AVOliCS Callenlien Center 400 Collins Road NE Mad Station 164100 Cedes Rapids. IA 52498 Tel. 319295.2185 Fax 319 295O337 Rockwell Collins May 14, 2003 W0030737.DOC Flight Options 26180 Curtiss-Wright Parkway Cleveland, 011 44143 Tel: (216) 797-3500 Attention: Subject: Mr. Jody Kremsreiter/ Mr. Richard Fine (Collins on-site) STC ST00881WI-0 Modification of Collins TCAS II System Installation with Collins TTR-920 Change 6.04a Receiver Transmitter and TPR-900 Mode S to a Collins TCAS II System Installation with Collins TTR-920, Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS II Receiver Transmitter and optional TPR-901 in Part 25 Aircraft Dear Mr. Kremsreiter: Enclosed is a compact disk with one copy each of the following FAA approved STC data: 1. STC ST00881WI-0 Certificate, dated December 1, 2000. 2. FAA Approved Model List (AML) Number ST00881WI-D, amended April 15, 2003. 3. Drawing Index 992-4358-001, Revision M. 4. One copy of each drawing listed on Drawing Index 992-4358-001. 5. Airplane Flight Manual Supplement, ACC-00-105, Revision -. This letter is our authorization for Flight Options to use this STC as basis for the installation of our equipment in your airplanes based on the following model and serial numbers provided by Mr. Richard Fine of Rockwell Collins. SDNY_GM_02755303 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242225 EFTA01327343

I SDNY_GM_02755304 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242226 EFTA01327344

Flight Options STC ST00881WI-D May 14, 2003 Page 2 Model 400A WO030737.DOC STC ST00881WI-D MSN MSN 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 aircraft serial number(s) to me for installations performed using this STC. My fax number is (319) 295-0337. Collins needs to receive this data before we can authorize additional installations. SDNY_GM_02755305 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242227 EFTA01327345

i SDNY_GM_02755306 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242228 EFTA01327346

is • Flight Options STC ST00881W1-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 complete 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 (319) 295-0618. Douglas W. Jessen Collins Avionics Certification Center Mail Station 164-100 /pah Enclosure SDNY_GM_02755307 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242229 EFTA01327347

SDNYGM02755308 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242230 EFTA01327348

0 US INV gamin d nearAvIsilon MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) Form Approved OMB No. 2120-0020 For FAA Use Only 41 C-le—ribt AdeMbeitrtike INSTRUCTIONS: Pnnt or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 or subsequent revision the 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 $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Beechjet Model 400A Serial No. RK- 2 414 Nationality and Registration Mark USA N99374 2. Owner Name (As shone on registration corifficate) Mist A-ig TPC ' CT -At- Address (As sham on registration certificate) go ( 5 Loal38 a COLcr*iTYt, KS 61, 0 7 3. For FM Use Only The data identified ' The 860e-deathbed - --- — — • -- — - • This Date herein complied with applicable aircraft subject to conformity approval is only for thiseircraft Approving airworthiness requirements inspection by a makermodel a vv. Inspector and is approved ri authorized elnumbez — only for in FAR 43 7 . new — EICAO P- L e-es-v,I$PECICa wolgiAlrlb`r- APR • 2 3 20O fraienie 4. Unit Identification 8. Type Unit Make j Model Serial No. Repair Alteration AIRFRAME X (As described in item 1 above) POWERPtANT .. PROPELLER APPLIANCE Type Manufacturer IL Conformity Statement A. Agency's Name and Address 8. Kind of Agency C. Certificate No. Keith Gawsyszawski Flight Options. Inc. 28180 Curtiss Wright Parkway Richmond Hts., OH 44143 X U.S. Certificated Mechanic AP 287603483 Foreign Certificated Mechanic Certificated Repair Station i Manufacturer D. I certify hereto have information Date April that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments been made in accordance with the requirements of Part 43 of the V.S. Federal Aviation Regulations and that the furnished herein is true and cermet to the best of my knowledge. 5, 2002 Signature of ' Individual a l 7:14•44. -q) 7. Approval for Return To Service Pursuant Administrator BY to the authority given persons specified below. the unit identified In item 4 was impeded in the manner prescrbed by the of the Federal Aviation Administration and is 00 APPROVED LI REJECTED FM Pt Standards Inspector Manufacturer gr. Inspection Authorization Other (Sped*, FM Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection Indy 4, Poo? nation Certificate or No. ifejt374.034,33,14 Signature ofrdividual a I MA Fa IV cow SONY_GM_02756309 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242231 EFTA01327349

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. 1 8. Description of Work Accomplished pf more space is required. attach additional sheets Identify with aircraft nationality and registration mark and date work completed I. 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 K Additional Sheets Are Attached 'Ll.S.GPO.1994-588-012100019 SDNY_GM_02755310 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242232 EFTA01327350

MAJOR REPAIR AND ALTERATION 0 U:S. Departnent (Airframe, Powerplant, Propeller, or Appliance) of bansportelon Fulani Agatha AdmIalentlan onn Approved OMB No. 21200020 For FAA Use Only Office MeMification J cc& 7 /49/ 4— 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 ivil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1058). I. Aircraft Make RAYTHEON AIRCRAFT Model 400A Serial No. RIC-244 Nationality and Registration Mark USA N793TA 2. Owner Name (As shown on registration certificate) KETTLER ROBERT, MICHELS PIPELINE CONSTRUCTION INC, SOUTHEASTERN MII,LS INC, REI AIR LLC, El-AL Maus (As shown on registration certificate) 101 S WEBB RD WICHITA ICS 67207-1315 3. For FAA Use Only 4. Unit Identifleadon S. Type Unit Make Model Said No. Repair Alteration AIRFRAME (As described In Item I above) X POWERPLANT PROPELLER APPLIANCE 'rape Manufacturer 6. Conformity Statement A. Agencts Name and Address B. Kind of Agency C. Certificate No. RAYTHEON AIRCRAFT SERVICES 1115 PAUL WILIUNS ROAD SAN ANTONIO TEXAS 78216 usCaracas:a Wavle CRS-XA14605K LIMITED AIRFRAME FonaseCerdneasedMechatie X Carer:mod Repos Sienna mamaceurer 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 nude in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulatio s and that the information famished herein is true and correct to the best of my Imowledge. Date 12-10-01 Siviature of Authorized Individual MONTY CARROLL /1.---C ---9 7. Approval for Return to Service 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 'n the manner prescribed by the 0 REJECTED El APPROVED FAA Flt. Standuds Inspector Manufacturer Inspection Authorization Other (Smelly) FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Grove Date of Approval or Rejection 12-10-01 Certificate or Daismation No. CRS-XA14605K Signature of Authorized Individual ye ir .: ,...._.?„ MONTY CARROLL FAA Form 337 (1248) SDNY_GM_02755311 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242233 EFTA01327351

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:nonspace is required attach additional skteu. Men* with aircraft nationality and registration mark and dale 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 FIREBLOCK1NG WAS ACCOMPLISHED IN ACCORDANCE WITH THE SKANDIA INC. TEST PLAN 48335 REV. IR DATED 12-04-01, REFERENCE THE FORM 8110-3 DATED 12-04-01 APPROVED BY DONNA J. PARRISH, DESIGNATED ENGINEERING REPRESENTATIVE, HDERY-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 48118 REV. IR. DATED 10-01-01 FOR P/N 8118-1 AND 8118-2 ONLY, APPROVED BY DONNA J. PARRISH, DESIGNATED ENGINEERING REPRESENTATIVE, IMERY-410100-CE, STRUCTURAL SPECIAL. END Additional Sheets Are Attached * US. GOVERNMENT HUNTING OFFICE: 1992-769412160157 SDNY_GM_02755312 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242234 EFTA01327352

Cr MAJOR REPAIR AND ALTERATION 01.ficurtentl (Airframe, Powerplant, Propeller, or Appliance) ol Trutuortatint Fettraihrtatice Adminittraara Form Approved OMB No.2120-0020 For FAA We Only Office kleMificatiat Is .5-'1 9 &- INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-I (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 ivil penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 19581 I. Aircraft 'Make RAYIHEON AEICRAFT Model 400A Serial No. MC-244 Nationality and Registration Mark USA N793TA 2- Owner Name (As:holm on registration certificate) RETTLER ROBERT, MICHELS PIPELINE CONSTRUCTION INC, SOUIREASTEItN MILLS INC, RE1 AIR LLC, ET-AL Address (As shown on registration certificate) 101 S WEBB RD WICHITA KS 67207-1315 3. For FAA Uso Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Altentio-i AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Par Manufacturer 6. Conformity Statement A. Agency's Name and Addrest B. Kind of Agency C. Certificate No. RAYTHEON AIRCRAFT SERVICES 1115 PAUL WIL1CINS ROAD SAN ANTONIO TEXAS 78216 U.S. Certificated Mechanic CRS4CA14605K LIMITED AIRFRAME RADIO CLASS 1,11, III Foreign Certificated Mechanic X Certificated RegokSrafioa Mazdaceate D. I certify that the repair and/or alteration nude to the unit( ) identified in item 4 above and described on the reverse or attachments hereto have been nude in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the infomution furnished herein is Mlle and correct to the best of my knowledite. Date 12-10.01 Signature of Authorized Individual MONTY CARROLL .-- 7. Approval for Return to Service BY Pursuant to the authority given perso s specified below, the unit identified Administrator of the Federal Aviation Administration and is in item 4 was inspected 'n the manner prescribed by the APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufactuner Inspection Authorization Other (Specify) FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Gmuo Date of Approval or Relation 12-10-01 Certificate or Designation No. CRS4CA14605K Signature of Authorized Individual MONTY CARROLL LW )e.e.r-arri FAA Form 337 OLIO SDNY_GM_02755313 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242235 EFTA01327353

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. S. Description of Work Accomplished Wince space is repine; attach addifional shags. Aka* with aircraft nationality and registration nark and date work completed) MAKE: RAYTHEON 400A S/N: 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 KAMALA J. MEADER, 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. IR DATED 12-05.01, REFERENCE THE FORM 8110-3 DATED 12-07-01 APPROVED BY ROBERT M. HURLEY, 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 Additional Sheets An Attached * US. GOVERNMENT PRINTING OFFICE: 1992.769-012/60W SDNY_GM_02755314 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242236 EFTA01327354

• • CO MAJOR REPAIR AND ALTERATION VS.Department (Airframe, Powerplant, Propeller, or Appliance) et Tonspotutlea Federal Astatba itendelstrallea orm Approved OMB Na 2120-0020 For FAA Use Only Office Ideoglication --5c-"/ 2 )42., 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 ivil penalty not to exceed 81,000 for each such violation (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) ICEITLER ROBERT, MICHELS PIPELINE CONSTRUCTION INC, SOUTHEASTERN MILLS INC, REt AIR LLC, ET-AL Address (As shown on registration certificate) 101 S WEBB RD WICHITA KS 67207-1315 3. For FAA Use 0 ly 4. Unit Identificadon S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described In Item I above) X POWERPLANT PROPELLER APPLIANCE Type 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. °vacua Mechanic CRS-XA14605K LIMITED AIRFRAME Fon* Catilkated Mechanic x Califtla Rep* Sudoo mmucra set D. 1 certify that the repair and/or alteration made to the twigs) 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 Imowledge. Data 12-10-01 Signature of Authorized bidividual MONTY CARROLL % 1 ce't 7. Approval for Return to Service BY Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is in item APPROVED 4 was inspected in the manner prescribed by the M REJECTED FAA FR- Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Medico 12-10-01 Certificate or Decimation No. CRS-XA14605K Signature of Authorized Individual " 1 .....4 40..27, MONTY CARROLL FAA Form 337 0240 SDNY_Gbl_0275531 5 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242237 EFTA01327355

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. S. Description of Work Accomplished (If mon space it royuirect attach additional shear. lan), with aircraft nationality and regtswation mark and dale work completed.) MAKE: RAYTHEON 400A SIN: RK-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. M. DATED 08-22-00, REFERENCE THE FORM 8110-3 DATED 12-07-01 APPROVED BY KAMALA J. MEADER, DESIGNATED ENGINEERING REPRESENTATIVE, IIDERT-405126-CE, STRUCTURAL. THE LIFE VEST CONTAINER WAS FABRICATED USING AAR COMPOSITES FLAT NOMEX PANEL PIN ATR-FP-25 I F2, REFERENCE THE FORM 8110-3 DATED 07-01-99 APPROVED BY JUDY BOGGS, 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 P01074-113. 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. ❑X Additional Sheets Are Attached * US. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 SDNY_Gtv1_02 75531 6 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242238 EFTA01327356

1 e MAJOR REPAIR AND ALTERATION US Ccpartronl of Tr-lun en (Airframe, Powerplant, Propeller, or Appliance) reden,Avation AderlMstran Form A OMB pproved No. 2120.0020'. For FAA Use Only S officeoisx.firgbo th".2. grv-2 INSTRUCTIONS: Print or typo 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 registra(ion certificate) AIRCAP LLC Address (As shown on registration certificate) 101 S WEBB RD WICHITA, KS 67207-1315 3. For FAA Use On y THE DATA IDENTIFIED HEREIN COMPLIES WITH APPUCAB AIRWORTHINESS REQUIREMENTS THE ABOVE DESCRIBED AIRCRAFT SU CT TQ C NFO INSPECTION BY A PERSON APR 0 4 2000 4 . AND IS APPROVED ONLY FOR AUTHORIZED IN FAR 43.7 DATE FAA INSPECTOR DPA-FSDO 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Rem 1 above) X POWERPLANT PROPELLER APPLIANCE Typo Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Elliott Aviation P. O. Box 100, Quad City Airport 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( ) 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. Dale 3/29/2000 Signature of orized Individual o tm 7. Approval fo etum to Signe Pursuant Administrator BY to the authority given of the Federal Aviation persons specified below, the unit Administration and is dentified in item 4 was inspected in the manner prescribed by the El REJECTED ix APPROVED FAA At. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Da e of Approval or Rejection f/9/ 690490 Certificate or De ignation No. CGHR812C Signature of rtzed,2ividual -.44:4,/, POP 00FtER FAA Form 337 nal* O SDNY_GM_02755317 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242239 EFTA01327357

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 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 2700-003-028 REV 0 DATED DECEMBER 19.1996. 3. PERFORMED EMI INTERFERENCE TEST IN ACCORDANCE WITH AC43.13-16 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) !MD 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 APPUCAPLE (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 FAA FORM 337 AND REVISED ICA. END Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 SDNY_GM_02755318 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242740 EFTA01327358

APR 2 1 law 0 MAJOR REPAIR AND ALTERATION us OVJOCKAI orrtheousisin (Airframe, Powerplant, Propeller, or Appliance) MITI Aviation athreaurmion Form Approved OMB No. 2120-0020 For FAA Use Only i. ce Ide)i5Gq-eiti — rPi'I - DO 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 Math N7S3TA 2. Owner Name (As shovm on registration certificate) AIRCAP LLC Address (As sham on registration certificate) 101 S WEBS RD 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. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Elliott Aviation P. O. Box 100, Quad City Airport Mollne, 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 US. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 4/14/00 Signalize Individual es,._,.....---__ . 7. Approval for R turn to Service- Pursuant Administrator BY to the authority given persons specified below. the unit dentilied in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and Is ig APPROVED 0 REJECTED FAA Fit Standards Inspector Manufacturer Inspection Authorization Other (Speuey) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 4/14/00 Certificate or Designation No. CGHR812C Signaturdicuthorized InclividuNa___ Ci ellP f , L crottaratereat FAA Form 337 time SDNY_GM_02755319 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_0024224 I EFTA01327359

ZrZZKCIO- 183 LT pue `ST `0T `6 `8 IL SHdV2IDVdVd 213C12:1O JA1.O11.Odd Ol1J3f8(1S OZESSL20INSANOS 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 work accomplished.) 400k RK-244, Nre3TA, 4/14/00 Removed all the interior and the cabinetry items to facilitate a complete refurbishment of the Interior per the customer's 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. D/L # 12777, REF 0 402396-402545. See the bum test report WO #45065-00 and the form 8110-3. Both dated 03/03/00 and approved by Judy boggs, D.E.R. #DERY 405020-CE, Structural special. Recovered the left and right hand drink ledge consoles with Rogers & Fabric. FRET #9103-05, Baroque, Treated at Skandia, REF treatment #SKFP41539. See the bum test report WO #46487- 00 and the FORM 8110-3, both dated 04-13-00 and approved by Judy Boggs, D.E.R. #DERY — 405020-CE structural special. Recovered both crew seats, seven cabin seats, the lavatory seat with leather Townsend leather: Leather, Classic pecan, Part #CL- 17, DA. #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. #405020-CE, structural special. The lower door panel aft side of the left hand partitlan and both game table inserts with leather Townsend Tiffany 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, grospolnt #440, beige, lot #8817-8824, treated at Skandia, Ref. Treatment #SKFP15268, see the bum test report WO#35268 dated 06-2499 and the form 8110-3 dated 07-16-99, both approved by Judy Boggs, 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 NO40669 carpet, color. ultra suede 034. See the bum test report #AIP stock and the form 8110-3 both dated 3-03-00 and approved by Carol Ann Watts, D.E.R. #50-572, 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 Cad F. Booth & Co. Waterfall Buginga Veneer., reference the bum test report #22702 dated 04-15-00 approved by Judy Boggs, D.E.R. ODERY405020-CE, for the flammability requirements. All seven cabin seats and the lavatory seat were frebloclo3d in accordance with FAR 25.853 (a) appendix F part 1(a) (1) (II) and FAR 25.85) (c) appendix F part II amendment 25-83. The flreblocking 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 Judy Boggs, D.E.R. #DERY-405020-CE, structural special. Reference the FAA Form 337 dated 04-14-00. Complied with AD 74-08-09 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. ENP fj Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA01327360

MAJOR REPAIR AND ALTERATION Form Approved OMB No. 2120-0020 UeDepartment (Airframe, Powerplant, Propeller, or Appliance) of Transportation For FAA Use Only • Federal Aviation AdmintstraUon Office Identification *me ) poug W01.)-61 INSTRUCTIONS: Print or typo 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 violation (Section 901 of Federal Aviation Ad of 1958). Make Raytheon Mode/ 400A 1. Aircraft Serial No. RK-244 Nationality and Registration Mark N42811R 2. Owner Name (As shown on registradon certificate) See Attached Copy Address (As shown on registration certificate) 101 S. Webb Rd. Wichita, KS 67201 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration described in Item I AIRFRAME (As above) X POWERPLANT t) ,..7. C.) Cli PROPELLER -L- i >—I C 'T APPLIANCE Type 0 " 0cn 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 descnbed 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 We and correct to the best of my knowledge. Date 03.06.00 Signature of Authorized Indivi ual . vim .— Oft/te e. /11 e led___ —\../A:' 7. Approval for Return To Service Pursuant o the authority given persons specified below, the unit identified in item 4 was Inspected in the manner proscribed by the Administrator of the Federal Aviation Administration and is G3 APPROVED 0 REJECTED FM Fit Standards Inspector Manufacturer X Inspection Authorization Other (Specify) BY FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 03-06-00 Certificate or Designation No. 454944057 Signature of Authorized Inclivklual f.ge..4.--filerjfie /.4 0( eet2 .7 .1 C orm 337 (1248) m TT/ :cr -17 SDNY_GM_02755321 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O242243 EFTA01327361

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 requited, attach additional sheets. Identity with aircraft nationaNty end registration mark and data wade 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 O Additional Sheets are Attached SDN Y_G1•1_02755322 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242244 EFTA01327362

ammo nam• •••mu O19MIWIT Or 19.0,14SPORIA1104-•EDEPA. STANDARD AIRWORTHINESS CERTIFICATE WAWA COA WEER ITIMESPORE mean+ Pawn cactmx1 , . cm. ~MN ••••••10101•Inerd 01000.4. b !TIM ••••••141. Tr. Palm .40.•••• Of SOP ••••••••••••••••••••6••••••••••••••••••••••00.•••••••••••••••••••••••a - Mae • TONSNOOTOINOS 1.10. Mee ••••••••• sena. most •• • ...11.0 OS • Ora.. MO..* 1. h/MYI. amnesia rowavao uut, CCM.° et ma oar or •0:0000•0 sisleflaUt att •••••••••••. osolmoS ••••••WONW.:•••• FAA Rona IllOO48se •4.1*.P.01110140411. CT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00242245 EFTA01327363

SDNY_CO.4_02756324 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00242246 EFTA01327364

. deem c. roweerrne-rtm••••ellOneelITOYMON ' STANDARD AIRWORTHINESS CERTIFICATE i' 4trtaxt".•." SHIM RATTIWAVINAVT MEANT ' ...=•"...s RK-244 "" ea" TRAIMP0RT 400A • "'hamSen." ••••• a •fts ••••• k. ..... 1•••••• es...a.... . ..• Won's. ..... .4.• • ••••••••••• W. wail .. mos Ina Oammin in buns. Cantos - ws. as Mr WOE • eeeceme to ernes *see ee e ...ere ee sew •• weer. ••• .04 woe eyes. se. ••••Onee 10-01-99 All i band ICIER CE-50115T „sett 'Pennon no. ow ?KATO May at Cana a I. hilOart retawart on. acatrilOWN. FAA Fmn111004 ow woe Ho. SDNY_GM_02755325 :T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00242247 EFTA01327365

! SONY_GM_02755326 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00242248 EFTA01327366

MAJOR REPAIR AND ALTERATION U.& Dmarestat (Airframe, Powerplant, Propeller, or Appliance) of Tralmortnee Federal Ashen Mahlstratko -Form Approved OMB No. 2120-0020 For FAA Use Only SW FSDO 17 0 47- Office Identification INSTRUCTIONS: Print or type all entries. See FAR 43.9, FM 43 Appendix B, and AC 43.9-1 (or subsequen revision thereog for instructions and disposition of this form. This report is remised by law (49 U.S.C. 1421). F Uwe 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 NaSonality and Registration Mark USA /442811R 2. owner Name (As shown on registration certificate) RAYTHEON AIRCRAFT COMPANY Address (As shown on registation Ce(tificete) PO BOX 85 WICHITA, KANSAS 67201-0085 3. For FAA Uso 0 Ty 4. Untt Identification S. Typo Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X PCMIEFtPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Nernst end Address B. Kind of Agency C. Certificate No. RAYTHEON AIRCRAFT SERVICES 1115 PAUL WHICINS ROAD SAN ANTONIO TEXAS 78216 U. S. CerMcatect Mechanic CRS-XA14605K LIMITED AIRFRAME RADIO CLASS MIMI Fccegn teak:Wed Mechanic X Ceruficated Repair Matte Manuteceng D. I testy that the repel, and/or alteration made to the un't(s) identified In item 4 above and described on the reverse or attachments hereto have been made in accordance with the recarkernants of Pad 43 of the U.S. Federal Aviation Regulation and that the information furnished herein is true and correct to the best o(my knowledge. Date 12-22-99 Signature of Authorized Individual MONTY CARROLL 7. Approval for Return to Service 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 D APPROVED 0 REJECTED FAA Ft Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee x Repair Simian Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 12-22-99 Certificate or Designation No. CRS-XA 14605K Signature of Authorized Individual MONTY CARROLL .n.---1- ac.r...ct loan Li (124a) SDNY_SM_02 755327 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242249 EFTA01327367

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 (gown space is required attach additional sham. Identify with aircraft nationally can Inglaration mark and date vont completed) MANE. RAYTHEON 400A S/N- RK-244 REG. N428FIR DATE: 12-72-99 INSTALLED AN ALLIEDSIGNAL FLITEFONE VI AIRBORNE RADIOTELEPHONE SYSTEM CONSISTING OF THE FOLLOWING EQUIPMENT'. MOD/MFG DESCRIPTION P/N WEIGHT ARM RT-18D REOTRANSMITIER W/RACK 400-0125-2000 7.8 47.8 WH-10 HANDSET 400-0123-112 1.5 1063 WH-10 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 NG76866 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. I 309 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. OFF 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- O Additional Sheets Are Attached * US. GOVERNMENT PRIMING OFFICE: I992-769412/60187 SDNY_GM_02755328 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242250 EFTA01327368

-"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 PIN I50-1364-000 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 WE 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. S. 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 43.13-16 CHAPTERS 4, 6, 7, IL AND 12, AND IN ACCORDANCE WITH AC 43.13-2A CHAPTERS 1, 2, 3, 11, AND 13. SDNY Glvl 02755329 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024225I EFTA01327369

SDNY_GM_02755330 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242252 EFTA01327370

...RAYTHEON AIRCRAFT SERVICES SAN ANTONIO, TX. PAGE 2 OF 2 DOCUMENT NO. PP VI-ICA-RK-244 DATE: 12-22-99 12. LIST OF SPECIAL TOOLS: SPECIAL TOOLS ARE NOT REQUIRED. 13. FOR COMMUTER CATEGORY AIRCRAFT: NOT APPLICABLE, THIS AIRCRAFT NOT COMMUTER CATEGORY AIRCRAFT a. ELECTRICAL LOADS: THE RAYTHEON AIRCRAFT SERVICES ELECTRICAL LOAD ANALYSIS DOCUMENT I REV. DATED AND THE RAYTHEON AIRCRAFT SERVICES EMI/FtFI 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 a 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. IL ASSISTANCE: NOT APPLICABLE. It 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 (Le. 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 135.4198. 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. SDNY_GIA_02755331 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242253 EFTA01327371

SDNY_GM_02755332 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242254 EFTA01327372

a e MAJOR REPAIR AND ALTERATION 'US Deturtmt (Airframe, Powerplant, Propeller, or Appliance) el liassaorlafill fault Mallon Mailed:Ma Form Approved OMB No. 2120-0020 For FAA Use Only Maw Identification oge SW FSDO 17 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (cc subsequent revision thereof) for Instetoons and disposibon of this form. This report is remieed by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 81.000 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 USA N42SHR 2. Owner Name (As shown on registration certificate) RAYTHEON AIRCRAFT COMPANY Address (As shown on regIsbstion certificate) PO BOX 85 WICHITA, KANSAS 67201.0085 3. For FAA Use Only 4. Unit Identification S. type Unit Make Model Serial No. Repak Alteration AIRFRAME (As described In Item I 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 IIIS PAUL WILKINS ROAD SAN ANTONIO TEXAS 78216 V.S. Certecarad Mechank CRS-XA1460$K LIMITED AIRFRAME RADIO CLASS 1,11,111 Foreign Caettarmad Mechanic X eertalleared Rena Staten Manufacturer D. I certify that the repair and/or alteration made to the w(s) identified In Item 4 above and desateed on the reverse or attachments hereto have been made In accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 12-22-99 I Signature of Authorized Individual MONTY CARROLL 7. Approval for Return to Service BY Pursuant to the authority given persons specified below, the unit identified in kern 4 was inspected in the manner press:abed by the Administrator of the Federal Aviation Administration and is El APPROVED 0 REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Seedy) FAA Designee )( Repair Station Person Approved by Transport Canada Mworthiness Group Date of App oval or Rejection 12-22-99 Certificate or Designation No, CRS-XA 14605K Signature of Authorized Individu I MONTY CARROLL / 2 1 FAA Form 337 (12.8$) SDNY_GM_02755333 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242255 EFTA01327373

NOTICE Weight and balance or operagng limitation changes shalt 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. S. Description of Work Accomplished Of mere space is required, attach additional sheets identify with aircraft netionaRy end registration mark and date stork completed.) MAKE: RAYTHEON 400A S/N- RK-244 REG. N428HR DATE- 12-T2-99 INSTALLED A SUNDSTRAND MK-VI GROUND PROXIMITY WARNING SYSTEM CONSISTING OF THE FOLLOWING EQUIPMENT: MOD/MFG DESCRIPTION P/N WEIGHT AM MIC-VI GPWS COMPUTER 965-0686-020 42 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 MSA3322SO 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-710I 37-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 PILOTS 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. Ern Q% Makin! Sheets Are Ma hod * US. GOVERNAGENT PRINTING OFFICE: 1992.769.012160157 SDNY_GM_02755334 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242256 EFTA01327374

%triad stem at 51rstrira Bepartment of Transportation —fiderol g.biation 2Idministration *uppiernental regpt Certificate Acmier S eerflecuseesehhsseei.e. Raytheon Aircraft Services, Inc. 3992 Aviation Circle Fulton County Airport-Brown Field Atlanta, Georgia 30336 .......0s,1/.2,4caftriazat /ta.darvfrihiScsrit,.-Za444vielselestwas .ndandat;,& .4(4.9.0.;ascryf-eanowsnat..dger edifeneakwas.enunta...99.4,ee 25 .924.0 . Federal Aviation SA3322SO AI 6SW : Beech wawa: ant gasavise4tle raAgar-dipar: Installation of a Sundstrand MK VI GEWan flCalthance with Jangar One. Drawing List No. 11892-GPWS, Rev. B, dated September 17, 1992, or lateriAA Approved revision. ...emagfasnecande.oaufr: 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, 1992, is a required part of this STC. Salecatioand2.4440,4or&rAret..dahaaa2.1.3:4 4Aalefatnta izza- noulaeciasaliantiaowsacc(nlennUtaz tv.acaserwaa.aanda4 , /÷1 ,CS..:vaerwirnja , StaahriveallervAandkalaam August 5, 1992 September 18, 1992 47 4 October 4, 1995 iSersocieeel: lae...012isetneheee/oss. (re,e, David P. OSt (SOnseort) Associate Manager, ACE-116A Athnta Aire ft Cerlifiestinn (Mee (MU) Any duration of this ter:Om& it punishable 87 o fine of not exetedusg 11,000, or impruorvnent not trending 3 yeas>. or both. This eta maybe tvensfersed in heeeniener with FAR 21.17. es,, e-alto-3O0-01) SDNY GM 02755335 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242257 EFTA01327375

.,. SDNY_GM_02755336 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242258 EFTA01327376

L_ 1-.11\ 11NV LIJ I DUG. LIST NO. 11892-GPWS DATE 9/1/92 REV. D DATE 3/22/93 e ET 1 OF 1 SYSTEM SUNDSTRAND MK-VI GPWS . AIRCRAFT TYPE BEECHJET 400E F.A.A. PROJECT NO.CE-115A-2970 STC SR 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 SIAISTANIATION REPORT OPUS AFMS B 3/22/93 AIRPLANE FLIGHT MANUAL SUPPLEMENT 6 060-3942 6/92 INSTALLATION DESIGN GUIDE 11892-2 A 3/22/93 INSTALLATION PROCEDURES 11892-3 A 3/22/93 mom 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 omsoo MINTING NAM 11 -8 8-29-92 SUPPORT !RACKET 892-1 A 3/22/93 GROUND TEST nwamuters 060-3956-000 D 9/17/92 FLIGHT TEST nmommums 500-8000-RO 8/29/92 DESIGN SPECIFICATIONS ADC-S00 SDNYGivl_02755337 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242259 EFTA01327377

SDNY_GM_02755338 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242260 EFTA01327378

US DEPARTMENT OF TRANSPORTATION FEDERAL AVIATIONADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 11/23/99 A/RCRAFT OR AIRCRAFT COMPONENT IDEITIRCATION MAKE Beech MODEL NO. 400A TYPE Muyin•AsAafflamplm elci Airplane NAME OF APPUCAfif Raytheon Aircraft Services UST OF DATA — moinsicAncea TITLE Raytheon Dressings RAS-67-9917 Rev IR Dated 11/05/99 Sundstrand Mk-VI Ground PrOXfftlity Warning Sys Note: This approval is for the Electrical aspects of the engineering design data only, and is not instaltabon approval. Approval tor aircraft S/Isi RK-244 only. Approval for GPWS is for only the minor deviations TO FM STC SA33225O. After modification is complete, perform EMI/RFI test in accordance with Raytheon report • RAS-GF-9714, EMURFI Test Procedure. PURPOSE OF DATA In support of a modification to install a GPWS in serial number RK-244. APPUCABLEREOUIREAtENTLAArspomkseassAl FAR 25.1301 a,b,c FAR 25.1359 d FAR 25.1431 0 CERTIFICATION - Under sighodzy vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Pan 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered None have been examined in accordance with established procedures and found to comply vischipplicable requimnans of the Pedaulavenion 1 Ng mat • El Reguarans. FtecercrxrA approval of these data Approve that dam SIONATURE(51 OF DESiGMTED Es43sEERna REPRESS:IAD/EIS) J DESMATION IAPMERS/S) CLASSIFICANONt61 • a fem"kter wtra-'.t.;. • •' . :! /; DERT-710137-SW Systems Ei Equipment Robert M. Hurley FM Form 8110-3 MI•70911LPNECES Parana EOMON 11-23-99 13:55 C4 90)- RECEIVED FROM:512 989-2998 P.93 SDNY GM 02755339 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15-, and 17 EFTA_00242261 EFTA01327379

SDNY_GM_02755340 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242262 EFTA01327380

Form APPreed 0 IA 0. No. 21204003 0 . APPLICATION FOR US Descreral AIRWORTHINESS a Tax0alcoan CERTIFICATE Federal ANollon Aerdeinrcrtion INSTRUCTIONS .. Print or type. 00 nol sidle In shaded area these WO XX FM use only. Submit ortinal Webs:in autlxdrod FM Represent:1MT If EIRDanal Komi, requTed. use an anachrnent. For special 013,4 Porrnia complete STORns X and VI of VII as apPkalle r I. AIRCROT DESCRIPTION I.REGISTRATION MAFIA N421114R 2AIRCFlAFT Rn.DERS NAVE (Afala) RAYTHEON AIRCRAFT COMPANY I ARC-RAPTMOM DESIGNATION 400A AYR MFR 1996 FAA BODING 2/ 45—. O.O 1 0 S. AECRAFT XCOLLI NO. RK-244 S. ENGINE BUILDERS NAME (AIMS) Pratt & Whitney Canada 7. ENGINE MOCEL DESIGNATION JT1SOS 5 /PS 8. NUMBER OF ENGINES 2 0. PROPELLER 13011.00TS NAME (Mho WA IE.PROPELLERMODEL DESIGNATION WA 11. AuTcRAFT is mrsostarepoteow !wee U. CERTIFICATION REQUESTED APPLICATION IS HEREBY MADE FOR : (Cnedeappfeatat Aron) A 1 X STANDARD AIRWORTHINESS CERTFICATE Einette eittgay, I 'NOM/ALI I Vnurr I 'Annan-on I zInvessnonT I I gum I lomat B SPECIAL AINNORT1w4F-SSCERTIRCATE (CANA approdete Nem) 2 URNS) 6 1 CLASS I PROVISIONAL (Manus don) 2 CLASS II I AGRICULTUREAPOPEST CONTROL 2 AERIAL SURVEYING 3 AERIAL ADVERTISNG 3 RESTRICTED leascateRstrOanOn0 Ns cone-NINO 4 FOREST OSTognons•A•fited 6 PATROLLING 6 WEATHERCONTROL 7 CARRIAGE OF CARGO 0 CYMER(Speoly) EXPEFoNE /RM. Ondaree epraNWO 1 RESEARCH AND DEVELOPMENT 2 AMATEUR WET 3 MORN 4 to be moducIA0 4 RACING 6 CREW IRONS Mier. SURVEY 0 TO SNOWCOMPLIANCE WITH FAR 1 FERRY FO3HT FOR REPOS ALREFIATI3NS. MAINIENANCE OR STORAGE B SPECIAL FLIGHT PERWr (Inianam caerseion naicial. P4n 2 EVACUATEFROMAREAOF IMPENDING DANGER coasstfo Sasebo Se of MTN ewers. 22,1 3 OPEARON RelECCESS OF IANuMUM CERTIFICATEDTAREOFF WEIGHT WPArabto on 4 DEL NERING OR EXPORT ISI Innomenon maw ntsmen s CUSTOMER DELIONSIPATRXIFLWITS C IS I, IMATIME AIRWORTHINESSCERTIFICATEraw* ABOVE 'Restricted Opetaabn'and Vatelartf or tented.'as epAYNN) § ...0 a V A- REGISTERED 01*ER (As Yawl on ordeceleol Ave fegrstratko) IF DEALER. DECK HERE ----IP I X NAYS RAYTHEON AIRCRAFT COMPANY ADDRESS P.O. BOX 66 WICHITA. KS 67201 B. AIRCRAFT CERTIFICATION BASIS (CMS( sppitate btcAs and ootAvtres 422s as ireSaMm0 x AIRCRAFT SPECAICATION OR TYPE CERTIFICATE DATA SHEET (GM No. . .,Rinislottho.) A16SW, Retie X AULRORTHiNEsS EXAMINES ION AD No.) ISSUE (CON cif a1scphable s coma*. 2At "li Andipve 99-20 AIRCRAFT LISTaNG SW Pape amarLerOn WA SUPPLEMENTAL 019E CERTIFICATE N/A ((Al number 0(nch STGInecepor222, C.NRCRAFT OPERATION MO MAINTENANCE RECORDS X (PECK IF RECORDS IN comptIANCE WTI FAR 91.4n... 417 TOTAL AIRFRAME HOURS 6:40 S EAFERNENTAL ',ze ONLY WAY/fan lb.., rho Ma resole et renewed) NIA . 0. CUMF1CATION — I hereby cosh, Oat am the regalefed **net (ce Ns awe) Cl the fl oe Cencnbed above; Dal the arca/ Ad-r.nnuaten In DCON.W.C. ral Sedlon A dine Federal AVerion Ad of Ma. and aceioNe Fed.* Amer Re3Alltns: anl aiesonhy vad tootle fee PS alrealhheSS (enflame requested. is regMenal et' the Federal /Magee tea the arra has been leapecead and is DATE OF APPLICATION yNATURE 10.01.09 Eugene Hainstook — AdngnIstratIve Staff OA 144'4 '4. i 2 2 A. THE AIRCRAFT DESCRIBED ABOVE HAS SEEN INSPECTED AND FOLINCIAIRWORINY BY: (Cavan. It Saran AR 25.122(2) 4*On) 2 FAR MCCate i6b PART 121 OR CERTIFICATE MOILER So CO .) IV 3 No ft 0 MECHANIC Sme Certitale ) 6 CERTIFICATED REPAIR STATION (Give Camera No.) AIRCRAFT MARVSACITAXER (GM. nag* el fan) OA TIRE $()W41.111£ gz a /i.:: c •Ii SON ALL apetrahte beds in items A end B) X THE CERTIFICATE REQUESTED AI End tot Is. Worse deputed h Scorn I NMI meets iewiretnents la: 4 AMENONENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE B. InspedIon IN a special point under Section VI FAA INSPECTOR FM DESIGNEE was concluded by: CERTIFCATE HOLDER UNDER: I FAROS! VAR 121.127 OR 135 I I FAR 146 DATE 1041.99 DISTRICT OFFICE CE.41 4 DESIGNEES SI TURE AMD NO. i is_ Robert Alliband, OMIR CE-501157 s FAAINSPECTORSSIGNATURE GP0:1909-241-67244013 SDNY_GIN_02755341 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242263 EFTA01327381

X speo.vgignanx ROAM uystotol gill 'A X VIII. AIRWORTHINESS DOCUMENTATION (FAA use only) (MOW Mo3) WV mot ileuepsxoy ui Doren IiicogrW3 ilautscrAxy panY3 t (pLyntsat upon smoral ot •WO4 'YAW/eon We Accra 0 X45 wavy 4 41144sty 0:4004/4 aoutle0 Oa ItAaMtva0,0 0 X OmPnv MVO WO Ind gen axtegamoV LI Poorg *lemur) enwankury %flotsam 1 Waintai unaingflY), 14 vv:Itgolcqd twang] seln3 3 fiNwtad vac...I weal lIcliV IxatI a uogrOgpio ter.tgoom.ty oatanj .g Par" IOOPIPLITI OuSado) mum g opitgatI SS ITIVI6 e if trfd 0..."44001014054110111414446400 Otigmado v X 0 X U*41 WOK WOW 11-009 IWOJ WA Arnow= p gWaSSIS V MillIVIIEIS tadg io MO 3110.04V 3ViVN 31V0 VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER TITAN PRODUCTION FUGHT TEST Pfilicia9 1150 ab .31 haiwve g pvI POSSRSRS USN SRI Leone ay IM Pm :wrietneeti 01444 moped age:00 Cor 13561PPV "“ue le-0943 OWI p lOS LC,PoS 41.1 Comp.:00g ki, vog fawn um,,,,, Kam, 0,0 Lg. pamsgaiggrjungung :smogs pagaenap iesue ova p Ovid. sy PS Aiwa pasta/ sal me I Ina /41,0 AWN I— NOUVOCittli33 'A fkersrntopmituipage ern/ NOILYa3d0 305 801 MYSS303,. OPAOSNO3 OW 5Ni:410.1)115,1f ONIMOTIOJ SRL 3 WA0110JSV gibl3VINICIQT,ISS3.011UOMIIIV3XECI1,103:1111331110>4 S300 1.14108P/ SW V (40,149) t014101 I tairattortil I soikroal i loval 1X3.14.103$11 OW 1.4YMAYINI. 30/4340 01031110034 /QC* Nouvano WM 3liglINdig VIA 01 rioat ialgiztOdeN VOCC) O 51140114 lialVaISNON301131<015110 .1110114 1014044210S30 0 )001114011411110/311 1103141014MaS 11000 (,1Wni) to011ne 9031000V WM/0 0303151038 1.1VbOUIV JO Naldni3S30 V i•i nr:lil Oa•• 1,3 me.)31111 OW 3)W14 NOUV011edV 3031W VI. PRODUCTION FLIGHT TESTOtO . . I 5033110140011340110403410034 51143101033 30 A1114400 3.10 -3 4 431SASI101133aNI HC113flOOtld 03A01.1ddY AlN0 31V3IiI1203 9d&I. /44nnto 44000:0 0:4101C.d040131•10110/133 P3110600Ild (urn, Mond* *ma USW NOLLIn0Otkl 13 553103V WeIN tranntavinrmi v SDNY_GM_02755342 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242264 EFTA01327382

gnaw Po late •Zitfoo DIPORDAPOI OS TOWISOCINTATOINI—ttelitAlMMTION AOSSTMATC•I STANDARD AIRWORTHINESS CERTIRCATE 7=-14-th- Tikti"AritcTh «wpm 11428111 400A S - a . y e W s s o , - - - - - a a 00 •••••••••• MN.. a Os • • ea lea* ••••••••/••••• ••••••••••••• •••••••••• • •••••••••••••••••••••• 000•••• ••••••••••••• olonno RE-244 GOMM TRANSPORT NONE • Tr rmc,or tons 10-01-99 Robert All Nand R LE-soup *et Or etakOt loa•SWILNINIAlwa t SIM 0 104 ton *.t 0011tairt whir al cartaotO to not •400.0.11 AIX•YON•Cl SRO.* MOW 41* FM Penn nos* ea SONY GM 02755343 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00242265 EFTA01327383

SONY_GM_02755,144 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00242266 EFTA01327384

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1. E. trEIraannat,,, =tons kern Fatuniairo 24-0078 AUTHORIZED RELEASE CERTIFICATE • BON DE SORTIE A UTORISE • 3 Comeau Rd Pio • Pe de ,Hasa a ton SEE BLOCK S • 5 auk OrtielCounanuena • ea a Paaranuateaaae 1000 :t & Whitney Canada Longueuil, MarioNiNotin Blvd. Quebec MG 1A1 P.0.19000016693 .....................,.............c.-.... I Pan Re • N• 0 ana I Dobai • Idematai • • On -Oil II. SealSaras No -NI a daft it SlalvilWoli• Wawa FREE TURBINE 3030100 VARIOUS I PCE-3A0257 MANUFACTURED TURBOFAN n -ISO-s .PPROVAL &IL FAA TYPE CERTTFICATE DMA- OEMS TO ITS UNITED STATES TYPE DESIGN (TYPE CERT/MATE NUMBER IOSEA) AND IS IN CONDMON FOR SAFE OPERATION. 3MN SUBJECTED BY THE MANUFACTURER TO A FINAL OPERATION CHECK AND IS IN A PROPER STATE OF AtRWORTHINESS. -ts: Ave* MOON WI Ii Used Pall. Ihecei .3100 . CAR Ste 10- Lananane Rana MOAK Duda WI MC 571 10 - Camleann arts ma nleaMO 014,3e0 /1100. *UP SS Iasi Wee pet • Peal Mad* dal/WI aftliA °Ana nal nenurnefence steed.. eteor• enter. Nett Call* as Is amIlowee naca• oaut • ME xi. 13. itn Inale) teal sat la abeam. want &Una IA • MORO Marna nab:04n *eh the no -ate. liana*, *tale CONNNONeN i• Nene* ea ••••••01 • a***** 1 •as LW oc.n.00.Y.WeattRI teo:oratinat *Modes at Ci .....oennns Enna as Nanny second n enn a:04%qm Sa0 ',ay y ....mg ioN,1* ale an we II In aannan canna. sandal, n aa IRPRAIRIERI Anna , 111M Win n WI) Nitase0 IN se**. Ii Deflate* fen*, « la tItilattO) *tram** nal thi pin n0405 K am It AroNNWReL NA -Rd anskInalan 20 Scare/ 21 Iona* An No- RN d'eslarisates I 00f APPROVAL • • LSI .110.015 • Non It Con 22 Pune main Waal - Mon Inuntinift• a /neat/ 73. Cade LERICHE MAY 19 1999 Muni sea tens eel 'Annie was aprAtty Rana. CaIl• Le inane Oall nInia taatainne encl.f anaa Rancats pennants USEPANSTALLER RESPONSENUTIES RESPONSABILITES DE L'USAUER/LIONTEUR I Val is. fallen**, MS aboard Nem 03ka all hulNeeNca• CeManAt 3.000/ AS n aceentprea was Wnageal re*eiton Of N ANwereeen ANINNte aninni visa a 3* “Nete •PIC•14 *MO 1 a O. awe.' you 14 ***sun. C÷4ta. ful max Ns *VbacencemeNtattenbles evn the A/kW...Natl.} AW0.0 tint (wetly laded r. conUst* enbeaX*Ceiticata Mal Cal. w. *teat lone* (*NW*** Nan * int*** C.I.C414), 111403 n 14:CPCIACC Wei en annal repta** et ex 'II be re.* • I eal ter ocul a ben beepesto pa ea pal ion Osil.)ette a 4030atal ae was** pas ler*Nenl etAbleitc•Oretaear k NeeteetecessnUtmantte. Innve enagamperanclend Panda eentemine1 an olstemerts nslesso tam aaara 4WD:a are e•tol* a AnvaTtnn nude • LI tea 1, I 1114 tIMItoll pre 1143(gtenCoNstleas• *mu* cpa to wan ea Anna...* wane lee sItabbanpasanamentIts ea Innen/ oe S•IP•91W41.140. • Inas. e. In Ciabul.C* appwasnat an eon 14 all a=rms** pas we nankeen a met** Ea La teen k Paw NOV** a rattnel 031 mane cm cantata* aNes (*.sunsets Emse seen be naltatens wY4nNa. al ••••••routerieuse). an**. 14410141t*Sle 0103.1* SON Y_Gfvf_02755346 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242268 EFTA01327386