL-27-169 REV. A LUBRICATION OMITTED FROM THE ROD END ASSEMBLY FOR THE FLIGHT SPOILER ACTUATOR. SERVICE LETTER INFORMATIONAL MOS 29-OCT-2003 SL 737-SL-27-170 TRAILING EDGE FLAP AND SPOILER HANDLE-LUBRICATION. SERVICE LETTER INFORMATIONAL MOS I8-DEC-2002 SL 737-SL-27-171 ELEVATOR CONTROL CABLE INSPECTION. SERVICE LETTER INFORMATIONAL MOS 21-JAN-2003 SL 737-SL-27-171 REV. A ELEVATOR CONTROL CABLE INSPECTION-INSUFFICIENT CLEARANCE. SERVICE LETTER INFORMATIONAL MOS 29-SEP-2003 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 267 Of 748 @ Camp Systems EFTA00618558

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 SL 737-SL-27-172 MOUNTING BRACKET FASTENERS INCORRECTLY INSTALLED. SERVICE LETTER INFORMATIONAL 02-JAN-2003 MOS SL 737-SL-27-173 ELEVATOR CABLE PULLEY NUT AND BOLT INSTALLATION-POTENTIAL FOR LOW TORQUE VALUE. SERVICE LETTER INFORMATIONAL MOS 01-AUG-2003 SL 737-SL-27-174 AILERON AND SPEED BRAKE CONTROL CABLE LOW TENSION. SERVICE LETTER INFORMATIONAL MOS 18-AUG-2003 SL 737-SL-27-175 AUTOPILOT ACTUATOR MOUNTING BOLTS-TORQUE INSPECTION. SERVICE LETTER INFORMATIONAL MOS 07-JUL-2003 SL 737-SL-27-175 REV. A AUTOPILOT ACTUATOR MOUNTING BOLTS-TORQUE INSPECTION. SERVICE LETTER INFORMATIONAL MOS 23-DEC-2003 SL 737-SL-27-176 AILERON CONTROL CABLE HIGH TENSION. SERVICE LETTER INFORMATIONAL MOS 13-JAN-2004 SL 737-SL-27-177 REV. A AILERON SPRING CARTRIDGE ANOMALIES. SERVICE LETTER INFORMATIONAL MOS 23-MAR-2004 SL 737-SL-27-178 REV. B TRAILING EDGE FLAP POWER DRIVE UNIT (POU) GEARBOX-NEW RETAINER WITH EXCLUDER SEAL. SERVICE LETTER INFORMATIONAL MOS 30-SEP-2004 SL 737-SL-27-178 REV. C TRAILING EDGE FLAP POWER DRIVE UNIT (POU) GEARBOX - NEW RETAINER WITH EXCLUDER SEAL (SUPERSEDED SUPERSEDED BY St 737-SL-27-178 REV. O). SERVICE LETTER 51OS SL 737-SL-27-178 REV. D TRAILING EDGE FLAP POWER DRIVE UNIT (POU) GEARBOX-NEW EXCLUDER SEAL. SERVICE LETTER RECOMMENDED MOS 30-NOV-2012 SL 737-SL-27-179 REV. A LEADING EDGE SLAT POSITION SENSOR INSTALLATION-POSSIBLE MIS-ORIENTATION ALLOWS WIRE BUNDLE INFORMATIONAL CHAFING. SERVICE LETTER MOS 15-JUL-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 268 Of 748 @ Camp Systems EFTA00618559

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 SL 737-SL-27-179 REV. B LEADING EDGE SLAT POSITION SENSOR INSTALLATION-POSSIBLE MIS-ORIENTATION ALLOWS WIRE BUNDLE CHAFING. SERVICE LETTER MOS 20-JUL-2004 51 737-SL-27-179 REV. C LEADING EDGE SLAT POSITION SENSOR INSTALLATION - POSSIBLE MIS-ORIENTATION ALLOWS WIRE BUNDLE CHAFING.. SERVICE LETTER MOS 26-APR-2005 51 737-SL-27-180 FLIGHT SPOILER PCU LEAKAGE DUE TO INCORRECT PISTON ROD SEAL. SERVICE LETTER MOS 04-AUG-2004 RECOMMENDED 51 737-SL-27-181 RUDDER SYSTEM ENHANCEMENT PROGRAM SERVICE BULLETIN-INCORRECT WIRE IN KIT. SERVICE LETTER INFORMATIONAL MOS I3-JUL-2004 51 737-SL-27-181 REV. A RUDDER SYSTEM ENHANCEMENT PROGRAM SERVICE BULLETIN - INCORRECT WIRE IN KIT. SERVICE LETTER MOS 25-MAY-2006 51 737-SL-27-182 ELEVATOR FEEL SHIFT MODULE FILLET SEAL INSPECTION. SERVICE LETTER INFORMATIONAL MOS II -OCT-2004 51 737-SL-27-183 ELEVATOR FEEL COMPUTER DISCLOSURE - OVERTOROUED FASTENERS. SERVICE LETTER INFORMATIONAL MOS I4-DEC-2004 51 737-SL-27-184 FLIGHT CONTROLS IN MAIN WHEEL WELL - CHANGES TO THE FINISH OF CADMIUM PLATED COMPONENTS.. SERVICE LETTER MOS 27-MAY-2005 SL 737-SL-27-184 REV. A FLIGHT CONTROLS IN MAIN WHEEL WELL - CHANGES TO THE FINISH OF CADMIUM PLATED COMPONENTS. SERVICE LETTER MOS I 3-DEC-2007 SL 737-SL-27-184 REV. 8 FLIGHT CONTROLS IN MAIN WHEEL WELL - CHANGES TO THE FINISH OF CADMIUM PLATED COMPONENTS. SERVICE LETTER MOS 19-JAN-2010 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 269 Of 748 @ Camp Systems EFTA00618560

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 SL 737-SL-27-185 07-DEC-2005 51 737-SL-27-185 REV. A RUDDER PEDAL ADJUSTMENT SHAFT. SERVICE LETTER 07-AUG-2066 SL 737-SL-27-186 TRAILING EDGE FLAP HANDLE HARD TO ROTATE - PULLEY AND CABLE CHECK. SERVICE LETTER MOS RUDDER PEDAL ADJUSTMENT SHAFT. SERVICE LETTER MOS MOS INFORMATIONAL 29-AUG-2005 SL 737-SL-27-186 REV. A TRAILING EDGE FLAP HANDLE HARD TO ROTATE - PULLEY AND CABLE CHECK. SERVICE LETTER MOS 09-APR-2007 SL 737-SL-27-186 REV. B TRAILING EDGE FLAP HANDLE HARD TO ROTATE - PULLEY AND CABLE CHECK. SERVICE LETTER COMPLIED WITH MOS 22-AUG-2008 I9-JUN-2007 3260:48 AFL 782 SL 737-SL-27-186 REV. C TRAILING EDGE FLAP HANDLE HARD TO ROTATE - PULLEY AND CABLE CHECK. SERVICE LETTER MOS 0I-APR-2009 RECOMMENDED SL 737-SL-27-188 AILERON CONTROL CABLE TENSION INSPECTION (SUPERSEDED BY 737-SL-27-188 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-27-188 REV. A AILERON CONTROL CABLE TENSION INSPECTION. SERVICE LETTER MOS SL 737-SL-27-189 09-JAN-2006 SL 737-SL-27-190 09-FEB-2006 TRAILING EDGE FLAP BALLSCREW - MIXED GREASE. SERVICE LETTER MOS STABILIZER TRIM MOTOR - EMI FILTER SUPPLIER CHANGE. SERVICE LETTER 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 270 Of 748 @ Camp Systems EFTA00618561

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 SL 737-SL-27-191 09-MAR-2006 SUSPECT CONTROL COLUMN WIRE BUNDLES. SERVICE LETTER MOS SL 737-SL-27-191 REV. A SUSPECT CONTROL COLUMN WIRE BUNDLES. SERVICE LETTER MOS 06-JUN-2006 SL 737-SL-27-191 REV. 8 SUSPECT CONTROL COLUMN WIRE BUNDLES. SERVICE LETTER MOS 22-MAR-2007 SL 737-SL-27-191 REV. C SUSPECT CONTROL COLUMN WIRE BUNDLES. SERVICE LETTER MOS 27-AUG-2007 51 737-SL-27-192 INSPECTION OF MACH TRIM TORQUE TUBE FOR OVERSIZED FASTENER HOLES OR EXCESSIVE FREEPLAY. SERVICE LETTER MOS 17-JUL-2006 51 737-SL-27-192 REV. A INSPECTION OF MACH TRIM TORQUE TUBE FOR OVERSIZED FASTENER HOLES OR EXCESSIVE FREEPLAY. SERVICE LETTER MOS 01-SEP-2006 SI. 737-SL-27-192 REV. 8 INSPECTION OF MACH TRIM TORQUE TUBE FOR OVERSIZED FASTENER HOLES OR EXCESSIVE FREEPLAY. SERVICE LETTER MOS 22-MAR-2007 SI. 737-SL-27-192 REV. C INSPECTION OF MACH TRIM TORQUE TUBE FOR OVERSIZED FASTENER HOLES OR EXCESSIVE FREEPLAY. SERVICE LETTER MOS 10-APR-2007 SI. 737-SL-27-192 REV. 0 INSPECTION OF MACH TRIM TORQUE TUBE FOR OVERSIZED FASTENER HOLES OR EXCESSIVE FREEPLAY. SERVICE LETTER MOS 24-JUL-2007 SI. 737-SL-27-19a STALL MANAGEMENT/YAW DAMPER MODULE ASSEMBLY MODIFICATION. M01747 NO. 1. M01748 NO. 2. PM 285A1010. SERVICE LETTER MOS 10-AUG-2006 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 271 Of 748 @ Camp Systems EFTA00618562

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 SL 737-SL-27-193 REV. A STALL MANAGEMENT/ YAW DAMPER MODULE ASSEMBLY MODIFICATION. M01747 NO. 1. MO I 748 NO. 2. PIN 285A1010. SERVICE LETTER MOS 27-JUL-2007 51 737-SL-27-195 ELEVATOR FEEL COMPUTER INPUT ROD WASHER INSTALLATION DISCREPANCY. SERVICE LETTER MOS I6-NOV-2006 SL 737-SL-27-195 REV. A ELEVATOR FEEL COMPUTER INPUT ROD WASHER INSTALLATION DISCREPANCY. SERVICE LETTER 24-JUL-2007 SL 737-SL-27-196 22-FEB-2007 MOS 22-AUG-2008 3260:48 AFL 782 TRAILING EDGE FLAP POSITION TRANSMITTER AND SKEW SENSOR CONNECTOR - WATER INGRESS. SERVICE LETTER MOS 51 737-SL-27-196 REV. A TRAILING EDGE FLAP POSITION TRANSMITTER AND SKEW SENSOR CONNECTOR - WATER INGRESS. SERVICE LETTER MOS 09-APR-2007 SL 737-SL-27-196 REV. 8 TRAILING EDGE FLAP POSITION TRANSMITTER AND SKEW SENSOR CONNECTOR - WATER INGRESS. SERVICE LETTER MOS I5-FEB-2008 SL 737-SL-27-198 10-APR-2007 51 737-SL-27-199 05-NOV-2007 SL 737-SL-27-200 19-OCT-2007 NOSE DOWN STAB TAKE-OFF WARNING SWITCH (S-546) PLACARD AND STAB NOSE DOWN LIMIT SWITCH (S-145) PLACARD INSTALLED INCORRECTLY. SERVICE LETTER MOS RUDDER TRIM INDICATOR - ERRATIC OR STUCK NEEDLE. SERVICE LETTER MOS WSA1 SPOILER CABLE MAY HAVE A MINIMAL RIDING CONDITION ON THE UPPER SIDE OF THE LOWER PULLEY OF THE 251A1411.6 SPOILER TURNAROUND PULLEY BRACKET. SERVICE LETTER MOS COMPUED WITH - IAW THE 58 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 272 Of 748 @ Camp Systems EFTA00618563

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 SL 737-SL-27-201 24-JAN-2008 LATERAL TRIM - AIRPLANE CONFIGURATION HISTORY AND CORRECTION. SERVICE LETTER MOS SL 737-SL-27-202 ELEVATOR FEEL COMPUTER - INSPECTION FOR FEEL COMPUTER RETURN SPRING. SERVICE LETTER MOS 24-JAN-2008 SL 737-SL-27-203 TROUBLESHOOTING FOR HIGH CONTROL WHEEL AND COLUMN FORCES. SERVICE LETTER MOS 24-JAN-2008 SL 737-SL-27-203 REV. A TROUBLESHOOTING FOR HIGH CONTROL WHEEL AND SUPERSEDED COLUMN FORCES (SUPERSEDED BY SL 737-SL-27-203 REV. B). SERVICE LETTER MOS SL SL 737-SL-27-203 REV. B 16-NOV-2012 737-SL-27-204 27-MAR-2008 TROUBLESHOOTING FOR HIGH CONTROL WHEEL AND COLUMN FORCES, SERVICE LETTER MOS SPEEDBRAKE GROUND PROXIMITY SENSOR ADJUSTMENT, SERVICE LETTER MOS RECOMMENDED SL 737-SL-27-205 ELEVATOR FEEL COMPUTER INPUT ROD FASTENER INSTALLATION DISCREPANCY. SERVICE LETTER MOS 18-JUL-2008 SL 737-SL-27-206 POSSIBLE CONTAMINATION OF STANDBY RUDDER PCU. SERVICE LETTER RECOMMENDED MOS 18-AUG-2009 SL 737-SL-27-207 SPEED BRAKE BRACKET ASSEMBLY -CABLE RETAINER BOLTS - TORQUE INSPECTION. SERVICE LETTER MOS 20-OCT-2008 SL 737-SL-27-208 SPOILER BRACKET MOUNTING BOLTS - TORQUE INSPECTION. SERVICE LETTER MOS 20-OCT-2008 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 273 Of 748 @ Camp Systems EFTA00618564

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: O5-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SL 737-SL-27-209 ELEVATOR POSITION SENSOR INSTALLATION - IMPROPER FASTENER TORQUE (SUPERSEDED BY SL 737-SL-27-209 REV. A). SERVICE LETTER MOS SUPERSEDED SL 737-SL-27-209 REV. A ELEVATOR POSITION SENSOR INSTALLATION - IMPROPER FASTENER TORQUE, SERVICE LETTER RECOMMENDED 22-MAR-2011 MOS SL 737-SL-27-210 19-AUG-2009 POSSIBLE CONTAMINATION OF AILERON/ELEVATOR PCU, SERVICE LETTER MOS RECOMMENDED SI. 737-SL-27-211 AIRPLANE PITCH UPSETS DURING MANUAL REVERSION TEST RECOMMENDED FLIGHTS DUE TO INCORRECT ADJUSTMENT OF ELEVATOR TAB PUSHRODS. SERVICE LETTER MOS OS-MAY-2009 a 737-SL-27-212 HORIZONTAL STABILIZER LIMIT AND WARNING SWITCH SUPERSEDED INSTALLATION (SUPERSEDED BY SL 737-SL-27-212 REV. A). SERVICE LETTER MOS a 737-SL-27-212 REV. A HORIZONTAL STABILIZER LIMIT AND WARNING SWITCH INSTALLATION (SUPERSEDED 8Y SL 737-SL-27-230 AND SL SUPERSEDED 737-SL-31-057). SERVICE LETTER MOS SL 737-SL-27-214 HORIZONTAL STABILIZER TRIM ACTUATOR- LOWER PLUG RECOMMENDED ASSEMBLY - OVER-SIZED 0 -RING GROOVE. SERVICE LETTER MOS 30-JUN-2009 SL 737-SL-27-215 LEAKAGE OF ELEVATOR TAB LOCK ACTUATORS ON SUPERSEDED RECENTLY DELIVERED AIRPLANES (SUPERSEDED BY SL 737-SL-27-215 REV. A). SERVICE LETTER MOS SL 737-SL-27-215 REV. A LEAKAGE OF ELEVATOR TAB LOCK ACTUATORS ON RECENTLY DELIVERED AIRPLANES. SERVICE LETTER RECOMMENDED MOS 04-DEC-2013 SL 737-SL-27-216 STABILIZER POSITION SENSOR INPUT ROD WASHER RECOMMENDED INSTALLATION DISCREPANCY. SERVICE LETTER MOS OS-NOV-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 274 Of 748 @ Camp Systems EFTA00618565

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 SL 737-SL-27-217 ELEVATOR SYSTEM COMPONENTS FASTENERS UNDERTOROUED. SERVICE LETTER RECOMMENDED MOS 08-DEC-2009 SL 737-SL-27-218 GROUND SPOILER INTERLOCK VALVE END PLATE ASSEMBLY RECOMMENDED INSTALLED UPSIDE DOWN. SERVICE LETTER MOS 07-JAN-2010 SL 737-SL-27-219 737NG FLAP/SLAT ELECTRONICS UNIT (FSEU) (M01746) - HISTORY. APPLICABILITY AND INTERCHANGEABILITY. SERVICE LETTER MOS 07-MAY-2010 SL 737-SL-27-220 AILERON CENTERING MECHANISM PIN DELIVERED WITHOUT REQUIRED SURFACE COATING. SERVICE LETTER RECOMMENDED MOS 26-JUL-2010 SL 737-SL-27-221 INCORRECT USE OF CAD PLATED SCREWS WITH TITANIUM PROXIMITY SENSOR P/N 80-207-01 ON WING LEADING RECOMMENDED EDGE. SERVICE LETTER MOS 20-AUG-2010 SL 737-SL-27-222 AILERON CENTERING MECHANISM LEVER DELIVERED WITH MINOR ASSEMBLY DAMAGE, SERVICE LETTER RECOMMENDED MOS 20-SEP-2010 SL 737-SL-27-223 GROUND SPOILER INTERLOCK VALVE IMPROVEMENTS. SERVICE LETTER RECOMMENDED MOS 14-OCT-2010 SL 737-SL-27-224 RUDER PCU - DAMAGE SUMMING LEVER BOLTS. SERVICE LETTER RECOMMENDED MOS 05-NOV-2010 SL 737-SL-27-225 6355C0001-01 STABILIZER TRIM MOTOR - MODIFICATION HISTORY (SUPERSEDED 8Y 737-SL-27-225 REV. A). SERVICE SUPERSEDED LETTER MOS SL 737-SL-27-225 REV. A 6355C0001-01 STABILIZER TRIM MOTOR- MODIFICATION HISTORY, SERVICE LETTER RECOMMENDED MOS 30-JAN-2014 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 275 Of 748 @ Camp Systems EFTA00618566

COMP Astant.frar• 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 SL 737-SL-27-226 STICK SHAKER MOTOR GROUND TERMINAL INSPECTION (SUPERSEDED BY SL 737-SL-27-226 REV. A). SERVICE LETTER MOS SUPERSEDED SL 737-SL-27-226 REV. A STICK SHAKER MOTOR GROUND TERMINAL INSPECTION (SUPERSEDED BY SL 737-SL-27-226 REV. B). SERVICE SUPERSEDED LETTER MOS SL 737-SL-27-226 REV. B 08-JUN-2012 STICK SHAKER MOTOR GROUND TERMINAL INSPECTION. SERVICE LETTER MOS RECOMMENDED SL 737-SL-27-227 RUDDER FEEL AND CENTERING INSTALLATION - FASTENERS UNDERTOROUED. SERVICE LETTER RECOMMENDED 17-NOV-2010 MOS SL 737-SL-27-228 TRAILING EDGE FLAP BALLSCREWS-IN-SERVICE WEAR. SERVICE LETTER RECOMMENDED 15-NOV-2010 MOS SI. 737-SL-27-229 737NG LEADING EDGE CRUISE DEPRESSURIZATION VALVE N00163). INCORRECTLY APPLIED INSTALLATION RECOMMENDED 16-DEC-2010 SEALANT. SERVICE LETTER MOS SL 737-SL-27-230 HORIZONTAL STABILIZER LIMIT SWITCH INSTALLATION (SUPERSEDED BY SL 737-SL-27-230 REV. A). SERVICE LETTER RECOMMENDED 31-MAR-2011 MOS SL 737-SL-27-230 REV. A HORIZONTAL STABILIZER LIMIT SWITCH INSTALLATION. SERVICE LETTER RECOMMENDED 08-FEB-20IS MOS SL 737-SL-27-231 GROUND STUD DECAL GD1086ST INCORRECTLY LABELED (SUPERSEDED BY SL 737-SL-27-231 REV. A). SERVICE SUPERSEDED LETTER MOS SL 737-SL-27-231 REV. A GROUND STUD DECAL GD1086ST INCORRECTLY LABELED (SUPERSEDED BY SL 737-SL-27-231 REV. 8). SERVICE SUPERSEDED LETTER 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 276 Of 748 @ Camp Systems EFTA00618567

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 SL 737-SL-27-231 REV. 8 09-DEC-2011 SL 737-SL-27-232 24-AUG-2011 SL 737-SL-27-233 09-DEC-2011 SL 737-SL-27-234 REV. A 13-AUG-2013 SL 737-SL-27-235 18-SEP-2012 SL 737-SL-27-236 GROUND STUD DECAL GD1086ST INCORRECTLY LABELED. SERVICE LETTER MOS AUTO SPEEDBRAKE ACTUATOR IMPROVEMENTS. SERVICE LETTER MOS WIRE BUNDLE W1032 POSSIBLE CHAFING. SERVICE LETTER MOS RECOMMENDED RECOMMENDED RECOMMENDED CORROSION PROTECTION FOR S138. S245. AND 51051 FLAP POSITION SWITCH CONNECTORS. SERVICE LETTER RECOMMENDED MOS GROUND STUD DECAL GD236ST POTENTIALLY LOCATED INCORRECTLY. SERVICE LETTER RECOMMENDED MOS S245 FLAP SWITCH CONNECTOR - POSSIBLE IMPROPER ASSEMBLY OF BACKSHELL CLAMP (SUPERSEDED BY SL SUPERSEDED 737-SL-27-236 REV. A). SERVICE LETTER MOS SL 737-SL-27-236 REV. A 5245 FLAP SWITCH CONNECTOR - POSSIBLE IMPROPER ASSEMBLY OF BACKSHELL CLAMP. SERVICE LETTER RECOMMENDED MOS 27-SEP-2012 SL 737-SL-27-238 19-SEP-2012 SL 737-SL-27-239 C5-FEB-20I3 SL 737-SL-27-240 16-NOV-2012 SL 737-SL-27-241 19-DEC-2012 INADVERTENT ACTIVATION OF RUDDER TRIM. SERVICE LETTER RECOMMENDED MOS RUDDER CENTERING UNIT SPRING ASSEMBLY - INCORRECT SPRING SEAT MATERIAL. SERVICE LETTER RECOMMENDED MOS TRAILING EDGE FLAP - ALTERNATE ELECTIC MOTOR - POSSIBILITY OF NO LUBRICATION FLUID. SERVICE LETTER RECOMMENDED MOS FLIGHT CONTROL DAMAGE CAUSED BY EXTREME WINDS. SERVICE LETTER 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 277 Of 748 @ Camp Systems EFTA00618568

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 SL 737-SL-27-242 POTENTIAL OF WIRES SHORTING TO GROUND ON STAB TRIM SWITCHES (SUPERSEDED BY SL 737-SL-27-242 REV. A). SUPERSEDED SERVICE LETTER MOS SL 737-SL-27-242 REV. A POTENTIAL OF WIRES SHORTING TO GROUND ON STAB TRIM SWITCHES (SUPERSEDED BY SL 737-SL-27-242 REV. B), SUPERSEDED SERVICE LETTER MOS SL 737-SL-27-242 REV. B 05-AUG-20I3 POTENTIAL OF WIRES SHORTING TO GROUND ON STAB TRIM SWITCHES. SERVICE LETTER MOS RECOMMENDED SL 737-SL-27-243 POSSIBLE ELECTRO-HYDRAULIC SERVO VALVE (EHSV) GASKET PLATE LEAKAGE ON PARKER AEROSPACE RUDDER RECOMMENDED POWER CONTROL UNITS (PCU), SERVICE LETTER MOS 21 -JUN-2073 SL 737-SL-27-244 POSSIBLE DISCREPANT FLOW LIMITER ASSEMBLIES. SERVICE LETTER RECOMMENDED MOS 06-SEP-2013 SL 737-SL-27-245 SHOULDER BOLT AND SLAT TORSION ROD CLEARANCE. SERVICE LETTER RECOMMENDED MOS 30-SEP-2013 SI. 737-SL-27-246 POSSIBLE EXTERNAL LEAKAGE FROM AILERON/ELEVATOR POWER CONTROL UNIT (PCU) CRANK ASSEMBLY SUPERSEDED (SUPERSEDED BY SL 737-SL-27-246 REV. A). SERVICE LETTER MOS SL 737-SL-27-246 REV. A POSSIBLE EXTERNAL LEAKAGE FROM AILERON/ELEVATOR POWER CONTROL UNIT (PCU) CRANK ASSEMBLY. RECOMMENDED SERVICE LETTER MOS 02-JUN-20I4 SL 737-SL-27-247 HORIZONTAL STABILIZER TRIM ACTUATOR- INPUT CAM ASSEMBLY- IMPROPERLY CARBURIZED. SERVICE LETTER RECOMMENDED MOS 21-APR-2014 SL 737-SL-27-248 FLIGHT SPOILER PCU RELIABILITY IMPROVEMENTS ON SHORT FIELD PERFORMANCE AIRPLANES. SERVICE LETTER RECOMMENDED MOS I I -JUN-20I4 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 278 Of 748 @ Camp Systems EFTA00618569

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 SL 737-SL-28-015 REV. D FUEL TANKS OPEN AND PURGED. ELECTRICAL POWER APPUCATION (SUPERSEDED 737-SL-28-082). SERVICE LETTER MOS SUPERSEDED I3-APR-2010 SL 737-SL-28-039 REV. B FUEL LEAK DETECTION AND REPAIR OVERVIEW VIDEO. SERVICE LETTER INFORMATIONAL MOS 1O-JAN-2002 SL 737-SL-28-044 REV. A AIRCRAFT USE OF DYED FUELS (SUPERSEDED BY SL 737-SL-28-044 REV. B). SERVICE LETTER SUPERSEDED - (s) MOS SL 737-SL-28-044 REV. B AIRCRAFT USE OF DYED FUELS. SERVICE LETTER RECOMMENDED MOS 02-APR-20I2 SL 737-SL-28-053 AIRCRAFT USE OF FUELS CONTAMINATED WITH DYE (SUPERSEDED BY SL 737-SL-28-053 REV. A). SERVICE LETTER SUPERSEDED MOS - SL 737-SL-28-053 REV. A AIRCRAFT USE OF FUELS CONTAMINATED WITH DYE. SERVICE LETTER RECOMMENDED MOS I6-APR-2012 SL 737-SL-28-055 DESIGN IMPROVEMENT FOR PITCH AND ROLL INCLINOMETERS TO PREVENT CRACKING OF GLASS TUBE, SERVICE INFORMATIONAL LETTER I8-JUN-1999 MOS - (s) SL 737-SL-28-055 REV. A DESIGN IMPROVEMENT FOR PITCH AND ROLL INCLINOMETERS TO PREVENT CRACKING OF GLASS TUBE. SERVICE INFORMATIONAL LETTER MOS 22-JAN-2003 SL 737-SL-28-056 FUEL QUANITITY PROCESSOR UNIT (FOPU) SOFTWARE IMPROVEMENTS. SERVICE LETTER INFORMATIONAL MOS 15-DEC-1999 - (s) SL 737-SL-28-057 NEW SCAVENGE PUMP INLET AND SCREEN.. SERVICE LETTER INFORMATIONAL MOS 15-AUG-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 279 Of 748 @ Camp Systems EFTA00618570

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 SL 737-SL-28-060 I9-OCT-2001 SHORT SCREWS INSTALLED ON ENGINE FUEL SHUTOFF VALVES. CROSSFEED VALVE. AND DEFUEL VALVE. SERVICE RECOMMENDED LETTER MOS SL 737-SL-28-060 REV. A SHORT SCREWS INSTALLED ON ENGINE FUEL SHUTOFF VALVES. CROSSFEED VALVE. AND DEFUEL VALVE. SERVICE INFORMATIONAL LETTER MOS 28-NOV-2001 - (s) SL 737-SL-28-060 REV. 8 SHORT SCREWS INSTALLED ON ENGINE FUEL SHUTOFF VALVES. CROSSFEED VALVE. AND DEFUEL VALVE. SERVICE LETTER MOS I5-OCT-2007 SL 737-SL-28-061 ESTIMATION OF FREEZING POINTS OF JET AMET A-I FUEL BLENDS(SUPERSEDEO BY SL 737-SL-28-061 REV. A). SUPERSEDED SERVICE LETTER MOS SL 737-SL-28-061 REV. A ESTIMATION OF FREEZING POINTS OF JET AMET A-I FUEL BLENDS(SUPERSEDEO BY SL 737-SL-28-061 REV. A). SUPERSEDED SERVICE LETTER MOS SI. 737-SL-28-061 REV. 8 ESTIMATION OF FREEZING POINTS OF JET A/JET A-I FUEL BLENDS (SUPERSEDED 8Y SL 737-SL-28-06I REV. C). SUPERSEDED SERVICE LETTER MOS SL 737-SL-28-061 REV. C ESTIMATION OF FREEZING POINTS OF JET AMET A-1 FUEL BLENDS. SERVICE LETTER RECOMMENDED MOS 28-NOV-2011 SL 737-SL-28-062 POSSIBLE MISS-LOCATION OF FUEL TANK VENT TUBE CLIMB PORT. SERVICE LETTER INFORMATIONAL MOS I8-JUN-2003 SL 737-SL-28-062 REV. A POSSIBLE MISS-LOCATION OF FUEL TANK VENT TUBE CLIMB PORT. SERVICE LETTER INFORMATIONAL MOS I5-SEP-2003 SL 737-SL-28-062 REV.B POSSIBLE MISS - LOCATION OF FUEL TANK VENT TUBE CLIMB PORT. SERVICE LETTER RECOMMENDED MOS 20-JUN-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 280 Of 748 @ Camp Systems EFTA00618571

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 SL 737-SL-28-063 APU FUEL LINE SHROUD DRAIN MAST DAMAGE PROTECTION. SERVICE LETTER MOS I9-NOV-2003 SL 737-SL-28-063 REV. A APU FUEL LINE SHROUD DRAIN MAST DAMAGE PROTECTION. SERVICE LETTER MOS I8-MAR-2005 SL 737-SL-28-063 REV. B APU FUEL LINE SHROUD DRAIN MAST DAMAGE PROTECTION. SERVICE LETTER MOS 07-AUG-2006 SL 737-SL-28-065 POTENTIAL FUEL LEAKS IN THE OUTBOARD ORYBAY ON 737NG AIRPLANE RETROFITTED WITH BLENDED WINGLETS. SERVICE LETTER MOS 28-JUN-2004 SL 737-SL-28-065 REV. A POTENTIAL FUEL LEAKS IN THE OUTBOARD ORYBAY ON 737NG AIRPLANE RETROFITTED WITH BLENDED WINGLETS. SERVICE LETTER MOS 01-AUG-2005 SL 737-SL-28-066 SPECIAL FEDERAL AVIATION REGULATION (SFAR) 88 DESIGN. OPERATION. AND MAINTENANCE TRAINING INFORMATION. SERVICE LETTER MOS 13-FEB-2007 SL 737-SL-28-066 REV. A SPECIAL FEDERAL AVIATION REGULATION (SFAR) 88 DESIGN. OPERATION. AND MAINTENANCE TRAINING INFORMATION. SERVICE LETTER MOS I 7-JUN-2008 SL 737-SL-28-067 SUSPECT FUELING FLOAT SWITCHES. SERVICE LETTER MOS 05-APR-2007 SL 737-SL-28-067 REV. A SUSPECT FUELING FLOAT SWITCHES. SERVICE LETTER MOS I3-DEC-2007 SL 737-SL-28-069 FUEL SYSTEM MOTOR OPERATED VALVE ACTUATORS, SERVICE LETTER MOS 21-MAY-2007 INFORMATIONAL INFORMATIONAL 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 281 Of 748 @ Camp Systems EFTA00618572

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 SL 737-SL-28-069 REV. A FUEL SYSTEM MOTOR OPERATED VALVE ACTUATORS. SERVICE LETTER 05-DEC-2008 MOS SL 737-SL-28-070 GROUND FAULT INTERRUPT (GA) RELAYS FOR THE FUEL BOOST PUMP. SERVICE LETTER MOS 24-JUL-2007 SL 737-SL-28-070 REV. A GROUND FAULT INTERRUPT (GFI) RELAYS FOR THE FUEL BOOST PUMP. SERVICE LETTER MOS 27-MAR-2008 SL 737-SL-28-07I AVIATION FUELS SPECIFICATION. SERVICE LETTER MOS I8-JAN-2008 SL 737-SL-28-07I REV. A AVIATION FUELS SPECIFICATION. SERVICE LETTER MOS I9-FEB-2008 SL 737-SL-28-071 REV. B AVIATION FUELS SPECIFICATION. SERVICE LETTER MOS 31 -JUL-2008 SL 737-SL-28-071 REV. C AVIATION FUELS SPECIFICATION (SUPERSEDED BY SL 737-SL-28-071 REV. D). SERVICE LETTER SUPERSEDED MOS SL 737-SL-28-07I REV. D AVIATION FUELS SPECIFICATION (SUPERSEDED BY SL 737-SL-28-071 REV. E). SERVICE LETTER SUPERSEDED MOS SL 737-SL-28-07I REV. E AVIATION FUELS SPECIFICATION. SERVICE LETTER RECOMMENDED MOS 27-JUN-20I2 SL 737-SL-28-072 WIRE BUNDLE W1126 POSSIBLE CHAFING. SERVICE LETTER MOS I8-JUL-2008 SL 737-SL-28-072 REV. A WIRE BUNDLE W1126 POSSIBLE CHAFING. SERVICE LETTER MOS 24-OCT-2008 74nsufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CM (EBT)-Estimated Base Time 282 Of 748 @ Camp Systems EFTA00618573

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 SL 737-SL-28-073 18-FEB-2009 AFL 863 SI. 737-SL-28-073 REV. A INTRODUCTION OF IMPROVED SPAR. DEFUEL AND CROSSFEED VALVE DISK (SUPERSEDED BY SL 737-SL-28-073 REV. SUPERSEDED 8). SERVICE LETTER INTRODUCTION OF IMPROVED SPAR. DEFUEL AND CROSSFEED VALVE DISK. SERVICE LETTER MOS - (s) MOS 29-AUG-2011 3533:32 COMPUEO WITH SL 737-SL-28-073 REV. 8 INTRODUCTION OF IMPROVED SPAR. DEFUEL AND CROSSFEED VALVE DISK (SUPERSEDED BY SL 737-SL-28-073 REV. SUPERSEDED COMPUEO WITH C). SERVICE LETTER MOS 29-AUG-2011 3533:32 AFL 863 SL 737-SL-28-073 REV. C 25-JUL-2012 INTRODUCTION OF IMPROVED SPAR. DEFUEL AND CROSSFEED VALVE DISK SERVICE LETTER MOS RECOMMENDED SL 737-SL-28-074 CENTER TANK REFUEL TUBE LOCATED IN THE RIGHT WING RECOMMENDED PM 344A2202-8 MAY BE INSTALLED BACKWARDS. SERVICE LETTER MOS I4-MAY-2009 SL 737-SL-28-075 POTENTIAL FOR FOREIGN OBJECTS LEFT IN THE FUEL TANK RECOMMENDED AFTER REWORK PRIOR TO AIRPLANE DELIVERY. SERVICE LETTER MOS I3-AUG-2009 SL 737-SL-28-076 POSSIBLE OVER-TWISTED LOCKWIRE ON THE MAIN TANK RECOMMENDED FUEL BOOST PUMPS. SERVICE LETTER MOS 24-NOV-2009 SL 737-SL-28-077 POSSIBLE OVER-TWISTED LOCKWIRE ON THE CENTER TANK RECOMMENDED FUEL BOOST PUMP DRAIN PLUG. SERVICE LETTER MOS 24-NOV-2009 SL 737-SL-28-078 POSSIBLE LACK OF SEALANT ON THE FUEL PUMP PRESSURE INFORMATIONAL SWITCH SPAR PENETRATIONS FOR THE LEFT AND RIGHT FORWARD MAIN-TANK PUMPS. SERVICE LETTER MOS 22-DEC-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 283 Of 748 @ Camp Systems EFTA00618574

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 SL 737-SL-28-079 22-DEC-2009 SL 737-SL-28-080 15-FEB-2010 POSSIBLE LACK OF SEALANT ON THE FUEL PUMP PRESSURE SWITCH SPAR PENETRATIONS FOR THE LEFT AND RIGHT CENTER-TANK OVERRIDE-PUMPS. SERVICE LETTER MOS INFORMATIONAL POTENTIAL UNDER-TORQUED FUEL SUMP DRAIN AND AN UNDER-TORQUED BULKHEAD FITTING NUT (SUPERSEDED SUPERSEDED BY 737-SL-28-080-A). SERVICE LETTER MOS SL 737-SL-28-080 REV. A POTENTIAL UNDER-TORQUED FUEL SUMP DRAIN AND AN UNDER-TORQUED BULKHEAD FITTING NUT. SERVICE LETTER MOS 09-JUN-20I0 SL 737-SL-28-081 CONNECTOR D01828 HAS INCORRECT PLATING. SERVICE LETTER RECOMMENDED MOS 25-MAR-2010 SL 737-SL-28-082 AIRCRAFT MAINTENANCE WITH FUEL CELLS OPEN. SERVICE LETTER INFORMATIONAL MOS I3-APR-2010 SL 737-SL-28-082 REV. A AIRCRAFT MAINTENANCE WITH FUEL CELLS OPEN (SUPERSEDED BY 737-SL-28-082 REV. B). SERVICE LETTER SUPERSEDED MOS 22-APR-20I0 SL 737-SL-28-082 REV. B AIRCRAFT MAINTENANCE WITH FUEL CELLS OPEN (SUPERSEDED BY SL 737-SL-28-082 REV. C), SERVICE LETTER SUPERSEDED MOS SL 737-SL-28-082 REV. C AIRCRAFT MAINTENANCE WITH FUEL CELLS OPEN. SERVICE LETTER RECOMMENDED MOS 27-JUN-20 I I SL 737-SL-28-083 POTENTIALLY MIS-INSTALLED LOCKWIRE FOR THE RH MAIN TANK FUEL QUANTITY INDICATING SYSTEM(FOIS) BULKHEAD CONNECTOR. SERVICE LETTER MOS I7-JUN-2010 SL 737-SL-28-085 WIRE BUNDLE CONTACTS P-15 REFUELING PANEL (SUPERSEDED BY SL 737-SL-28-085 REV. A). SERVICE LETTER SUPERSEDED 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 284 Of 748 @ Camp Systems EFTA00618575

CAMP Asiant.fran Atna: 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 SL 737-SL-28-085 REV. A WIRE BUNDLE CONTACTS P-15 REFUELING PANEL. SERVICE LETTER RECOMMENDED MOS 31-JAN-2012 SI. 737-SL-28-086 PM 343A2212-31-4 WATER SCAVENGE TUBE CLEARANCE (SUPERSEDED BY SI. 737-SL-28-086 REV. A). SERVICE SUPERSEDED LETTER MOS SL 737-SL-28-086 REV. A PM 343A2212-31-4 WATER SCAVENGE TUBE CLEARANCE (SUPERSEDED BY SL 737-SL-28-086 REV. B). SERVICE SUPERSEDED LETTER MOS SL 737-SL-28-086 REV. B P/N 343A2212-3/-4 WATER SCAVENGE TUBE CLEARANCE (SUPERSEDED BY SL 737-SL-28-086 REV. C). SERVICE RECOMMENDED LETTER MOS I8-APR-2012 SL 737-SL-28-086 REV. C PM 343A2212-3/-4 WATER SCAVENGE TUBE CLEARANCE (SUPERSEDED BY SL 737-SL-28-086 REV. 0). SERVICE SUPERSEDED LETTER MOS SL 737-SL-28-086 REV. D PIN 343A2212-31-4 WATER SCAVENGE TUBE CLEARANCE. SERVICE LETTER RECOMMENDED MOS 25-MAR-2014 SL 737-SL-28-087 FUEL QUANTITY INDICATION SYSTEM (FOIS) FUEL TANK UNITS WITH PLASTIC CLAMPS. SERVICE LETTER RECOMMENDED MOS 05-MAY-2011 SL 737-SL-28-088 SHIELD GROUND WIRES NOT CONNECTED TO GROUND STUD (SUPERSEDED BY SL 737-SL-28-088 REV. A). SERVICE SUPERSEDED LETTER MOS SL 737-SL-28-088 REV. A SHIELD GROUND WIRES NOT CONNECTED TO GROUND STUD. SERVICE LETTER RECOMMENDED MOS 14-NOV-2011 SL 737-SL-28-089 MOTOR OPERATED VALVE (54OV) ACTUATOR IMPROVEMENT. SERVICE LETTER RECOMMENDED MOS I9-DEC-2011 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 285 Of 748 @ Camp Systems EFTA00618576

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 SL 737-SL-28-090 20-JUL-2012 SL 737-SL-28-09I REFUELING PANEL LAMP MOD. SERVICE LETTER MOS • RECOMMENDED MISSING GROMMET FOR THE CENTER FUEL TANK SUMP DRAIN VALVE (SUPERSEDED BY SL 737-SL-28-091 REV. A). SUPERSEDED SERVICE LETTER MOS SL 737-SL-28-09I REV. A MISSING GROMMET FOR THE CENTER FUEL TANK SUMP DRAIN VALVE. SERVICE LETTER RECOMMENDED 13-JUN-2012 MOS SL 737-SL-28-092 POTENTIAL MISSING WASHER AT FUEL TANK VENT TUBE DRAIN. SERVICE LETTER RECOMMENDED 20-JUL-2012 MOS SL 737-SL-28-093 MAIN TANK REFUEL TUBE ASSEMBLY. 344A2201-12. MAY BE INSTALLED INCORRECTLY. SERVICE LETTER RECOMMENDED 06-MAR-2013 MOS SL 737-SL-28-094 FUEL TEMPERATURE SENSOR WIRE CHAFING. SERVICE LETTER RECOMMENDED I9-JUN-2013 MOS SL 737-SL-28-095 ENGINE FUEL SUCTION FEED TEST - ENGINE PARAMETER CHANGES RECOMMENDED I3-AUG-2013 . SERVICE LETTER MOS SL 737-SL-28-096 ENGINE FUEL SHUTOFF VALVE WIRE CHAFING. SERVICE LETTER RECOMMENDED 10-DEC-2013 MOS SL 737-SL-28-098 FUEL BOOST PUMP BACKSHELL CHAFING WIRES. SERVICE LETTER RECOMMENDED 24-JUN-2014 MOS SL 737-SL-28-099 POSSIBLE MISSING FINISH ON APU DRAIN MAST TUBE. SERVICE LETTER RECOMMENDED MOS SL 737-SL-29-069 HYDRAULIC PRESSURE SWITCH REPLACEMENT. SERVICE LETTER INFORMATIONAL 26-AUG-1996 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 286 Of 748 @ Camp Systems EFTA00618577

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 SL 737-SL-29-069 REV. A HYDRAULIC PRESSURE SWITCH REPLACEMENT. SERVICE LETTER MOS 30-JAN-1997 - Is) 51 737-SL-29-069 REV. 8 HYDRAULIC PRESSURE SWITCH REPLACEMENT. SERVICE LETTER MOS 09-APR-1999 - (s) 51 737-SL-29-069 REV. C HYDRAULIC PRESSURE SWITCH REPLACEMENT. SERVICE LETTER MOS 24-MAY-2010 SL 737-SL-29-074 27-JUN-1998 SL 737-SL-29-075 18-AUG-1998 SL 737-SL-29-076 20-NOV-1998 INFORMATIONAL INFORMATIONAL RECOMMENDED HYDRAULIC PRESSURE TRANSDUCER IMPROVEMENT. SERVICE LETTER INFORMATIONAL MOS - (s) IMPROVED HYDRAULIC STANDBY SYSTEM MODULAR PACKAGE HOUSING. SERVICE LETTER INFORMATIONAL MOS - (s) CHAFING OF HYDRAULIC SYSTEM A ELECTRIC MOTOR-DRIVEN PUMP PRESSURE HOSE ON RETURN FILTER V-BAND INFORMATIONAL CLAMP. SERVICE LETTER MOS - Is) SL 737-SL-29-076 REV. A CHAFING OF HYDRAULIC SYSTEM A ELECTRIC MOTOR-DRIVEN PUMP PRESSURE HOSE ON RETURN FILTER V-BAND INFORMATIONAL CLAMP. SERVICE LETTER MOS 29-JUN-1999 - (s) SL 737-SL-29-078 HYDRAULIC FLUID NEW FORMULATION. SERVICE LETTER INFORMATIONAL MOS 29-JUL-1999 - SL 737-SL-29-079 INSUFFICIENT SWAGE ON THRUST REVERSER HYDRAULIC HOSES. PM AS115-06H0152. SERVICE LETTER INFORMATIONAL MOS 13-DEC-1999 - (s) SL 737-SL-29-080 CROSS CONNECTION OF LANDING GEAR HYDRAULIC LINES. SERVICE LETTER INFORMATIONAL MOS 05-JUL-2000 - 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 287 Of 748 @ Camp Systems EFTA00618578

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 SL 737-SL-29-081 03-NOV-2000 St 737-SL-29-082 IMPROVED ENGINE DRIVEN HYDRAULIC PUMP HOSE QUICK-DISCONNECTS. SERVICE LETTER MOS 500 (s) AFL NEW ELEVATOR TAB LOCK ACTUATOR HOSE. SERVICE LETTER MOS 17-NOV-2000 - (s) St 737-SL-29-082 REV. A NEW ELEVATOR TAB LOCK ACTUATOR HOSE. SERVICE LETTER MOS 21-DEC-2000 - (s) St 737-SL-29-082 REV. B NEW ELEVATOR TAB LOCK ACTUATOR HOSE. SERVICE LETTER MOS 23-MAR-2004 23-JUL-2001 320 127 St 737-SL-29-083 REV. A POSSIBLE IMPROPERLY TORQUED JAM NUTS ON BULKHEAD HYDRAULIC FITTINGS. SERVICE LETTER MOS 12-OCT-2001 - (s) St 737-SL-29-084 POSSIBLE THIN-WALL CONDITION ON PARKER ABEX ELECRTIC MOTOR-DRIVEN PUMPS. SERVICE LETTER MOS 24 (s) 08-OCT-2001 St 737-SL-29-084 REV. A POSSIBLE THIN-WALL CONDITION ON PARKER ABEX ELECRTIC MOTOR-DRIVEN PUMPS. SERVICE LETTER MOS 24 (s) 08-OCT-2001 St 737-SL-29-085 LOOSE JAM NUT ON ENGINE STRUT HYDRAULIC FITTING. SERVICE LETTER MOS 21-AUG-2002 INFORMATIONAL COMPUED WITH - -ACCOMPLISHED ON AAC WO 1828 AVV040 CLOSED 06/1561. CONSTITUTES TERMINATING ACTION. INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL AFL St 737-SL-29-085 REV. A LOOSE JAM NUT ON ENGINE STRUT HYDRAULIC FITTING. SERVICE LETTER INFORMATIONAL MOS 03-JUN-2003 St 737-SL-29-085 REV. B LOSE JAM NUT ON ENGINE STRUT HYDRAULIC FITTING (SUPERSEDED BY SL 737-SL-29-085 REV. C). SERVICE LETTER SUPERSEDED 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 288 Of 748 @ Camp Systems EFTA00618579

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 SL 737-SL-29-085 REV. C 10-JUN-2011 LOOSE JAM NUT ON ENGINE STRUT HYDRAULIC FITTING. SERVICE LETTER MOS RECOMMENDED SL 737-SL-29-086 ELECTRIC MOTOR OPERATED HYDRAULIC SHUTOFF VALVE INTERCHANGEABILITY. SERVICE LETTER INFORMATIONAL MOS 27-NOV-2002 SL 737-SL-29-087 TITEFLEX DISCLOSURE.IMPROPER HEAT TREATMENT ON HOSE B-NUTS. SERVICE LETTER INFORMATIONAL MOS I4-APR-2003 SL 737-SL-29-088 DRUCK HYDRAULIC PRESSURE TRANSDUCER DISCREPANCY. SERVICE LETTER INFORMATIONAL MOS I7-JAN-2003 SL 737-SL-29-089 ENGINE DRIVEN PUMP(EDP) AND AIR DRIVEN PUMP (ADP)- REPLACEMENT OF DISCREPANT WEAR PLATE. SERVICE INFORMATIONAL LETTER MOS 26-MAR-2003 SL 737-SL-29-090 FLIGHT CONTROLS HYDRAULIC MODULAR PACKAGE REPLACEMENT - INTERCHANGEABILITY (SUPERSEDED BY SL SUPERSEDED 737-SL-29-090 REV. A). SERVICE LETTER MOS SL 737-SL-29-090 REV. A FLIGHT CONTROLS HYDRAULIC MODULAR PACKAGE REPLACEMENT-INTERCHANGEABILITY. SERVICE LETTER RECOMMENDED MOS 23-NOV-2011 SL 737-SL-29-091 METHODS TO HELP REDUCE OR ELIMINATE PRELOAD WHEN REPLACING FRACTURED HYDRAULIC PRESSURE TUBE PfN 312A2110-2 IN 737NG STRUTS. SERVICE LETTER MOS 24-MAR-2005 St 737-SL-29-092 REV. A RECOMMENDED ACTION TO RESOLVE CORROSION OF HYDRAULIC TUBES IN THE WHEEL WELLS CAUSED BY EXPOSURE TO POTASSIUM-CONTAINING RUNWAY DEICING FLUIDS. SERVICE LETTER MOS 22-AUG-2005 St 737-SL-29-092 REV. 8 RECOMMENDED ACTION TO RESOLVE CORROSION OF HYDRAULIC TUBES IN THE WHEEL WELLS CAUSED BY EXPOSURE TO POTASSIUM-CONTAINING RUNWAY DEICING FLUIDS. SERVICE LETTER MOS 21-MAR-2006 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 289 Of 748 @ Camp Systems EFTA00618580

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 SL 737-SL-29-095 HYDRAULIC FLUID EXTERNAL LEAKAGE - RELIABILITY IMPROVEMENTS (SUPERSEDED BY SL 737-SL-29-095 REV. A), SUPERSEDED SERVICE LETTER MOS 51 737-SL-29-095 REV. A HYDRAULIC FLUID EXTERNAL LEAKAGE - RELIABILITY IMPROVEMENTS. SERVICE LETTER 22-DEC-2010 51 737-SL-29-096 INCORRECT SEALS IN HYDRAULIC SYSTEM A HEAT EXCHANGER FITTINGS. SERVICE LETTER 12-APR-2007 MOS MOS 51 737-SL-29-097 INCORRECT SADDLE-TYPE TUBE CLAMPS INSTALLED. SERVICE LETTER MOS 24-JUL-2007 51 737-SL-29-099 CORROSION-RESISTANT HYDRAULIC FUSES (SUPERSEDED BY 737-SL-29-099-A). SERVICE LETTER MOS 28-AUG-2007 51 737-SL-29-099 REV. A CORROSION-RESISTANT HYDRAULIC FUSES. SERVICE LETTER MOS 07-JUN-20I0 51 737-SL-29-100 TROUBLESHOOTING OF REPEATED ENGINE-DRIVEN PUMP FAILURES. SERVICE LETTER MOS 10-OCT-2007 SL 737-SL-29-100 REV. A TROUBLESHOOTING OF REPEATED ENGINE-DRIVEN PUMP FAILURES. SERVICE LETTER I7-OCT-2007 51 737-SL-29-101 17-DEC-2007 MOS FILTER ELEMENTS WITH INCORRECT EPDXY OR INCORRECTLY MACHINED 0 -RING GROOVES. SERVICE LETTER MOS SL 737-SL-29-101 REV. A FILTER ELEMENTS WITH INCORRECT EPDXY OR INCORRECTLY MACHINED 0-RING GROOVES. SERVICE LETTER MOS 20-FEB-2008 RECOMMENDED SUPERSEDED 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 290 Of 748 @ Camp Systems EFTA00618581

CIMP Asiant.Inne Attn....14C 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: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SL 737-SL-29-102 20-JUN-2008 STANDBY HYDRAULIC SYSTEM CASE DRAIN FILTER I CHECK VALVE INSTALLED REVERSED. SERVICE LETTER MOS SL 737-SL-29-102 REV. A STANDBY HYDRAULIC SYSTEM CASE DRAIN FILTER / CHECK VALVE INSTALLED REVERSED. SERVICE LETTER 23-JAN-2009 MOS AFL SL 737-SL-29-103 HYDRAULIC FLUID - NEW FORMULATION. SERVICE LETTER MOS 26-JUN-2008 SL 737-SL-29-103 REV. A HYDRAULIC FLUID - NEW FORMULATION. SERVICE LETTER MOS 07-MAY-2012 • SL 737-SL-29-104 EXCESS SLACK IN WIRE W8538 CAUSES CHAFING AGAINST FAIRING PANEL. SERVICE LETTER MOS 29-AUG-2C08 28-SEP-2009 3378:04 812 SL 737-SL-29-104 REV. A EXCESS SLACK IN WIRE W8538 CAUSES CHAFING AGAINST FAIRING PANEL (SUPERSEDE BY SL 737-SL-29-104 REV. B). SERVICE LETTER MOS RECOMMENDED SUPERSEDED SL 737-SL-29-104 REV. B EXCESS SLACK IN WIRE W8538 CAUSES CHAFING AGAINST FAIRING PANEL. SERVICE LETTER RECOMMENDED MOS 18-MAY-2011 SL 737-SL-29-105 HYDRAULIC RESERVOIR DRAIN VALVE LEAKAGE. SERVICE LETTER MOS 11-AUG-2C08 SL 737-SL-29-106 RECOMMENDED HANDLING AND STORAGE PRACTICES FOR HYDRAULIC COMPONENTS USING BMS 3-11. SERVICE LETTER MOS 17-FEB-2009 SL 737-SL-29-107 18-MAY-20O9 CRACKING OF HYDRAULIC STANDBY SYSTEM RESERVOIR BOSS—AVAILABILITY OF NEW TUBE. SERVICE LETTER MOS RECOMMENDED COMPLIED WITH ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CAN (EBT)-Estimated Base Time 291 Of 748 '2 Camp Systems EFTA00618582

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 SL 737-SL-29-108 HYDRAULIC PRESSURE MODULE CARTRIDGE CHECK VALVE RECOMMENDED FRACTURES. SERVICE LETTER MOS 07-JUL-2009 SL 737-SL-29-108 REV. 8 HYDRAULIC PRESSURE MODULE CARTRIDGE CHECK VALVE FRACTURES. SERVICE LETTER INFORMATIONAL MOS IS-MAR-2010 SL 737-SL-29-108 REV. C HYDRAULIC PRESSURE MODULE CARTRIDGE CHECK VALVE FRACTURES (SUPERSEDED BY SL 737-SL-29-108 REV. SUPERSEDED 0). SERVICE LETTER MOS SL 737-SL-29-108 REV. D POTENTIAL PERSONAL HAZARD - HYDRAULIC PRESSURE MODULE CARTRIDGE CHECK VALVE FRACTURES SUPERSEDED (SUPERSEDED BY SB 737-SL-29-108 REV. E). SERVICE LETTER MOS SL 737-SL-29-108 REV. E POTENTIAL PERSONAL HAZARD - HYDRAULIC PRESSURE MODULE CARTRIDGE CHECK VALVE FRACTURES. SERVICE RECOMMENDED LETTER I2-JUL-2013 SL 737-SL-29-109 MOS INTRODUCTION OF AXIALLY SWAGED PERMANENT HYDRAULIC FITTING AND TUBE INSTALLATIONS TO THE MAIN SUPERSEDED LANDING GEAR (MLG) WHEEL WELL (SUPERSEDED BY SL 737-SL-29-109 REV. A). SERVICE LETTER MOS SI. 737-SL-29-109 REV. A INTRODUCTION OF AXIALLY SWAGED PERMANENT HYDRAULIC FITTING AND TUBE INSTALLATIONS TO THE MAIN SUPERSEDED LANDING GEAR (MLG) WHEEL WELL (SUPERSEDED BY SL 737-SL-29-109 REV. B). SERVICE LETTER MOS SI. 737-SL-29-109 REV. 8 INTRODUCTION OF AXIALLY SWAGED PERMANENT HYDRAULIC FITTING AND TUBE INSTALLATIONS TO THE MAIN RECOMMENDED LANDING GEAR (MLG) WHEEL WELL. SERVICE LETTER -JAN-2012 SL 737-SL-29-110 I8-JUN-2010 SL 737-SL-29-111 MOS HYDRAULIC FLUID - NEW FORMULATION-SKYDROL-PE-5. SERVICE LETTER MOS POSSIBLE HYDRAULIC TUBE INSUFFICIENT CLEARANCE. MAIN WHEEL WELL (SUPERSEDED 8Y SL 737-SL-29-111 REV. SUPERSEDED A). SERVICE LETTER 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 292 Of 748 @ Camp Systems EFTA00618583

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 SL 737-SL-29-111 REV. A POSSIBLE HYDRAULIC TUBE INSUFFICIENT CLEARANCE. MAIN WHEEL WELL. SERVICE LETTER MOS 28-SEP-2011 SL 737-SL-29-112 RETURN FILTER MODULE IMPROVEMENTS - SYSTEM-A AND SYSTEM-B HYDRAULIC POWER (SUPERSEDED BY SL SUPERSEDED 737-SL-29-112 REV. A). SERVICE LETTER MOS RECOMMENDED SL 737-SL-29-112 REV. A RETURN FILTER MODULE IMPROVEMENTS - SYSTEM-A AND SYSTEM-B HYDRAULIC POWER (SUPERSEDED BY SL SUPERSEDED 737-SL-29-112 REV. 8). SERVICE LETTER MOS SL 737-SL-29-112 REV. 8 RETURM FILTER MODULE IMPROVEMENTS - SYSTEN-A AND SYSTEM-B HYDRAULIC POWER. SERVICE LETTER RECOMMENDED MOS I9-JUL-2012 SL 737-SL-29-113 POTENTIAL INSUFFICIENT CLEARANCE BETWEEN HYDRAULIC TUBE AND FILTER MODULE. SERVICE LETTER RECOMMENDED MOS I6-SEP-2011 SL 737-SL-29-114 MISSING PACKING IN FUSE ASSEMBLY PIN 2-7680-2 (SUPERSEDED BY SL 737-SL-29-114 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-29-114 REV. A MISSING PACKING IN FUSE ASSEMBLY PIN 2-7680-2. SERVICE LETTER RECOMMENDED MOS I8-APR-2012 SL 737-SL-29-115 GROUND STUD DECALS GO304DC 8 GD304ST (SUPERSEDED BY SL 737-SL-29-115 REV. A). SERVICE LETTER SUPERSEDED MOS SL 737-SL-29-115 REV. A GROUND STUD DECALS GO304DC 8 GD304ST (SUPERSEDED BY 737-SL-29-115 REV. B). SERVICE LETTER RECOMMENDED MOS 08-AUG-20I2 SL 737-SL-29-115 REV. 8 GROUND STUD DECALS GO304DC 8 GD304ST. SERVICE LETTER RECOMMENDED MOS 06-MAR-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 293 Of 748 @ Camp Systems EFTA00618584

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 SL 737-SL-29-116 POSSIBLE INSUFFICIENTLY TIGHTENED HYDRAULIC TUBE CONNECTIONS - LEFT AND RIGHT INBOARD WING REAR SUPERSEDED SPAR INSTALLATIONS (SUPERSEDED BY SL 737-SL-29-116 REV. A). SERVICE LETTER MOS SL 737-SL-29-116 REV. A POSSIBLE INSUFFICIENTLY TIGHTENED HYDRAULIC TUBE CONNECTIONS? LEFT AND RIGHT INBOARD WING REAR RECOMMENDED SPAR INSTALLATIONS. SERVICE LETTER MOS I3-APR-2012 SL 737-SL-29-117 IMPROVED EDP PRESSURE HOSE QUICK-DISCONNECTS. SERVICE LETTER RECOMMENDED 30-JUL-2012 MOS SL 737-SL-29-118 DETERMINE INSTALLATION TORQUE FOR TUBES/FITTINGSMOSES. SERVICE LETTER RECOMMENDED 30-NOV-2012 MOS SL 737-SL-29-119 TROUBLESHOOTING HYDRAULIC TUBE/FITTING/HOSE LEAKAGE. SERVICE LETTER RECOMMENDED 02-APR-20I3 MOS SL 737-SL-29-120 PREMATURE LEAKAGE OF SHAFT SEAL ON PARKER HYDRAULIC EDP AND PTU. SERVICE LETTER RECOMMENDED 10-DEC-2013 MOS SI. 737-SL-29-121 INCORRECT ORIENTATION OF POWER TRANSFER UNIT (PTU) RECOMMENDED 03-APR-20I4 PRESSURE FILTER ASSEMBLY. SERVICE LETTER MOS SL 737-SL-30-017 COWL THERMAL ANT-ICE VALVE IMPROVEMENT. SERVICE LETTER INFORMATIONAL 13-OCT-2000 MOS - (s) SL 737-SL-30-019 INTRODUCTION OF IMPROVED NOSE COWL THERMAL ANTI-ICE VALVE (SUPERSEDED BY SL 737-SL-30-019 REV. A). SUPERSEDED SERVICE LETTER 28-JUL-2003 SL 737-SL-30-019 REV. A 20-SEP-2013 MOS INTRODUCTION OF IMPROVED NOSE COWL THERMAL ANTI-ICE VALVES. SERVICE LETTER 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 294 Of 748 @ Camp Systems EFTA00618585

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 SL 737-SL-30-021 WINDOW HEAT CONTROL UNIT - DUST CONTAMINATION CLEANING PROCEDURES. SERVICE LETTER 29-AUG-2006 MOS AFL SL 737-SL-30-024 IDENTIFICATION OF DRAIN MAST MATERIAL. SERVICE LETTER INFORMATIONAL MOS 28-APR-2010 28-SEP-2009 3378:04 812 SL 737-SL-30-025 POTENTIAL IMPROPERLY TORQUED NUTS ON THE WING ANTI-ICE DUCT SUPPORT CLAMP (SUPERSEDED BY SL SUPERSEDED 737-SL-30-025 REV. A), SERVICE LETTER MOS SL 737-SL-30-025 REV. A POTENTIAL IMPROPERLY TORQUED NUTS ON THE WING ANTI-ICE DUCT SUPPORT CLAMP. SERVICE LETTER RECOMMENDED MOS 12-AUG-2013 SL 737-SL-31-038 COMMON DISPLAY SYSTEM (CDS) SOFTWARE UPDATE. SERVICE LETTER INFORMATIONAL MOS 08-DEC-1998 - (s) SI. 737-SL-31-039 COMMON DISPLAY SYSTEM (CDS) AND AIRPLANE INFORMATION MANAGEMENT SYSTEM (AIMS) NORMALLY WHITE INFORMATIONAL (NW) DISPLAY UNIT (DU) INCORPORATION. SERVICE LETTER MOS 10-MAR-1999 - (s) SI. 737-SL-31-039 REV. A COMMON DISPLAY SYSTEM (CDS) AND AIRPLANE INFORMATION MANAGEMENT SYSTEM (AIMS) NORMALLY WHITE INFORMATIONAL (NW) DISPLAY UNIT (DU) INCORPORATION. SERVICE LETTER MOS 18-DEC-2000 - (s) SL 737-SL-31-040 STICK SHAKEN SPEED DIFFERENCES INFORMATION. SERVICE LETTER INFORMATIONAL MOS 05-APR-1999 - (s) SL 737-SL-31-041 COMMON DISPLAY SYSTEM(CDS) BLOCK POINT 99 SOFTWARE RELEASE. SERVICE LETTER INFORMATIONAL MOS 24-DEC-1999 -(s) SL 737-SL-31-042 DISPLAYS: INCORPORATION OF PHASE II NORMALLY WHITE DISPLAY UNITS. SERVICE LETTER INFORMATIONAL MOS 1 7-SEP-2001 - (s) 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 295 Of 748 @ Camp Systems EFTA00618586

C4INI Asitant.P Inne Ad-gnu...14C 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 SL 737-SL-31-042 REV. A DISPLAYS: INCORPORATION OF PHASE II NORMALLY WHITE DISPLAY UNITS. SERVICE LETTER MOS 07-NOV-2C07 SL 737-SL-31-043 RUDDER PEDAL POSITION SENSOR COTTER PIN INSTALLATION. SERVICE LETTER MOS 21-NOV-2C01 • (s) SL 737-SL-31-044 COMMON DISPLAY SYSTEM (CDS) BLOCK POINT 02 SOFTWARE RELEASE. SERVICE LETTER MOS 11-FEB-2003 • SL 737-SL-31-044 REV. A COMMON DISPLAY SYSTEM (COS) BLOCK POINT 02 SOFTWARE RELEASE. SERVICE LETTER 07-MAR-2003 SL 737-SL-31-044 REV. B COMMON DISPLAY SYSTEM (COS) BLOCK POINT 02 SOFTWARE RELEASE. SERVICE LETTER 04-JUN-2003 MOS MOS SL 737-SL-31-044 REV. C COMMON DISPLAY SYSTEM (CDS) BLOCK POINT 02 SOFTWARE RELEASE. SERVICE LETTER MOS 07-JUL-2003 SL 737-SL-31-044 REV. D COMMON DISPLAY SYSTEM (CDS) BLOCK POINT 02 SOFTWARE RELEASE. SERVICE LETTER MOS 04-AUG-2C03 • SL 737-SL-31-044 REV. E COMMON DISPLAY SYSTEM (CDS) BLOCK POINT 02 SOFTWARE RELEASE. SERVICE LETTER 24-OCT-2003 SL 737-SL-31-044 REV. F COMMON DISPLAY SYSTEM (COS) BLOCK POINT 02 SOFTWARE RELEASE. SERVICE LETTER MOS 02-DEC-2003 MOS SL 737-SL-31-045 OPTICAL QUICK ACCESS RECORDER (OOAR) P/N D52C00 SERIES MODIFICATION. SERVICE LETTER MOS 02-FEB-2005 SL 737-SL-31-046 COMMON DISPLAY SYSTEM (COS) BLOCK POINT 04 SOFTWARE RELEASE. SERVICE LETTER MOS 03-MAR-2005 INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL INFORMATIONAL ?-Insufficient Information +-Task exists in Inspection Manual (s)-Suppressed Requirement (ex)-Excluded Tasks '-Estimated Due (New Requirement) (EFF)-Effective CAN (EBT)-Estimated Base Time 296 Of 748 .2 Camp Systems EFTA00618587

CORP As man wire „veland up AD/SI Status Report 737.72UBJ REVISION 21 Silk! 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 SL 737-SL-31-046 REV. A COMMON DISPLAY SYSTEM (CDS) BLOCK POINT 04 SOFTWARE RELEASE. SERVICE LETTER 28-JUN-2005 SL 737-SL-31-046 REV. 8 COMMON DISPLAY SYSTEM (CDS) BLOCK POINT 04A SOFTWARE RELEASE. SERVICE LETTER 16-NOV-2005 51 737-SL-31-047 GPS CLOCK REPLACEMENT. P/N 9010-14, SERVICE LETTER I6-JAN-2006 51 737-SL-31-048 COMMON DISPLAY SYSTEM (CDS) BLOCK POINT 06 SOFTWARE RELEASE. SERVICE LETTER MOS 19-SEP-2006 MOS MOS MOS SI. 737-SL-31-048 REV. A COMMON DISPLAY SYSTEM (CDS) BLOCK POINT 06 SOFTWARE RELEASE. SERVICE LETTER MOS 22-AUG-2008 18-SEP-2007 3260:48 AFL 782 SL 737-SL-31-049 CDS INHIBITION OF PFD TIME CRITICAL ALERTS, SERVICE LETTER MOS 15-MAR-2007 SL 737-SL-31-050 COMMON DISPLAY SYSTEM (CDS) DISPLAY ELECTRONIC UNIT (DEU-II). SERVICE LETTER MOS 12-SEP-2007 SL 737-SL-31-050 REV. A COMMON DISPLAY SYSTEM (CDS) DISPLAY ELECTRONIC UNIT (DEU-II), SERVICE LETTER MOS 05-MAY-2008 SL 737-SL-31-051 DISPLAYS: INCORPORATION OF PHASE 3 NORMALLY WHITE DISPLAY UNITS. SERVICE LETTER MOS 09-JAN-2009 SL 737-SL-31-051 REV. A DISPLAYS: INCORPORATION OF PHASE 3 NORMALLY WHITE RECOMMENDED DISPLAY UNITS. SERVICE LETTER MOS 26-MAR-2009 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 297 Of 748 @Camp Systems EFTA00618588

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 SL 737-SL-31-051 REV. B DISPLAYS: INCORPORATION OF PHASE 3 NORMALLY WHITE DISPLAY UNITS. SERVICE LETTER MOS 26-JUN-2009 SL 737-SL-31-051 REV. C DISPLAYS: INCORPORATION OF PHASE 3 NORMALLY WHITE DISPLAY UNITS. SERVICE LETTER MOS RECOMMENDED RECOMMENDED 10-SEP-2009 SL 737-SL-31-052 AURAL WARNING MODULE PIN 69-78214-4. SERVICE LETTER RECOMMENDED MOS 01-MAY-2009 SL 737-SL-31-052 REV. A AURAL WARNING MODULE P/N 69-78214-4. SERVICE LETTER RECOMMENDED MOS 16-SEP-2009 SL 737-SL-31-052 REV. B AURAL WARNING MODULE P/N 69-78214-4. SERVICE LETTER RECOMMENDED MOS 14-DEC-2009 SI. 737-SL-31-053 COMMON DISPLAY SYSTEM (CDS) DISPLAY ELECTRONIC RECOMMENDED UNIT (DEU-II) MOD A. SERVICE LETTER MOS I I -SEP-2009 SI. 737-SL-31-055 P8 AISLE STAND STAB TRIM LIGHTPLATE WITH INCORRECT NOMENCLATURE RECOMMENDED . SERVICE LETTER MOS 22-FEB-2010 SL 737-SL-31-056 NEW S651 SPEEDBRAKE LEVER TAKEOFF WARNING SWITCH ANOMALIES (SUPERSEDED BY SL 737-SL-31-056 REV. A). SUPERSEDED SERVICE LETTER MOS SL 737-SL-31-056 REV. A NEW S651 SPEEDBRAKE LEVER TAKEOFF WARNING SWITCH ANOMALIES. SERVICE LETTER RECOMMENDED MOS I9-MAY-2011 SL 737-SL-31-057 HORIZONTAL STABILIZER TAKEOFF WARNING SWITCH INSTALLATION (SUPERSEDED BY SL 737-SL-31-057 REV. A). RECOMMENDED SERVICE LETTER 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 298 Of 748 @ Camp Systems EFTA00618589

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 SL 737-SL-31-057 REV. A HORIZONTAL STABILIZER TAKEOFF WARNING SWITCH INSTALLATION. SERVICE LETTER RECOMMENDED MOS 08-FEB-2013 SL 737-SL-31-058 P1-3 AND P3-1 PANEL MODIFICATION: VENDOR SERVICE BULLETINS FOR THE CABIN ALTITUDE AND TAKE-OFF SUPERSEDED WARNING LIGHTS (SUPERSEDED BY SL 737-SL-31-058 REV. A). SERVICE LETTER MOS SL 737-SL-31-058 REV. A P1-3 AND P3-1 PANEL MODIFICATION: VENDOR SERVICE BULLETINS FOR THE CABIN ALTITUDE AND TAKE-OFF RECOMMENDED WARNING LIGHTS. SERVICE LETTER MOS 06-AUG-20I2 SL 737-SL-31-059 DISPLAYS: INCORPORATION OF PHASE 3A NORMALLY WHITE RECOMMENDED 77-SEP-2012 DISPLAY UNITS. SERVICE LETTER MOS SL 737-SL-32-074 PROXIMITY SWITCH ELECTRONIC UNIT, P/N Z85A1600. BITE MODULE CASKET MODIFICATION. SERVICE LETTER INFORMATIONAL 01 -JAN-2000 MOS - (s) SL 737-SL-32-075 IMPROPERLY TORQUED NOSE WHEEL STEERING TILLER NUT. SERVICE LETTER INFORMATIONAL 19-MAR-I999 MOS - (s) SL 737-SL-32-075 REV. A IMPROPERLY TORQUED NOSE WHEEL STEERING TILLER NUT. SERVICE LETTER INFORMATIONAL 17-NOV-2000 MOS - (s) SL 737-SL-32-076 MLG BRAKE HOUSING CORROSION AT HYDRAULIC DISCONNECT. SERVICE LETTER RECOMMENDED 17-SEP-2001 MOS - (s) SL 737-SL-32-076 REV. B MAIN LANDING GEAR BRAKE HOUSING CORROSION AT THE HYDRAULIC DISCONNECT COUPLING. SERVICE LETTER INFORMATIONAL 17-SEP-2001 MOS - (s) SL 737-SL-32-077 MLG TIRE SHOULDER WEAR. SERVICE LETTER RECOMMENDED 05-MAY-1999 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 299 Of 748 @ Camp Systems EFTA00618590

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 SL 737-SL-32-078 02-JUL-1999 SL 737-SL-32-079 ANTISKID/AUTOBRAKE CONTROL UNIT UPGRADE. SERVICE LETTER MOS - Is) APPROVED LG TIRE SUPPLIER P/NS (SUPERSEDED BY SL 737-SL-32-079 REV. A). SERVICE LETTER RECOMMENDED SUPERSEDED MOS - Is) SL 737-SL-32-079 REV. A APPROVED LG TIRE SUPPLIER P/NS (SUPERSEDED BY SL 737-SL-32-079 REV. B). SERVICE LETTER SUPERSEDED MOS - Is) SI. 737-SL-32-079 REV. B APPROVED SUPPLIER PART NUMBERS FOR LANDING GEAR (SUPERSEDED BY SL 737-SL-32-079 REV. C). SERVICE SUPERSEDED LETTER MOS - (s) SI. 737-SL-32-079 REV. C APPROVED SUPPLIER PART NUMBERS FOR LANDING GEAR TIRES (SUPERSEDED BY SI. 737-SL-32-079 REV. O). SUPERSEDED SERVICE LETTER MOS SI. 737-SL-32-079 REV. F APPROVED SUPPLIER PART NUMBERS FOR LANDING GEAR TIRES (SUPERSEDED BY SL 737-SL-32-079 REV. G). SUPERSEDED SERVICE LETTER MOS SL 737-SL-32-079 REV. G APPROVED SUPPLIER PART NUMBERS FOR LANDING GEAR TIRES (SUPERSEDED BY SL 737-SL-32-079 REV. H). SUPERSEDED SERVICE LETTER MOS SL 737-SL-32-079 REV. H APPROVED SUPPLIER PART NUMBERS FOR LANDING GEAR SUPERSEDED TIRES (SUPERSEDED BY SL 737-SL-32-079 REV. I). SERVICE LETTER MOS SL 737-SL-32-079 REV. I APPROVED SUPPLIER PART NUMBERS FOR LANDING GEAR TIRES (SUPERSEDED BY SL 737-SL-32-079 REV. J). SUPERSEDED SERVICE LETTER MOS SL 737-SL-32-079 REV. J APPROVED SUPPLIER PART NUMBERS FOR LANDING GEAR TIRES (SUPERSEDED BY SL 737-SL-M-079 REV. K), SUPERSEDED SERVICE LETTER 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 300 Of 748 @ Camp Systems EFTA00618591