Flight Options STC ST00881WI-D May 14, 2003 Page 2 WO030737.DOC STC ST00881WI-D Model MSN MSN 400A RK006 RK248 RK016 RK252 RK022 RK257 RK027 RK260 RK030 RK264 RK031 RK265 RK045 RK268 RK062 RK271 RK093 RK273 RK146 RK274 RK161 RK276 RK168 RK279 RK178 RK282 RK180 RK284 RK186 RK289 RK189 RK292 RK195 RK295 RK198 RK297 RK201 RK301 RK202 RK305 RK209 RK307 RK222 RK310 RK230 RK317 RK234 RK324 RK237 RK327 RK239 RK328 RK244 RK334 RK245 Please return a record of any additional aircra performed using this STC. My fax number is data before we can authorize additional installations. (s) to me for installations Collins needs to receive this EFTA00012069

% % a ..) EFTA00012070

••• Flight Options STC ST00881WI-D May 14, 2003 Page 3 WO030737.DOC Flight Options is responsible for the regulatory approval of any deviations from STC ST00881WI-D. Instructions explaining how to access the data on the CD have been inserted inside the jewel case. Customer satisfaction is important to us, and we would appreciate your input. Please corn lete and return the enclosed questionnaire or email me at nd let us know how we can best serve you. We trust this data will fulfill your installation requirements. However, if you have any questions, please call me at Collins Avionics Certification Center /pah Enclosure EFTA00012071

EFTA00012072

ee MAJOR REPAIR AND ALTERATION US DoPan:mon 0 (Airframe, Powerplant, Propeller, or Appliance) Federal /Melton Admkdstrallon Form Approved OMB No. 2120-0020 For FAA Use Only Arh ienn INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 or subsequent revision for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 31,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Beechjet Model 400A Serial No. RK- .214 4 Nationality and Registration Mark USA N 793T/) 2. Owner Name (As shown on registration certificate) Sitni AL.e TP C er-At_ Address (As shown on registration certificate) coicitarf, KS (.7. 1 °2 3. For FAA Use Only The data identified herein complied with applicable airworthines - The above described aircraft subject to conformity inspected - - ----- a - - --- --- ' This approval is ontifor this'aircraftmakerm Date Approving Inspector tr i m - 12002 6. Type 4. Unit Identification Unit Make Model Serial No. Repair Alteration AIRFRAME described in item X (As 1 above) POWERPLANT 7 1 • PROPELLER • APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Keith Gawsyszawski i i Richmond Hts., ON 44143 X U.S. Certificated Mechanic AP 287603483 Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above hereto have been made in accordance with the requrements of Part 43 of the U.S. information furnished herein is true and correct to the best of my knowledge. and described on the reverse or attachments Federal Aviation Regulations and that the Date April 5, 2002 7. Approval for Return To Service Pursuant Administrator BY to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is 00 APPROVED U REJECTED FM Fit. Standards Inspector Manufacturer ,K., Inspection Authorization Other (Specify) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 44 4,1 ?00?- Certificate or Designation No. iv,-1.1374.93A3P1 PM Noto EFTA00012073

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 1. Removed existing Tail Navigation Light Assembly including the rubber shock mount. 2. Installed Whelen Engineering, Inc. Model 70805-01 Tail Position Light Assembly in accordance with part number 04-0112558-00 instruction sheet to include installation procedures and drawing number 70805. 3. The light assembly will be operationally tested under Flight Options Continuous Airworthiness Maintenance Program under Phases IC, 9C and I7C. 4. Weight and Balance change found negligible. END-- Additional Sheets Are Attached *U.S.GPO:1994-568-012/00019 EFTA00012074

CO MAJOR REPAIR AND ALTERATION PO U.S. Department (Airframe, Powerplant, Propeller, or Appliance) of Transportation Federal Malkin Administration 'arm Approved OMB No. 2120-0020 For FAA Use Only Office Identification Li W!? Mt- INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make RAYTHEON AIRCRAFT Model 400A Serial No. RK-244 Nationality and Registration Mark USA N793TA 2. Owner Name (As shown on registration certificate) KETTLER ROBERT, MICHELS PIPELINE CONSTRUCTION INC, SOUTHEASTERN MILLS INC, REI AIR LLC, ET-AL Address (As shown on registration certificate) WICHITA KS 67207-1315 3. For FAA Use Only 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT • PROPELLER APPLIANCE TYPe Manufacturer 6. Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. RAYTHEON AIRCRAFT SERVICES SAN ANTONIO TEXAS 78216 us. Certificated Meclunie CRS-XA14605K LIMITED AIRFRAME Foreign Certificated Mechanic X ertificated Station C Repro M anufacturer D. I certify that the repair and/or have been made in accordance furnished herein is true and correct Date 12-10-01 alteration made to the unit(s) with the requirements to the best of m identified of Part 43 of knowled the unit identified and is in item 4 the U.S. Federal in item above and described on the reverse or attachments hereto Aviation Regulations and that the information 4 was inspected 'n the manner prescribed by the 0 REJECTED BY Pursuant to the authority given persons specified below, Administrator of the Federal Aviation Administration Pi APPROVED FAA Fit- Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee x Repair Station Person Approved by Transport • a Airworthiness Grou Date of Approval or Rejection 12-10-01 Certificate or Desisnation No. CRS-XA14605K FAA Form 337 (12.81) EFTA00012075

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. !den* with aircraft nationality and registration mark and date work completed.) MAKE: RAYTHEON 400A S/N: RK-244 REG: N793TA DATE: 12-10-01 ALL SEVEN CABIN SEATS AND THE LAVATORY SEAT WERE FIREBLOCKED IN ACCORDANCE WITH FAR 25.853 (a) APPENDIX F PART I (a) (1) (ii) AND FAR 25.853 (c) APPENDIX F PART II AMENDMENT 25-83. THE FIREBLOCKING WAS ACCOMPLISHED IN ACCORDANCE WITH THE SKANDIA INC. TEST PLAN #8335 REV. IR DATED 12-04-01, REFERENCE THE FORM 8110-3 DATED 12-04-01 APPROVED BY DESIGNATED ENGINEERING REPRESENTATIVE, #DERY-410100-CE, STRUCTURAL SPECIAL. SEE THE FORM 8110-3 DATED 10-09-01 AS REFERENCE FOR THE FIREBLOCKING FLAMMABILITY TEST RESULTS OF THE SEATS THAT WAS PREVIOUSLY TESTED AND APPROVED ON THE SKANDIA INC. TEST PLAN #8118 REV. IR DATED 10-01-01 FOR P/N 8118-1 AND 8118-2 ONLY, APPROVED BY DESIGNATED ENGINEERING REPRESENTATIVE, #DERY-410100-CE, STRUCTURAL SPECIAL. END El Additional Sheets Are Attached * U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00012076

0 MAJOR REPAIR AND ALTERATION I Department (Airframe, Powerplant, Propeller, or Appliance) el Federal Aviation Transportation Administration Form Approved OMB No. 2120.0020 For FAA Use Only Office Identification .9-7 9 a -, INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such vjolation (Section 901 Federal Aviation Act of I9581. I. Aircraft Make RAYTHEON AIRCRAFT Model 400A Serial No. RK-244 Nationality and Registration Mark USA N793TA 2. Owner Name (As shown on registration certificate) ICEITLER ROBERT, MICHELS PIPELINE CONSTRUCTION INC, SOUTHEASTERN MILLS INC, REI AIR. LLC, ET-AL Address (As shown on registration certificate) WICHITA KS 67207-1315 3. For FAA Use Only 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type ' Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. RAYTHEON AIRCRAFT SERVICES SAN ANTONIO TEXAS 78216 U.S. Certifkated Mechanic CRS-XA14605K LIMITED AIRFRAME - RADIO CLASS 1,11,III Foreign Certificated Mechanic X Certificthated Repair Station Mara a:rum D. I certify that the repair and/or alteration made to the unit(s) have been made in accordance with the requirements furnished herein is true and correct to the best of m Date 12-10-01 identified in item 4 above and described on the reverse or attachments hereto of Part 43 of the U.S. Federal Aviation Regulations and that the information knowled e. BY Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is l7 APPROVED 0 REJECTED FAA Fit Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee x Repair Station Pawn Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 12-10-01 Certificate or Designation No. CRS-XA14605K FAA Form 317 (12.88) EFTA00012077

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (i f more space is required attach additional sheets. Men* with aircraft nationally and registration mark and date work completed) MAKE: RAYTHEON 400A SIN: RK-244 REG: N793TA DATE: 12-10-01 MODIFIED THE EXISTING RIGHT HAND FORWARD GALLEY/CLOSET CABINET IN ACCORDANCE WITH THE RAYTHEON AIRCRAFT SERVICES DWG. #528-2526-001 REV. A DATED 07-27-00, REFERENCE THE FORM 8110-3 DATED 12-07-01 APPROVED DESIGNATED ENGINEERING REPRESENTATIVE, #DERT-405126-CE, STRUCTURAL. THE MODIFICATION CONSISTED OF INSTALLING ELECTRICAL PROVISIONS FOR A MAPCO, CUP HOLDERS AND LIGHTING IN THE FORWARD SECTION OF THE BAGGAGE CABINET. THE ELECTRICAL WIRING FOR THE GALLEY/CLOSET CABINET WAS INSTALLED IN ACCORDANCE WITH THE RAYTHEON AIRCRAFT SERVICES DWG. #RAS-73-0112 REV. ER DATED 12-05-01, REFERENCE THE FORM 8110-3 DATED 12-07-01 APPROVED BY DESIGNATED ENGINEERING REPRESENTATIVE, #DERT-710137-SW, SYSTEMS AND EQUIPMENT. THE MODIFIED GALLEY/CLOSET CABINET HAS A NEW WEIGHT OF 84.5 Lbs. AND A MOMENT OF 12844.0. THE WEIGHT AND BALANCE FORM AND THE EQUIPMENT LIST HAVE BEEN REVISED AND BOTH FORMS HAVE BEEN INSERTED IN THE AIRCRAFT FLIGHT MANUAL. END Ei Additional Sheets Me Attached * U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00012078

egp/ 1) MAJOR REPAIR ANDALTERATION US. Department (Airframe, Powerplant, Propeller, or Appliance) of Transportation Federal Aviation AdmInistntIon Form Approved OMB No. 2120-0020 For FAA Use Only Office Idenfification .....Nca-207 p t. INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51,000 for each such *lotion (Section 901 Federal Aviation Act of 19581. 1. Aircraft Make RAYTHEON AIRCRAFT Model 400A Serial No. RK-244 Nationality and Registration Mark USA N793TA 2. Owner Name (As shown on registration certificate) KETTLER ROBERT, MICHELS PIPELINE CONSTRUCTION INC, SOUTHEASTERN MILLS INC, REI AIR LLC, ET-AL Address (As shown on registration certificate) WICHITA KS 67207-1315 3. For FAA Usc Only 4. Unit Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPFI 1 Pla. APPLIANCE Wile Manufacturer 6. Conformity Statement A. Agencys Name and Address B. Kind of Agency C. Certificate No. RAYTHEON AIRCRAFT SERVICES 1115 PAUL WILKINS ROAD SAN ANTONIO TEXAS 78216 U.S Certificated Mechanic CRS-XAI4605K LIMITED AIRFRAME Foreign Catikated MeCtiallk X Certificated Repafr Station Mandsctunt D. I certify that the repair and/or alteration made to the unit( have been made in accordance with the requirements tbmished herein is true and correct to the best of m Date 12-10-01 ) identified in item 4 above and described on the reverse or attachments of Part 43 of the U.S. Federal Aviation Regulations and that the information hereto BY Date Pursuant to the authority given persons specified below, the unit identified in item Administrator of the Federal Aviation Administration and is la APPROVED 4 was inspected in the manner prescribed by the III REJECTED FAA Mt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) of Approval FAA Designee or Rejection 12-10-01 x Repair Station Certificate or Desinnation No. CRS-XA14605K Person Approved by Transport FAA Form 337 (1243s) EFTA00012079

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be ' compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished #f more space it required. attach additional sheets. Identify with aircraft nationally and registration mark and date work completed) MAKE: RAYTHEON 400A S/N: RIC-244 REG: N793TA DATE: 12-10-01 FABRICATED AND INSTALLED A NEW THE LIFE VEST CONTAINER IN THE TOILET CABINET IN ACCORDANCE WITH THE RAYTHEON AIRCRAFT SERVICES DWG. #562-3832-001 REV. IR DATED 08-22-00, REFERENCE THE FORM 8110-3 DATED 12-07-01 APPROVED BY DESIGNATED ENGINEERING REPRESENTATIVE, #DERT-405126-CE, STRUCTURAL. THE LIFE VEST CONTAINER WAS FABRICATED USING AAR COMPOSITES FLAT NOMEX PANEL P/N ATR-FP-251F2, REFERENCE THE FORM 8110-3 DATED 07-01-99 APPROVED BY DESIGNATED ENGINEERING REPRESENTATIVE, #CHI-410, STRUCTURAL SPECIAL. THE MODIFICATION OF THE CONTAINER WAS FOR THE INSTALLATION OF A NEW EASTERN AERO MARINE LIFE VEST, P/N PO1074-113. THE WEIGHT CHANGE IS NEGLIGIBLE. THE EQUIPMENT LIST HAS BEEN REVISED TO REFLECT THE NEW LIFE VEST AND HAS BEEN INSERTED IN THE AIRCRAFT FLIGHT MANUAL. END El Additional Sheets Am Attached * U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00012080

••• 0 I us oepaiment MAJOR REPAIR AND ALTERATION errnhnscxxiatan (Airframe, Powerplant, Propeller, or Appliance) Federal Million .......„„n Form Approved OMB No. 2120-0020 e'z,-... For FAA Use Only "le c'ethisro oge; ' ftb INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make RAYTHEON Model 400A Serial No. RK-244 Nationality and Registration Mark N793TA 2. Owner Name (As shown on registratkin certificate) AIRCAP LLC Address (As shown on registration certificate) WICHITA, KS 67207-1315 3. For FAA Use On y THE DATA IDENTIFIED HEREIN COMPLIES WITH APPLICAB AIRWORTHINESS REQUIREMENTS AND IS APPROVED ONLY FOR THE ABOVE DESCRIBED AIRCRAFT SU d CT T C NFO TY INSPECTION BY A PERSON AUTHORIZED IN FAR 43.7 APR 0 4 2000 DATE DPA-FSDO 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME described in Item 1 X (As above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Elliott Aviation Moline, IL 61266-0100 U.S. Certified Mechanic CGHR812C Foreign Certified Mechanic X Certificatedted Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 3/29/2000 7. Approv Pursuant to the authority given persons specified below, the unit dentified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 03 APPROVED 0 REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Da e of Approval or Rejection ft 9/ 90D0 Certificate or Designation No. CGHR812C Siaillilli Opp FAA Form 337 (1zes) EFTA00012081

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (if more space is required, attach additional sheets, Identify with aircraft nationality end registration mark and date work accomplished) 1. INSTALLED PENNY & GILES PASSENGER DIGITAL CABIN DISPLAY MODEL 2700. 2. THE CABIN DISPLAY WAS FLUSH MOUNTED IN THE FWD RH CLOSET/GALLEY CABINET AT 152.0 INCHES AFT OF DATUM FACING AFT. CONNECTED UNIT TO FACTORY PROVISION HARNESS LOCATED IN THE CABINET. THE UNIT WILL DISPLAY TEMPERATURE, TRUE AIRSPEED, ALTITUDE AND E.TA INFORMATION. THE DISPLAY IS FAA/PMA CERTIFIED. THE CABIN DISPLAY WAS INSTALLED IN ACCORDANCE WITH B&D INSTALLATION MANUAL P/N 2700-003-026 REV 0 DATED DECEMBER 19,1996. 3. PERFORMED EMI INTERFERENCE TEST IN ACCORDANCE WITH AC43.13-1B SECTION 8 PARAGRAPH 11-107 AND FAR 23.1309 AND 23.1431. 4. WEIGHT AND BALANCE DATA, EQUIPMENT LIST AND AIRFRAME LOGBOOKS WERE REVISED TO REFLECT THIS INSTALLATION. 5. FOR THE ABOVE INSTALLED SYSTEM NO ADDITIONAL MAINTENANCE IS REQUIRED BEYOND THE REQUIREMENTS OF 14 CFR PART 91 SUBPART E MAINTENANCE, PREVENTATIVE MAINTENANCE AND ALTERATIONS PER THE FOLLOWING INSTALLATION MANUAL• (1) B&D INSTALLATION MANUAL P/N 2700-003-026 REV 0 DATED DECEMBER 19,1996 5. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS CHECKLIST (1) INTRODUCTION-REF THIS 337 FORM BLOCK 1 (2) DESCRIPTION-REF THIS 337 FORM BLOCK 8 (3) CONTROL OPERATION INFORMATION- REF THIS 337 FORM BLOCK 8 (4) SERVING INFORMATION-NOT APPLICABLE (5) MAINTENANCE INSTRUCTIONS-REF THIS 337 FORM BLOCK 8 (6) TROUBLESHOOTING INFORMATION-REF THIS 337 FORM BLOCK 8 (7) REMOVAL AND REPLACEMENT-REF THIS 337 FORM BLOCK 8 (8) DIAGRAMS- NOT APPLICABLE (9) SPECIAL INSPECTION REQUIREMENTS-NOT APPLICABLE (10) APPLICATION OF PROTECTIVE TREATMENTS-NOT APPLICABLE (11) DATA-NOT APPLICABLE • (12) LIST OF SPECIAL TOOLS-NOT APPLICABLE (13) COMMUTER CATERGORY NC- ELECTRICAL LOAD ANALYSIS-NOT APPLICAPLE (14) NO ADDITIONAL OVERHAUL TIME LIMITATIONS (15) AIRWORTHINESS LIMITATIONS SECTION-NOT APPLICABLE (16) REVISION-IF A REVISION TO THIS ICA IS NECESSARY A LETTER WILL BE SUBMITTED TO THE LOCAL FSDO WITH A COPY OF THE REVISED FM FORM 337 AND REVISED ICA. END K Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00012082

• APR 2 1 MI I US Department MAJOR REPAfR AND ALTERATION of TronsporisSan (Airframe, Powerplant, Propeller, or Appliance) Fodor& Aviation AdmInistraUon Form Approved OMB No. 2120-0020 For FAA Use Only Atm Idettnyi lliefl- -F SDO INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BEECH Model 400A Serial No. RK-244 Nationality and Registration Mark N793TA 2. Owner Name (As shown on registration certificate) AIRCAP LLC Address (A wn n strafion certificate) WITCHA KS 67207-1315 3. For FAA Use On y 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Con ormity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Elliott Aviation Moline, IL 61266-0100 U.S. Certified Mechanic • . CGHR812C • Foreign Certified Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) Identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 4/14/00 Si 7. Appro Pursuant Administrator BY to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and Is IEJ APPROVED ID REJECTED FAA Ft Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 4/14/00 Certificate or Designation No. C G FAA Form 337 OM) EFTA00012083

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date worn accomplished.) 400A, RK-244, N793TA, 4/14100 Removed all the interior and the cabinetry items to facilitate a complete refurbishment of the interior per the customers request. Removed all the finishes and material's as required. Recovered the cabin headliner, the left and right hand window panels, the emergency exit panel and the cabin door upper panel with Douglas Interior products: Fabric, DEF 9135, PN 04, Ivory, DA. # 12777, REF # 402396-402545. See the bum test report WO #45065-00 and the form 8110-3, Both dated 03/03/00 and approved by D.E.R. #DERY 405020-CE, Structural special. Recovered the left and right hand drink ledge consoles with Rogers & n: Fabric, FRET #9103-05, Baroque, Treated at Skandia, REF treatment #SKEP41539. See the burn test report WO #46487- 00 and the FORM 8110-3, both dated 04-13-00 and approved by Judy Boggs, D.E.R. #DERV — 405020-CE structural special. Recovered both crew seats, seven cabin seats, the lavatory seat with leather Townsend leather. Leather, Classic pecan, Part #CL- 17, D/L #11428. See the bum test report WO# 44969-00 and the form 8110-3, both dated 03-01.00 and approved by Judy Boggs, D.E.R. 5020-CE structural special. The lower door panel , aft side of the left hand partitlan and both game table inserts with leather pecan, TF-17 D/L 11429.See bum test report Wo # 44969-00 dated 03/01/00 and approved by Judy Boggs DER # DERV 405020-CE. Recovered the aft right hand partition, the outboard side of the aft stub partition. the three panels of the aft baggage compartment and the Inside of the fwd closet/galley cabinet with aircraft interior products, fabric, grospoint #440, beige, lot #8817-8824, treated at Skandia, Ref. Treatment #SKFP15268, see the bum test report WO#35268 dated 06-24-99 and the form 8110.3 dated 07-16.99, both approved by D.E.R. #CHI-410, Structural special. Cut, fitted, surged and installed new carpet throughout the cockpit and cabin area using aircraft interior products, CTM Pattern N r. ultra suede 034. See the burn test report #AIP stock and the form 8110-3 both dated 3-03-00 and approved b D.E.R. #60-572, structures (interiors).. Removed the pilot and copilot crew seat restraint systems. Both restraint systems were sent out to Am Safe, Inc. for rework. Installed both crew seat restraint systems P/N 504246-401-2291 after work was accomplished by Am- Safe, Inc. Reference both 8130-3 Forms dated 04-07-00 from Am-Safe, Inc. Removed the lavatory seat and all cabin seat belt assemblies and inertia reels. Sent all out to Belt Makers, Inc. for rewebbing. Installed the rewebbed lavatory seat and all cabin seat belt assemblies and inertia reels, see the certification paperwork, WO #31888R. The galley/closet, upright storage cabinet, fwd and aft bulkheads, game tables, drink ledges and the vanity cabinet was covered with Carl F. Booth & Co. Waterfall Buginga Veneer., requirements. All seven cabin seats and the lavatory seat were fireblocili ew illardance with FAR 25.853 (a) appendix F part I (a) reference the burn test report #22702 dated 04-15-00 approved by D.E.R. #DERY405020-CE, for the flammability (1) (II) and FAR 25.85) (c) appendix F part II amendment 25-83. The fireblocking was accomplished in accordance with the Skandia, Inc. test plan #5880 Rev. new dated 04-13-00, , reference the form 8110-3 dated 04-13-00 approved by D.E.R. #DERY-405020-CE, structural special. Reference the FM Form 337 dated 0414-00. Complied with AD 7408-09 R2 Transport category that have one or more lavatories equipped with paper or linen waste receptacles by installing placards as required by this AD. AD 98-25-10R1 Aircraft Belts, Inc. Seat restraint system does not apply due to aircraft belts being AM-Safe inc. aircraft seat belts. The work performed on this aircraft has been inspected in accordance with the current maintenance rules of the Federal Aviation Regulations and for the work performed this aircraft is approved for return to service. Weigh and balance change negligible. END Q Additional Sheets Are Attached * U.S. G. P.O 1990-791-753 EFTA00012084

MAJOR REPAIR AND ALTERATION Form Approved OMB No. 2120-0020 uSOeparonent (Airframe, Powerplant, Propeller, or Appliance) of Transportatfon For FAA Use Only Federal Aviation - Administration Office Identification ) roue- ce- 00b-61 ofr INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each violation (Section 901 of Federal Aviation Act of 1958). Make Raytheon Model 400A 1. Aircraft Serial No. RK-244 Nationality and Registration Mark N428HR 2. Owner Name (As shown on registration certificate) See Attached Copy dd vin on registration certificate) . . Wichita, KS 67201 3. For FAA Use Only 4. Unit Identification S. Typo Und Make Model Serial No. Repair Alteration described in Item 1 AIRFRAME (As above) X POWERPLANT C) C..i --: •-•C --- .: C.") Z. .• • PROPELLER • .. et . . 8 - -I a - t APPLIANCE Type —"" 00 •• 0crt Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Kenneth W. Chitty X U.S. Certificated Mechanic 454944057 101 S. Webb Foreign Certificated Mechanic P.O. Box 2902 Certified Repair Station Witchita, Ks 67201-2902 Manufacturer D. I certify that the repair and/or alteration made to the unit(s Identified in item 4 above and described on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my know edge. Date 03-06-00 Signature of A 7. Approval for Retu Pursuant o the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is 031 APPROVED 0 REJECTED FAA Fit Standards Inspector Manufacturer X Inspection Authorization Other (Specify) BY FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Grou • Date of Approval or Rejection 03-06-00 Certificate or Designation No. 454944057 Signature of FAA Form 337 (12-88) 1r/ cc rn EFTA00012085

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If mom space is required, attach additional shoots. Identify with aircraft nationality and registration mark and date 1•.a& completed.) Installed Dog Harness P/N CS-H-1 in accordance with Aerodesign Engineering Report 1912-1 Rev.IR, 6-9-96, ( Faa Form 8110-3 dated 03-03-2000 is the Approved Data ) "Structual Substantiation, Restraint Harness for a Dog, installed into an Aircraft." This installation meets FAR 25.853b-2 Flammability requirements. This harness will be stored with the NC loose equipment and a copy of the Engineering report will be placed in the Flight Manual, instructions are in paragraph 3.0 No Weight & Balance change. END K Additional Sheets are Attached EFTA00012086

UNITED STATES OF規钢獻 DEPARTMENT OF TRA料SPORTATION-FEDERAL AVIATION ADMINISTR盯ION STANDARD AIRWORTHINESS CERTIFICATE NATO世AL耐AND REGISTRATION 'ARKS 2. 咽剮鄲TURER AND h ODEL 3．觫CRAFT SERIAL NU nER ．CATEGORY 暇黷蠟珊蒸戀鱗p轄Y N79n; 瞧 R和244 曬 5. AUTHORITY AND BASIS FOR ISSUANCE This airworthiness ceft翱郎鯽ed puts ant to the Federal Aviation Act of 195 and certifies that, as of the date o f issuance, the . a rcraft to which issued has been inspected and found to confofm to the type cectitate therC拖r, to be in condition for safe ope昭(ion: and has been sl own to meet the requirements of the applicable compreheilsive and detaited aim°rthiness code as provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein, Exceptions' 體齲 6 TERMS AND CONDITIONS Unless sooner surrendefed, suspended, revoked, or a termina∥on date is otherwise甾伍廿ished by the Admin trator, this 胖onihiness cerl'kale Ise什ective as long as the maintenance ．preventat e maintenance, and alle藺o鷓are perlorrned in accordance with Parts21．43．. d91 of theFederalAviatio fifiequ • lions,as appropriate, and the aircraft is registered in the United States, DATE OF ISSUANCE DESIGNATION NUMBER 可 璁囔鋤囤7 Any alteration, reprodu ion, or misuse of this cerlilicate may be punishable by a line not exceeding Si, 0,o imprisonment not exceeding 3．… years, or both, THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS,I . ; FAA Form 81昤2 眸) . *U.S,G.P.0:1 8 66S028 EFTA00012087

1 0 f. $ ' EFTA00012088

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND ' REGISTRATION MARYS N4281IR 2 11711d.UNIAiiirRALFT COMPANY 4001 3 AIRCRAFT SERIAL NUMBER RK-244 4 CATEGORY TRANSPOR 5 AUTHORITY AND BASIS FOR ISSUANCE This airwortiness certificate is issued pursuant tote Federal Aviation Act of 1958and certifies that, as of the date of issuance, the aircraft to which issued has been inspected and lound to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein. Exceptions: NONE 6 TERMS AND CONDITIONS Unless sooner surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator, this airworthiness certificate is effective as long as the maintenance, preventative maintenance, and alterations are performed in accordance with Parts 21,43, and 91 of the FederalAvialion Regulations, as appropriate, and the aircraft is registered in the United Stales. DATE OF ISSUANCE 10-01-99 DESIGNATION NUMBER MIR CE-50115, Any alteralion, reproduction, or misuse of thiscerhlicate may be punishable by a fine not exceeding S1,000, or imprisonment notexceeding 3 years, or both, THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100.2 (8.,s2) *U,S, GOVERNMENT PRINTING OFFICE:1R31 • 668.228 EFTA00012089

$ EFTA00012090

Or ?-11 fol MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) of Transportation Went Aviation Administration 1-orm Approved OMB No. 2120-0020 For FAA Use Only Office identification SW FSDO 17 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix 8, and AC 43.9-1 (or subsequen revision thereof) for Instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of1959). 1. Aircraft Make RAYTHEON Model 400A Serial No. RK-244 Nationality and Registration Mark USA N428HR 2. Owner Name (As shown on registration certificate) RAYTHEON AIRCRAFT COMPANY Address (As shown on registration certificate) WICHITA, KANSAS 67201-0085 3. For FAA Uso Only 4. Unit Identification 5. Typo Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement I-A, Agency's Name and Address 8. Kind of Agency C. Certificate No. RAYTHEON AIRCRAFT SERVICES SAN ANTONIO TEXAS 78216 U.S. Dedicated Mechanic CRS-XA14605K LIMITED AIRFRAME RADIO CUSS I,II,III Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the und(s) have been made in accordance with the requirements furnished herein is true and correct to the best of my knowledge. Date 12-22-99 of Part identified in item 4 above and described on the reverse or attachments hereto 43 of the U.S. Federal Aviation Regulations and that the Information , 7 BY Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is in item 4 was inspected in the manner prescribed by the fP APPROVED 0 REJECTED FAA Rt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Gro • Date of Approval or Rejection 12-22-99 Certificate or Designation No. CRS-XA14605K FAA Form 337 (1248) EFTA00012091

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identtot with aircraft nationally and registration mark and date kettlecompleted.) MAKE: RAYTHEON 400A Wit RK-244 REG: N428HR DATE: 12-22-99 INSTALLED AN ALLIEDSIGNAL FLITEFONE VI AIRBORNE RADIOTELEPHONE SYSTEM CONSISTING OF THE FOLLOWING EQUIPMENT: MOD/MFG DESCRIPTION WEIGHT ARM RT-18D REC/TRANSMITTER WRACK 400-0125-2000 7.8 47.8 WH-I0 HANDSET 400-0123-112 1.5 106.3 WH-IO HANDSET W/CORD 400-0123-112 2.5 252.0 AT-462 ANTENNA 121-014378-01 0.5 365.1 THE ALLIEDSIGNAL FLITEFONE VI SYSTEM WAS INSTALLED IN ACCORDANCE WITH THE BEECH AIRCRAFT CORPORATION DWG. #128-340675, REV. ORIGINAL, DATED 11-13-95 AND THE CHANGE ORDER #G76866 DATED 10-11-96. THE ELECTRICAL WIRING FOR THIS INSTALLATION WAS INSTALLED IN ACCORDANCE WITH THE BEECH AIRCRAFT CORPORATION DWG. 128-340606 REV. A DATED 10-27-94. A FUNCTIONAL TEST OF THE EQUIPMENT HAS BEEN PERFORMED IN ACCORDANCE WITH FAR 25.1301, FAR 25.1309 AND CHECKED IN ACCORDANCE WITH FAR 25.1431 FOR OPERATING SATISFACTORILY AND DID NOT ADVERSELY AFFECT OTHER COMPONENTS INSTALLED IN THE AIRCRAFT. THE ALLIEDSIGNAL FLITEFONE VI OPERATORS MANUAL P/N: 006-08834.0000 AND THE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOC. #FF VI-ICA-RK-244 DATED 12-22-99 HAVE BEEN INSERTED IN THE AIRCRAFT AS PART OF THE AIRCRAFT'S PERMANENT RECORDS. THE AIRCRAFT WEIGHT AND BALANCE FORM AND EQUIPMENT LIST HAVE BEEN REVISED TO REFLECT THIS MODIFICATION AND BOTH FORMS HAVE BEEN INSERTED IN THE AIRCRAFT FLIGHT MANUAL. END- K Additional Sheets Are Attached * U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00012092

RAYTHEON AIRCRAFT SERVICES ,SAN ANTONIO, TX. PAGE 1 OF 2 DOCUMENT NO. FF VI-ICA-RK-244 DATE: 12-22-99 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR A BEECHCRAFT MODEL 400A WITH AN ALLIEDSIGNAL FLITEFONE VI AIRBORNE RADIOTELEPHONE SYSTEM I. INTRODUCTION: THIS MAJOR ALTERATION TO THIS AIRCRAFT OBLIGATES THE AIRCRAFT OPERATOR TO INCLUDE THE FOLLOWING MAINTENANCE INFORMATION PROVIDED BY THIS DOCUMENT IN THE OWNER/OPERATOR'S AIRCRAFT MAINTENANCE MANUAL AND THE OWNER/OPERATOR'S AIRCRAFT SCHEDULED MAINTENANCE PROGRAM. 2. DESCRIPTION: THE ALLIEDSIGNAL FLITEFONE VI AIRBORNE RADIOTELEPHONE SYSTEM CONSISTS OF A RECEIVER/TRANSMITTER INCLUDING ITS MOUNTING RACK, TWO HANDSETS INCLUDING MOUNTING RACKS, TWO RETRACT CORDS, AN ANTENNA, ASSOCIATED WIRING, AND ANY RELATED HARDWARE. THE BASIC RADIOTELEPHONE SYSTEM IS A MOBILE COMMUNICATION SYSTEM FOR AIRCRAFT. IT OPERATES IN A FREQUENCY RANGE BETWEEN 454.675 - 454.975 Mhz 13 CHANNELS TO RECEIVE AND 459.675 - 459.975 Mhz 13 CHANNELS TO TRANSMIT. 3. CONTROL, OPERATION INFORMATION: REFERENCE THE ALLIEDSIGNAL FLITEFONE VI INSTALLATION MANUAL, REV. E, REPORT 1362, BASIC ISSUE DATED SEP. 1/90 AND THE ALLIEDSIGNAL FLITEFONE VI OPERATOR'S MANUAL P/N 006-08834-0000. 4. SERVICING INFORMATION: THE ALLIEDSIGNAL FLITEFONE VI AIRBORNE RADIOTELEPHONE SYSTEM IS ON CONDITION AND THERE IS NO PERIODIC, PREVENTIVE, OR SCHEDULED MAINTENANCE REQUIRED FOR CONTINUED OPERATION OF THIS SYSTEM. 5. MAINTENANCE INSTRUCTIONS: THE SCHEDULED MAINTENANCE TASKS REQUIRED BY THIS MODIFICATION TO BE ADDED TO THE AIRCRAFT OWNER/OPERATORS APPROPRIATE AIRPLANE MAINTENANCE PROGRAM AS FOLLOWS: a. PERFORM, ON AT LEAST AN ANNUAL BASES, A PERIODIC INSPECTION OF THE EQUIPMENT RACK, EQUIPMENT MOUNTINGS, ASSOCIATED WIRING, CABLES, CONNECTORS, HARDWARE, ANTENNA AND RELATED AIRCRAFT STRUCTURE FOR INTEGRITY, SECURITY, WEAR, CHAFFING, AND ETC.. SPECIAL ATTENTION SHOULD BE GIVEN TO THE AIRCRAFT PRIMARY STRUCTURE WITH REGARDS TO FATIGUE AND STRESS CRACKING, CORROSION, AND ETC.. 6. TROUBLESHOOTING INFORMATION: REFERENCE THE ALLIEDSIGNAL FLITEFONE VI AIRBORNE RADIOTELEPHONE SYSTEM MAINTENANCE MANUAL P/N 150-1364-000 REV. E, DATED SEP. 90 OR LATER REVISION. 7. REMOVAL AND REPLACEMENT INFORMATION: REFERENCE THE ALLIEDSIGNAL FLITEFONE VI AIRBORNE RADIOTELEPHONE SYSTEM MAINTENANCE MANUAL P/N 150-1364-000 REV. E, DATED SEP. 90 OR LATER REVISION. SHOULD IT BECOME NECESSARY TO REMOVE THE FLITEFONE VI, SECURE THE ASSOCIATED CABLES AND WIRING, COLLAR THE APPLICABLE CIRCUIT BREAKERS, PLACARD THE AIRCRAFT THAT THE UNIT HAS BEEN REMOVED, REVISE THE WEIGHT & BALANCE AND THE EQUIPMENT LIST AND MAKE A LOGBOOK ENTRY THE UNIT HAS BEEN REMOVED FOR SERVICE, REFER TO 91.213 OF TITLE 14 OF THE CODE OF FEDERAL REGULATIONS AND/OR THE AIRCRAFT'S MEL. 8. DIAGRAMS: THERE ARE NO ACCESS PLATES THAT NEED TO BE REMOVED FOR INSPECTION. 9. SPECIAL INSPECTION REQUIREMENTS: SPECIAL INSPECTION REQUIREMENTS ARE NOT APPLICABLE 10. APPLICATION OF PROTECTIVE TREATMENTS: APPLICATION OF PROTECTIVE TREATMENTS ARE NOT APPLICABLE. 11. DATA: INSTALLATION REQUIREMENTS MAY BE FOUND WITHIN THE ACCEPTED INDUSTRY PRACTICES CONTAINED WITHIN AC 43.13-1B CHAPTERS 4, 6, 7, 11, AND 12, AND IN ACCORDANCE WITH AC 43.13-2A CHAPTERS 1, 2, 3, II, AND 13. EFTA00012093

%a EFTA00012094

"RAYTHEON AIRCRAFT SERVICES • SAN ANTONIO, TX. 12. LIST OF SPECIAL TOOLS: SPECIAL TOOLS ARE NOT REQUIRED. PAGE 2 OF 2 DOCUMENT NO. FF VI-ICA-RK-244 DATE: 12-22-99 13. FOR COMMUTER CATEGORY AIRCRAFT: NOT APPLICABLE, THIS AIRCRAFT NOT COMMUTER CATEGORY AIRCRAFT a ELECTRICAL LOADS: THE RAYTHEON AIRCRAFT SERVICES ELECTRICAL LOAD ANALYSIS DOCUMENT REV. DATED AND THE RAYTHEON AIRCRAFT SERVICES EMI/RFI GROUND TEST PROCEDURES DOCUMENT N REV. DATED HAVE BEEN PLACED IN THE AIRCRAFT AS PART OF THE AIRCRAFT's PERMANENT RECORDS. b. METHODS OF BALANCING FLIGHT CONTROLS: N/A TO THIS INSTALLATION c. IDENTIFICATION OF PRIMARY AND SECONDARY STRUCTURES: N/A TO THIS INSTALLATION d. SPECIAL REPAIR METHODS APPLICABLE TO THE AIRPLANE: N/A TO THIS INSTALLATION 14. RECOMMENDED OVERHAUL PERIODS: THERE ARE NO ADDITIONAL OVERHAUL TIME LIMITATIONS. IS. AIRWORTHINESS LIMITATION SECTION: THERE ARE NO ADDITIONAL AIRWORTHINESS LIMITATIONS. 16. REVISION: THE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS CHECKLIST (ICA) MAY BE REVISED BY SUBMITTING A LETTER TO THE LOCAL FSDO WITH A COPY OF THE REVISED FAA FORM 337 AND REVISED ICA. THE FAA INSPECTOR ACCEPTS THE CHANGE BY SIGNING BLOCK 3 AND INCLUDING THE FOLLOWING STATEMENT: "THE ATTACHED REVISED/NEW INSTRUCTIONS FOR CONTINUED AIRWORTHINESS (DATE ) FOR THE ABOVE AIRCRAFT OR COMPONENT MAJOR ALTERATION HAVE BEEN ACCEPTED BY THE FAA, SUPERSEDING THE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS (DATE )." ONCE THE REVISION HAS BEEN ACCEPTED, A MAINTENANCE RECORD ENTRY WILL BE MADE, IDENTIFYING THE REVISION, ITS LOCATION AND DATE OF THE FORM 337. 17. ASSISTANCE: NOT APPLICABLE. 18. IMPLEMENTATION AND RECORD KEEPING: a. FOR MAJOR ALTERATIONS PERFORMED IN ACCORDANCE WITH FAA FIELD APPROVAL POLICY, THE OWNER/OPERATOR OPERATING UNDER PART 91 IS RESPONSIBLE FOR ENSURING THAT THE ICA IS MADE PART OF THE APPLICABLE SECTION 91.409 INSPECTION PROGRAM FOR THEIR AIRCRAFT. THIS IS ACCOMPLISHED WHEN A MAINTENANCE ENTRY IS MADE IN THE AIRCRAFT'S MAINTENANCE RECORD IN ACCORDANCE WITH SECTION 43.9. THIS ENTRY RECORDS THE MAJOR ALTERATION AND IDENTIFIES THE ORIGINAL ICA LOCATION (e.g., BLOCK 8 OF FAA FORM 337) ALONG WITH A INSPECTION/MAINTENANCE REQUIREMENTS. b. FOR MAJOR ALTERATIONS PERFORMED IN ACCORDANCE WITH A FIELD APPROVAL ON AIR CARRIER AIRCRAFT, THE AIR CARRIER OPERATOR IS RESPONSIBLE FOR ENSURING THAT THE ICA IS MADE PART OF THE APPLICABLE INSPECTION/MAINTENANCE PROGRAM FOR THEIR AIRCRAFT. IF A PROCEDURE IS NOT CURRENTLY INCLUDED IN THE OPERATOR'S MANUAL TO INCORPORATE ICA, THIS PROCESS WILL NEED TO BE APPROPRIATELY ADDRESSED (i.e. THE OPERATOR SUBMITS A REVISION TO ITS MAINTENANCE PROGRAM TO THE APPLICABLE CERTIFICATE-HOLDING DISTRICT OFFICE (CHDO). a FOR AIRCRAFT INSPECTED UNDER AN APPROVED AIRCRAFT INSPECTION PROGRAM (AAIP), THE OPERATOR WILL SUBMIT A CHANGE TO THE CHDO IN ACCORDANCE WITH SECTION 135.419B. d. FOR AIR CARRIER AIRCRAFT INSPECTED USING AN ANNUAL 100 HOUR INSPECTION PROGRAM, A REFERENCE TO NEW ICA WILL BE MADE IN THE AIRCRAFT'S MAINTENANCE RECORD IN ACCORDANCE WITH SECTION 43.9. THIS ENTRY RECORDS THE MAJOR ALTERATION AND IDENTIFIES THE ORIGINAL ICA LOCATION (e.g., ICA ARE LOCATED/ATTACHED TO BLOCK 8 OF FAA FORM 337). IN ADDITION, THE OPERATOR WILL REQUEST A REVISION TO THE OPERATOR'S OPERATIONS SPECIFICATIONS, ADDITIONAL MAINTENANCE REQUIREMENTS, WHICH INCORPORATES THE ICA INTO THE INSPECTION PROGRAM. EFTA00012095

EFTA00012096

ea MAJOR REPAIR AND ALTERATION KS. Deputnient (Airframe, Powerplant, Propeller, or Appliance) of I/deb:oration federal Aviation Admmoration Form Approved OMB No. 2120-0020 For FAA Use Only 02pe tdentification gene bYV FSDO 17 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequen revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a dvii penalty not to exceed 51000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make RAYTHEON Model 400A Serial No. RK-244 Nationality and Registration Mark USA N428HR 2. Owner Name (As shown on registration certificate) RAYTHEON AIRCRAFT COMPANY Address As shown on registration certificate) WICHITA, KANSAS 67201-0085 3. For FAA Uso Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. RAYTHEON ALRCRAFT SERVICES SAN ANTONIO TEXAS 78216 RADIO U.S. Certificated Mechanic CRS-XA14605K LIMITED AIRFRAME CLASS MUM Foreign Certificated Mechanic X certificated Repairs tation Manufacturer D. I net* that the repair and/or alteration made to the unit(s) have been made in accordance with the requirements furnished herein is true and correct to the best of my knowledge. Date 12-22-99 of Part the is identified in item 4 above and described on the reverse or attachments 43 of the U.S. Federal Aviation Regulations and that the information hereto specified below, Administration and BY Pursuant to the authority given persons Administrator of the Federal Aviation unit identified in item 4 was inspected In the manner prescribed by the 0 APPROVED 0 REJECTED FAA Rt. Standards Inspector Manufacturer Inspection Authorization Other (SIKCifY) FM Designee x I Repair Station Person Approved Canada Airworthin by Transport - p • Date of Approval 12-22-99 or Rejection Certificate or Designation No. CRS-XA14605K FAA Form 337 (I2-8e) EFTA00012097

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all pmvious alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (It more space is required, attach additional sheets Identify with aircraft nationality and registration mark and date work completed.) NINCE: RAYTHEON 400A S/N: RK-244 REG: N428HR DATE: 12-22-99 INSTALLED A SUNDSTRAND MIC-VI GROUND PROXIMITY WARNING SYSTEM CONSISTING OF THE FOLLOWING EQUIPMENT: MOD/MFG DESCRIPTION P/N WEIGHT ARM MK-VI GPWS COMPUTER 965-0686-020 4.2 33.1 ADC-500 CONVERTER 500-8020 2.3 38.2 BRACKET & PLATE 0.5 36.1 WIRING & CONNECTOR 3.5 54.0 THE SUNDSTRAND MK-VI GPWS SYSTEM WAS INSTALLED IN ACCORDANCE WITH THE STC #SA3322SO ISSUED 09-18-92 AND REISSUED 10-04-95 AND THE HANGER ONE MASTER DRAWING LIST #11892-GPWS, REV. D DATED 03-22-93. THE ELECTRICAL WIRING WAS INSTALLED IN ACCORDANCE WITH THE RAYTHEON AIRCRAFT SERVICES DWG. #RAS-67-9917 REV. IR DATED 11-05-99, REFERENCE THE FORM 8110-3 DATED 11-23-99 APPROVED BY ROBERT M. HURLEY, DESIGNATED ENGINEERING REPRESENTATIVE #DERT-710137-SW, SYSTEMS AND EQUIPMENT. A FUNCTIONAL TEST OF THE EQUIPMENT HAS BEEN PERFORMED IN ACCORDANCE WITH FAR 25.1301, FAR 25.1309 AND CHECKED IN ACCORDANCE WITH FAR 25.1431 FOR OPERATING SATISFACTORILY AND DID NOT ADVERSELY AFFECT OTHER COMPONENTS INSTALLED IN THE AIRCRAFT. THE SUNDSTRAND MK-VI GPWS APPROVED FLIGHT MANUAL SUPPLEMENT, REV. B DATED 03-30-93 HAS BEEN INSERTED IN THE SUPPLEMENT SECTION OF THE AIRCRAFT FLIGHT MANUAL AND THE GPWS PILOT'S GUIDE P/N 060-4087-000 REV. A DATED 10-96 HAS BEEN INSERTED IN THE AIRCRAFT AS PART OF THE AIRCRAFTS PERMANENT RECORDS. THE AIRCRAFT WEIGHT AND BALANCE FORM AND THE EQUIPMENT LIST WERE REVISED TO REFLECT THIS MODIFICATION AND BOTH FORMS WERE INSERTED IN THE AIRCRAFT FLIGHT MANUAL. END— D Additional Sheets Are Attached * U.S. GOVERNMENT PRINTING OFFICE: '992-769-012,60157 EFTA00012098

tad Ztatta Drxrim Beparanutt of transportation—fuleral 2thation Sadminisattion *upplemental tgpe Certificate c../Yetzinkit- al rcs, Inc. Fulton County Airport-Brown Eteld Atlanta, Georgia 30336 .gatiZadLa.7 .,.4w,a(4/i02.erirvA-fefe,i/owthns idoedmiXearnitalthn444;td.oniefedin;a SA3322SO .d.. A. ;a4,0friatadifenowoneater aaizaameraiemena-ari 25 . Federal Aviation a r ze.ama. iternsia e—peeareA.L.Snee...- ate: „ea Al6SW Beech 400A -44 ale-a9/47/ 5-Sesrv 4 k 2r: Installation of a Sundstrand MK VI GPAYWn necordance with ranger One. Drawing List No. 11892-GPWS, Rev. B, dated September 17, 1992, or I/16;r FAA Approved revision. Seciiim-44andLrea:rnad: This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that aircraft. FAA Approved Airplane Flight Manual Supplement, dated September 18, I992, is a required part of this STC. ir ewasaxeitseesandiefry4eWores:rdir eataithukte,oPS‘leitis-r.Wren ,a1,44esasrarre.esess,.e:tv.#4-4wesatias- S.2;:s4rai tars,z..1;:w COP2neiuIenx/Zon. August 5, 1992 September 18, 1992 October 4, 1995 Associate Manager, ACE-116A Atlanta Aircraft rertifititinn Offira (Title) Any alteration of this en:Orate is punishable by a fine of not exceeding ;1,000, or imprisonment not exceeding 3 years, or both. This route nay be transferred in accordance with FAR 21.17. CAA rota 6110-2 11 0-60) EFTA00012099

4- EFTA00012100

I II IV I L-I JJI~t-i1N_INV L_ .L - DWG. LIST NO. 11892- GPWS DATE 9/1/92 REV. D DATE 3/22/93 ET 1 OF 1 SYSTEM SUNDSTRAND MK- VI GPWS F. A. A. PROJECT NO. CE- 115A- 2970 . AIRCRAFT TYPE BEECHJET 400E STC SA 3 -3 2 2S0 DATED 9/18/92 DRAWING NO. REVISION SHTS PAGE EO/REMAR LTR DATE TITLE . TRI- 92- 108 9 - 2- 92 STRUCTURAL SUBSTANIATION REPORT GPWS AFMS B 3/22/93 AIRPLANE FLIGHT MANUAL SUPPLEMENT S 060- 3942 6/92 INSTALLATION DESIGN GUIDE 11892- 2 A 3/22/93 INSTALLATION PROCEDURES 11892- 3 A 3 / 2 2/93 BLOCK DIAGRAM 1 1 11892- 4 D 3/22/93 WIRING DIAGRAMS ° 2 182 11892- 5 8 - 29- 92 PARTS LIST & GENERAL NOTES 11892- 6 8 - 29- 92 GPWS MOUNTING PLATE 11892- 7 8 - 31- 92 ADC-S00 MOUNTING PLATE 11 '- 8 8 - 29- 92 SUPPORT BRACKET 892-1 A 3/22/93 GROUND TEST PROCEDURES 060- 3956- 000 D 9/17/92 FLIGHT TEST PROCEDURES 500- 8000- RO 8/29/92 DESIGN SPECIFICATIONS ADC-S00 .. . EFTA00012101

, • d a EFTA00012102

U.S DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 11)23/99 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION HAKE Beech MODEL NO. 400A TYPE Muria Rodeo. Idelmopstr. toc.I Airplane NAME OF APPLICANT Raytheon Aircraft Services LIST OF DATA - - ' IDENTIFICATION TITLE " Raytheon Drawings RAS-67.9917 Rev IR Dated 11/05/99 Sundstrand Mk-VI Ground Pro>amrty Warning Sys Note: This approval is for the Electrical aspects of the engineering design data only, and is not installation approval. Approval for aircraft SIN RK-244 only. Approval for GPWS is for only the minor deviations to FAA STC SA3322SO. . After modification is complete, perform EMURFI test In accordance with Raytneon report RAS-GF-9714, EMI/RF1 Test Procedure. PURPOSE OF DATA In support of a modification to install a GPWS in serial number RK-244. APPUCAS LE REOUIREMENTS(ArtspeoficcaA) FAR 25.1301 a,b,c FAR 25.1359 d FAR 25.1431 c CERTIFICATION - Under authority vested by direction of the of appointment under Pan 183 of the Federal Aviation Regulations, None have beat examined Administrator and in accordance with conditions and dam listed above and on attached sheets numbered in accordance with established procedures and found limitations to comply with applicable requirements of the Federal Aviation 70W Therdore K Rccommead Regulations. approval of That data these this ra Approve SIGNATURE(SI OF DESIGNATED ENGINEERING R AWES) DESIGNATION NUMBERS(E) CLASSIFICATIONS) DERT-710137-SW Systems & Equipment FAA Form 8110-3 (i1.70)9SEPMCESPRETICUS ENRON OFOreal 11- 23-99 13:SS RECEIVED FRO14:512 989-2998 P.03 EFTA00012103

t EFTA00012104

Form Approved O.M.B. No.21208018 APPLICATION FOR 0 . LLSDeporimcre AIRWORTHINESS of tonsponalicn CERTIFICATE Federal Arlation Administration INSTRUCTIONS - Print or type. Do not write in shaded areas: these are for FM useonly. Submit original only to an authorized FM Representative. II additional spacers required. use an attachment For special fight penes compete Sectaans II and VI or VII as applicable I. AIRCRAFT DESCRIPTION 1REGISTRATION MARK N428HR 2AIRCRAFT BUILDERS NAILS (Make) RAYTHEON AIRCRAFT COMPANY 3. AIRCRAFT MODEL DESIGNATION 400A 4.YR. MFR 1999 FM CODING 7,s cc 1 0 5. AIRCRAFT SERIAL NO. RK-244 6. ENGINE BUILDERS NAME WNW Pratt & Whitney Canada 7. ENGINE MODEL DESIGNATION JT15I3-5 tif --; // L S 8. NUMBER OF ENGINES 2 9. PROPELLER BUILDERS NAME (Mike) N/A 10. PROPELLER MODEL DESIGNATION N/A 11. AIRCRAFT LS (Check t I apptitable) (IMPORT II. CERTIFICATION REQUESTED APPLICATION IS HEREBY MADE FOR: (Check applicable awns ) A 1 X STANDARD AIRWORTHINESS CERTIFICATE (Indkate category) I Th)RMAI I I Inure t (ACROBATIC x (TRANSPORTI I GLIDER I BALLOON B SPECIAL AeftWOFITHINESS CERTIFICATE (Clerk Aapropda Ferns) 2 LIMITED 5 1 CLASS I PROVISIONAL (Mc:rate doss) 2 CLASS II 1 AGRICULTURE AND PEST CONTROL 2 AERIAL SURVEYING 3 AERIAL ADVERTISING 3 RESTRICTED (indicate opention(s) to be conducted) 4 FOREST (Wida(e conservation) 5 PATROLLING 6 WEATHER CONTROL 7 CARRIAGE OF CARGO 0 OTHER (Spear) EXPERIMENTAL flmacare operation(4) 1 RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT 3 EXHIBITION 4 to be Conducted) 4 RACING 5 CREW TRAINING MKT. SURVEY 0 TO SHOW COMPLIANCE WITH FAR I FERRY FLIGHT FOR REPAIRS. ALTERATIONS. MAINTENANCE OR STORAGE 8 SPECIAL FLIGHT PERMIT ancricale 00rvattbn to be conducted. then 2 EVACUATE FROM AREA OF IMPENDING DANGER complete Section VI or Fil as side) 3 OPEAT)ON IN EXCESS OF MAXIMUM CERTIFICATED TAKE-OFF WEIGHT apµcaNe on testae 4 DELIVERING OR EXPORT 15 I IPROCIUCTION FLIGHT TESTING 6 CUSTOMER DEMONSTRATION FLIGHTS C a Mu TIPLE AIRWORTHINESS CERTIFICATE (Check ASOVE Reftrided O0mM:on-and 'Standard' orUnided.'as eppdcab/ej ttL OWNER'S CERTIFICATION A. REGISTERED OWNER (As shorm on cerlificata ol aircraft registration) IF DEALER. CHECK HERE --ilt X NAME RAYTHEON AIRCRAFT COMPANY ADDRESS P.O. BOX 85 WICHITA, KS 87201 B. AIRCRAFT CERTIFICATION BASIS (Check opStobte Web and compkfa eerns as indkated) x AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE DATA SHEET (Give No. and Redsios No.) A16SW, Ray. 19 X AIRWORTHINESS DIRECTIVES (Cheek if ea applicable AD3 complied *In end 94P latest AD No.) ISSUE 99-20 AIRCRAFT LISTING (Ohre Pogo nyndelfFP N/A SUPPLEMENTAL TYPE CERTIFICATE (UR number cresol STCIncorpora fed) N/A C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS X CHECK IF RECORDS IN COMPLIANCE WM FAR 91.4.141. 417 TOTAL AIRFRAME HOURS BAO 3 EXPERIMENTAL ONLY (Enter hours dorm Ono° last ceiocato issued cr renewed) N/A • D. Admindballan elnyorthy CERTISCATON — I hereby certify that I am the registered owner (of his agent) A lho aircraft 'Ulan/eft above: mat the alrOaft Is registered with the Federal Aviaron Si accordance wen Section 501 of the Federal A/Saban Act of 1958. and appncobie Federal Adelson ReguiXions: and that the aircraft has been Inspected and Is and estable for the any:farness ceralkato requested. DATE 1041-99 OF APPLICATION Eugene Hainstock —Administrative Staff CIA A. THE AIRCRAFT OFftauRFD ABOVE WS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Complete This Sec on • is g - 2 FAR PART 121 OR 127 CERTIFICATE HOLDER (GA* Certaata Ab.) 3 CERTIFICATED MECHANIC (Gore CERTIFICATED REPAIR STATION (Gem CertAcare Certificate No) 6 No) a 4 0 ga ci 5 AIRCRAFT MANUFACTURER (We name or fend DATE TITLE SIGNATURE (alearALL riPPitable bodes in ilems A and B) X THE CERTIFICATE REQUESTED A. lend that Ow aircraft des/Abed In Scram I or VII meets requirements for: 4 AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHWESS CERTIFICATE p. B. Inspection for a special permit under Section VII FAA INSPECTOR I FM DESIGNEE g V i was conducted by: : I , . ... • R UNDER: 1 iFAR 65 I !AR 121.127 OR 135 I I FAR 145 c >iE gV DATE 10-01.99 DISTRICT OFFICE CE-43 4 1 FM INSPECTOR SIGNATURE FAA Form 81304 ii1481SUPERSEDES PREVIOUS EDITION GP0:1910241472/ta913 EFTA00012105

VI. PRODUCTION PUSHY TESTING A. MANUFACTURER . . . . NAME ADDRESS B. PRODUCTION BASIS (Check •Plattable Kern) PRODUCTION CERTIFICATE (GM pultrodon cetera,. number) TYPE CERTIFICATE ONLY APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE QUANTITY OF CERTIFICATES REOUIRED e FOR OPERATING NEEDS ► DATE OF APPLICATION NAME AND TITLE CAW or twe) SIGNATURE VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER THAN PRODUCTION FLIGHT TEST A. DESCRIPTION OF AIRCRAFT REGISTERED OWNER ADDRESS BUILDER (Make) MODEL SERIAL NUMBER REGISTRATION MARK B. ESCRIPTION OF FLIGHT CUSTOMER DEMONSTRATION FLIGHTS 0 (CUM if afanItafW) FROM TO VIA DEPARTURE DATE DURATION C. CREW REQUIRED TO OPERATE THE AIRCRAFT AND ITS EQUIPMENT PILOT I (CO-PILOT I (NAVIGATOR I I °MIER (SP°611) JI D. TN AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS REQUIREMENTS AS FOLLOWS: C E. THE FOLLOWING RESTRICODNS ARE CONSIDERED NECESSARY FOR SAFE OPERATION Rise attachment d necessary) .. . F. CERTIFICATION — I hereby certify lhal 18m tie nelstered war far Ns agent) of the *wail drambed above; that the aircraft is regtstered with the Federal Waton Administration in awYclance with Saloon 501 of the Federal Avtadon Ad of 1958. and applicaSe Federal Anadon Regutsticets; and that the airodft has been inspected and is aim:My lot the fliaM desoted. DATE NAME AND TITLE (Print 0" IMO SIGNATURE VIE AIRWORTHINESS DOCUMENTATION (FAA use only) X A. Operating Umnations and Marldngs In Compliarde wits FM 91.9 91.34-9 as AMatcatdo G. Statement of cord:miry FAA Form 8130-9 (Attach *hen feedred) H. Foreign AnwortNneSS Certificate." for Import Agoraft (Attach WWI /MAW B. °snail Operating UredaticoS Attached C. Data. Drawn. Photographs. etc (Attached whoa muffed) I. PreviousMu:manes& Condole Issued in ACCOfd&ICO VAIII FAR CAR (OrIghalAttached) X D. Current Weght are, Balance Inftemation Avaitatle In Alrcran E. Mater Remy and mieratren. FAA Conn 337 (Attached Men rewind) X J. Current /Unworthiness Cerlifcale Issued in Accordance with FAR 21.183 MI oaf 183 31 (Copy *P.M..) X F. This Inspection Recorded In Mersa Regards EFTA00012106

. EADT .Ortik.T__ES OF AMERICA R DEPARTMENT OF TRANSPORTATION-FEDERAL FE AVIATION ADMINISTRATION 4 STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND REGISTRATION MARKS N428FIR 2 MANUFACTURER AND MODEL RAYTHEON AIRCRtFT COMPANY 400A 3 AIRCRAFT SERIAL NUMBER R(.244 4 CATEGORY TRANSPORT 5 AUTHORITY AND BAS S FOR ISSUANCE This amorthinesscerlilicale is issued pursuant tote FederalAviation Act 011958 and cerlifies that, as of the date ol issuance, the aircraft to which issued has been inspected and bound to conform to the type cedificale therefor, to be in condition for safe operation. and has been shown io meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein, Exceptions. NallE 6 TERMS AND CONDITIONS Unless sooner surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator, this airworthiness certficate is effective as long as the maintenance, preventative maintenance, and alterations are performed in accordancewithParis2 4 n i1. r : . , . 10 . • .11 orahistegisIeredintheUded Slates, DATE OF ISSUANCE DESIGNATION NUMBER 10-01-9R ' •IR CE 01157 Any alteration, reproduclion,or misuse° I iscera icate may be punishable by a fine notexceeding $1,000, or imprisonmentnot exceeding 3 years, or both, THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS, FAA Form 8100-2 (a421 U.S. GOVERNMENT PRINTING OFFICE; 1591 •• 658.225 EFTA00012107

• • • • I, 4 EFTA00012108

C-- 77 I Coming • Pmr1 CANADA 2- E .- Transports Form E Canada Canada TorrtwuFre 24-0078 AUTHORIZED RELEASE CERTIFICATE - BON DE SORTIE AuTORtSé 3 Oemrmate Re, No . N•ee Menem do bees SEE BLOCK 5 4 Organ:ma • Otgantuee O Pratt & Whitney Canada Longueutl, Quebec 14G 1A1 5 Work OrmoConvaclavom . Son oe tnwancenlrablackee P.0.1 4000014605 ~mum. es Lens. l«....... IA U...len••••••• C.••••• 0 In 7 Desenotton FREE TURBINE TURBOFAN IT 15D-3 5 PM No • 6r de meta 3030100 9 Eicaly • kammstnlé • VARIOUS 10 Ory - Ore 1 11. Sometteleb No • area54MA» PCE-3A0256 12. 5141usAtIork • CimAravai MANUFACTURED 13 Recasts • Remarepn CANADIAN TYPE APPROVAL E-I I, FAA TYPE CERTIFICATE E25F.A. THIS ENGINE CONFORMS TO ITS UNTIED STATES TYPE DESIGN (TYPE CERTIFICATE NUMBER E23EA) AND IS IN CONDTTION FOR SAFE OPERATION. THIS ENGINE HAS BEEN SUBJECTED BY THE MANUFACTURER TO A FINAL OPERATION CHECK AND IS INA PROPER STATE OF AIRWORTHKESS. 14 New Pats • Pietas newts: AVM Cruses Set Nat* CANNY. 561 Cana« mal he pan(%) idencrel nose. OMNI el o eat cereTié Menke speo5rO as Week 13. Ni (Nt) been tad s. actawrece Enmeaciu•MAnipeate in ~Mace mM me ~Over' Mamie *Wen eats ass »itn ow itsvOniwnell t.OneeP1CO ewe Is Dell 001W la ger...le) enedut We-Mete a» 13. a Conn !ha »nlµale(s) COMOMemede Mix 43-0491 ee Penceofes et an resetinents se nar~wit .4.4. 19 Used Pans • Pieces usagets • CAR $71.10.14awmtnem• Reuse MC 571 10 - CertalCVM apt mbalenanoe Cerat.ect mat the maintenance &pealed abet* Ns been II cal emAll pa la Meanenee Spécae DAM • Tel pene are m •0:4541.InCt mil te MOON* stantlanf a fl eck& conlormemoni an normes ee ningabk4 of ~men Emil as .meeesse Speeded In DIM 4050mblet. Mens. anemmt sp5364.11 es ease 13.1a 13, me on a) n tare) skates foe scree. Ie rose en stew» ele It Ides) petals) eel atatnée. I6 Agreed Rel Na • Ref etautOrdalayi 20 Smtelum 21. ApplOvol RH. NM • RH omnonsabon I DOT APPROVAL 4 . 5/II I It Dale HAY 1 8 1999 22 Nome Mud or twintiodi - Rem telsetysegrapSewleVaorna) 23 Da - • IOSIaler n1413100.53.41/10Ck apply witri applcoNe leamal data Le entepeur eed winger Tedmea.45116 levee It. eennkneetkiqueS permeates. USERRNSTALLER RESPONSIBIUTIES R erporunt b welerstano tbe: M exillenOr 01 Ihel ~anent am eon not Morwicaly conittvle »Mary 10 NeWIMPWmNyCNJsstMtly. Van me user/Mama worts in 5000nUnCe int the moon*. segUNICAS 011, PiroOrlhuneoS Au:betty 0•11eren101an V{ AO•OtOOnelb kanConly or e» oxavry speoCed in lay. 10 rs C•51.2•31 net the vse*MitsPee eat...es MI Miner MoCiálhaeSt AJR104ity meets Mrlskompanenhiasteakkes from Me Amm>115.5ms ~Mayel ON country eyries et Po* I, Sinernenls 14 and IT CO nol ce•••11Mle Mu:Mon ~MAIM in aO cnes the Mrs. itenneal ~mamma mead 1~1 COS, a imeinlenenee instatelmn cenecaten nun» n accordance in. tne national semeebon by IN Yemenite», before me wean may be ilswn store osseoel RESPONSABILITES DE VUSAGERINIONTEUR a en moommi de ben eoropmeom ea de pin $0n toltelee CO emareent no cambia pat forttn•ent Macneaton elmteder la péceNoMpOuntleasenkee. Lemma tusnedironlesleusel DavaNe confmrémenl Dux stletnrill name 43me autord0 Ge ~natal.. *nee we 13010M6 de tuna,» munte ILI pu 1. t tN elItolel eue tutageraonteuNeute) Mum. eue sms Monk Co nemfaiNdd ample les Mon/CONTosanlidenserreks de TaufOnk de nawyeaté insane a la cant. Les Otace10.2 Mmausenl n.m. eases II el le ne =Moen: pal taw cenAcmon de ~thee En INA temps k ~set leampue C. ratan& at 03Mena one anikaten Mks menenenee !rose seta let lb;1enittlet ~a -ea. par Anapedmanieugevie). awe eve ratTond Mane elematt. EFTA00012109

1z c.} ci, E -taanssaort II:2:ft Form FONMASed 24-0078 AUTHORIZED RELEASE CERTIFICATE - BON DE SORTIE AUTORISE 3. CtrufcaN Ref No • N•41 'Orem< du DCA SEE BLOCK 5 42 :t at Whitney Canada Longueuil, uebee 4 1A1 $work OtdecCenbaellletre44 • Ban 0•1244oVentrautaate P.O. 1 4000016693 ..........,.........,•................<—.... FREE TURBINE TURBOFAN 11-15D-5 B Pan Ho • Woe ate 3030100 9 Elabery-A44416146 • VARIOUS 10 Oty • COO 1 II. Sonaltflatch Na - IP de sea PCE4A0257 12. StOnsiWork• ElaUtrovoi MANUFACTURED 5PPROVAL &I I, FAA TYPE CERTIFICATE EISEA. 'ORMS TO ITS UNITED STATES TYPE DESIGN (TYPE CERTIF/CATE NUMBER E2SEA) AND IS IN CONDITION FOR SAFE OPERATION. SEEN SUBJECTED BY 11W MANUFACTURER TO A FINAL OPERATION CHECK AND IS IN A PROPER STALE OF AIRWORTHINESS. veil: A'44 C14440 5.11 M de N C1442,561 Ote6144 ito.e. mot es l ess send* cue 4 mu para(s) tdet4114S) 4 44cl etA 13. has 0441 been said S. evIremeni spear; A Ia ease 13, a lontl el6 4 woos:lanes ea% be consoveRswispeattIE oontoinitisem aux &ages cc nd sou.. the aroonlontis «nceits1 Dentate, el OW Netements do na4 524514 cc.. 12 Used Pans. Rtees 03.12642 . CAR 571.10- AlartlerstACe ReAsse MC 571.10- CerlAcacon Nutt rrainlyatinCe Cented mot the manienance tended Rene has been u est one* quo ta onanlenruxe sptelfate el444. a Ail portormed 4 accordance wrin The raptcattle slanctods enema* Cordceintowne sox not444 de Annaba/a ot 3eSveddieseet FAcept as amines* Wedded 4 Mock app1Cabt S. S.44 4 auvenen 0461.1. i la cast IL 4 13. the WM* WO retested to1141242 is tense en Sentee de Ia (64)01441(1) al syl00160. 1. Appebal Ref. PIP ail crovionsousn 20. Sencitiec 21. Amore Ref. NP -flit 02.4.2243en I CIOTAPPROM 4. SI I IL Date HAI 19 1999 n Home mood et 44241). Nom (clacCOoropn16 cv Owe*/ 23. Oats hillier natal 0042444.4 ekolcivio wen aseleaki Reeked data • Le mayor dal vinner Cacirnombel6 cote las donntos bereicons pertnentes. USERANSTALLER RESPONSIBILITIES RESPONSABILITES DE L'USAGERXMONTEUR I um the existence el this °severest Row does not aucontabcaNt constitute aulsonry to ail Ye ettOrdinCe vele the NOWA rossemons of on Alnoschness Aullsordy clAttent pan Pie Covsky speared in bloat 14 4 Drum IF* ustanswite ensure' vv.: 'ism.. DO partstocconentsrasseenttles from ex AossairielasiAONOSIf C04•1•21Pteded COnstitite inUallaton ceitAcaten In at cafe Use stash Roma' lealeeteirled.e 'two 414440n Cel,fiCati00 1111ad g 3CCartellICe MN MO NW.* resivisson by Me 34 may In Av.ri - II ass 444444n1 de ben comptenctre eve de pa' son exestanoe es &anent ne 0:440.4 pas totaNntord ravenotion censuses 5$ peostomposonVensemble. Lon44 14.1•94444444(044) Vavv:hv conloimemem au itetements natal v4 Cone 3•4140 de • naAptalid, axe's qua Noon% de 4.44210446 mono 6 la case 1.11 at mantel Qa 4144244413414442, 0 stast.sce We Sea Mane co &beaten. acorn* In of eteementes do raotont6 de raropaCit6 mace a la case 1. Les 064.1waLco4 tip tatactlant No Cates 14 el 19 ne COnSleuefe pal oet onstrabon Ce moo ne En IPA leaps la dower leatrodoe 411•4•Onet 601 Content one uneaten apes nueuenoree felt scion Its esiVernsies nakikeikXxi Pat 42149•04044444•11. /want Coe 1464nel 4412 116401O4 EFTA00012110