0 MAJOR REPAIR AND ALTERATION ILE- DtPD4449191. (Airframe, Powerplant, Propeller, or Appliance) Transportation • Federal Aviation Administration - Forts, Approved OMB No. 2120.0020 For FAA Use Only Office Montifuntion / 5 6... rt• 49 -10-... •9 / INSTRUCTIONS: Print a all entries. See FAR 43.9, FAR 43 Ardis B, and AC.43.9. I (or subsequent revision thereof for instniaions and deposition *Antis form This report is requ law (49 U.S.C. 142 I), Failure to repo rota in anion penalty not to exceed $1,000 for rucksack violation (Section 901 Federal Aviation At of I9$4 I. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N505LS 2. Owner Name (As shown on registration certificate) NORTHWEST DELAWARE CORP Address (as Amon on registration certificate) 1105 N. MARKET ST WILMINGTON DE 19899 • 3. For FAA Use Only 4. Unit Identification S. Type Unit Make I Model _I Serial No. . Repair Alteration AIRFRAME --- (As deseribed in ikon I above) ••---•-•----•—••-- XX POWERPLANT PROPELLER APPLIANCE 1.4' ' 4 Manufacturer 6. Conformity Statement A. AgeneYs Name and Address R Kind of Agency C. Catifrcate Na TIMCO . Lake City Municipal Airport Lake City, FL 32025 US. Certificated Mechanic DU4R141M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. Irani& that the repair and/or alteration made to the units identified in item 4 above and dmaibed on the raven* or attachments hereto have been made in accordance with requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information Punished herein is true and carat to the beta of my knowledge. Date August 23, 1999 Signature of Authorized Individual Arthur E. Saylor 7. Approval for Return To seniadlit4e ce Pursuant Administrator BY to the authority given persons specified below, the unit identified in item of the Federal Aviation Administration and is El APPROVED 4 was inspected in the manner prescribed by the REJECTED • FAA Flt. Standards Inspector Manufactora Inspection Authorization Other (Spann.) FAA Daiftwe X Repair Station Person *woad by Tampon Canada Ainnethintss Group Date of Approval or Rejection August 23, 1999 Certificate or De:0vation No. DU4R141M Signature of Scott L. Authorized ividest Palm FAA Form 337 (12-88) This 337 supersedes 337 dated August 7, 1999 SDNY_GM_02759847 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246769 EFTA01331232

NOTICE j freight 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 Of more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) Boeing 727-31 Reg. No. N505LS S/N 20015 August 23, 1999 Page 1 The following major repairs were accomplished: I. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 56 IAW TIMCO E.O. 99-1190 Rev. PR dated 12 JUL 99 Approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delmainated skin above #2 engine pylon L/H side at stations 1342.4, I371.5 and 1387.85 IAW TIMCO E.O. 99-1191 Rev. lilt dated 23 Jul 99 approved per FAA Form 8110-3 by DER D. Joynes DER #DERY-635317-NM dated 21 July 99. 3. 060H I-0027 Repaired cracked and disbonded #2 engine upper skin on aft fairing assembly IAW ROHR Engineering Repair Data Sheet and FAA Form 8110-3 by DER Jeffrey D. Shutrump DER #DERY-605526-NM dated August 3, 1999. SUMMARY 1. All work accomplished IAW TIMCO E.O.'s, ROHR Engineering Repair Data Sheet and FAA Form 8110-3's. 2. Records of all work accomplished is on file at this repair station under work order 060/T-361. --end- 0 Additional Sheets Are Attached us.00wormarridonnia onyx ien.resoivout SDNY_GM_02759848 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246770 EFTA01331233

ft) MAJOR REPAIR AND ALTERATION US. Depannum of (Airframe, Powerplant, Propeller, or Appliance) Transportation e Federal Aviation Admbdstradon Pam Approved monk. 21204020 For FAA Use Only Office Identification .4OO'—ear 7/ INSTRUCTIONS: Print r twee all nitrite See FAR 43.9, FAR 43 midix B sad AC.43.9.I (or subsequent revision thtreof for inskucticas and ffisporaion °PM form. This repro is requiredby Mae (49 U.S.C. 1421). Endure to rep m tan In 4 C1•11 penalty nee to exceed 11,000 for esch such violation (Section 901 Federal Aviation Act of ISIS) I. Aircraft Make Boeing Model 727-31 Said No. 20115 Nationality and Registration Mask N505LS 2. owner Name (As shown on regittration«rtificato) NORTHWEST DELAWARE CORP Address (u shown on registration cobra:ate) 1105 N. MARKET ST WILMINGTON DE 19899 3. For FAA Um Only 4. Unit Identification 5. Type - Unit Make Model I Serial No. Repair Alteration AIRFRAME XX GU described titan I above) POWERPLANT PROPELLER APPLIANCE TY,. Manufacturer 6. Conformity Statement A. Agway's Name and Addams B. Kind of Agency C. Certificate No. TIMCO • Lake City Municipal Airport Lake City, FL 32025 US. Certificated Mechanic DU4R141M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair ancVor alteration made to the units identified in item 4 above and desaibed on the male or attachments hereto have been made in moord.uwe with requirements of Rut 43 of the V.S. Federal Aviation Regulations and Out the information famished herein is we and coirect to tiro tent of my anossIcdgc. Dale August 7, 1999 Signature otAuthorized Gregory A Christman,/ FTh 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 prescribed by the of the Federal Aviation Administration and is Z APPROVED O REJECTED FAA Fit Standards inspector Manufacturer . Impaction Anthorization Other (SpeeiM FAA Designee X Repair Station Person Approved by TransprtCuada Airworthiness Ciro Dale of Approval or Rejection August 7, 1999 Certificate or Daignation Nn DU4R141M Signature of ottL am FAA Form 337 (12-88) SDNY_Gh4_02759849 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EF1'A_00246771 EFTA01331234

. 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 confonnisy with the applicable airworthiness requirements. S. Description of Work Accomplished (If more spaces required, attach additional sheets. Identify with aircraft nationality and registration mask and date work completed.) Boeing 727-31 Reg. No. N505LS S/N 20115 August 7, 1999 Page 1 The following major repairs were accomplished: I. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 45.5 TAW TIMCO E.O. 99-1190 Rev. PR dated 12 JUL 99 approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delaminated skin above #2 engine pylon L/H side at stations 1342.4, 1371.5 and 1387.85 JAW TIMCO E.O. 99-1191 Rev. YR dated 23 Jul 99 approved per FAA form 8110-3 by DER D. Jaynes DER #DRRY-635317-NM dated 21 July 99. 3. 060H1-0027 Repaired cracked and disbanded #2 engine upper skin on aft fairing assembly JAW ROHR Engineering Repair Data Sheetand FAA Form 8110-3 by DER Jeffrey D. Shutrump DER #DERY-605526-NM dated August 3, 1999. SUMMARY 1. All work accomplished TAW TIMCO E.O.'s , ROHA Engineering Repair Data Sheet and FAA Form 8110-3's. 2. Records of all work accomplished are on file at this repair station under work order 060/T361. end El Additional Sheets Are Attached * us. oovaionrirrinterremoenct IM449419,40U7 SDNY_GM_02759850 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246772 EFTA01331235

1u1.21. 1999, 22:06 PDT MegNum': CPZ-LR1C-99-00014H Page 2 of 2 67/Z1/99 RED IS :08 FAX 9 @Oat U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE ZZL.1 tic; 159C AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727 TYPE Glirydone, Radio. Heliconer. err.) Airplane NAME OF APPLICANT • Boeing Commercial Airplane Group LIST OF DATA IDENTIFICATION TITLE. • • CPZ-LRier89.0204-'112 Dated-9.1cl 1999 - ' CM-Lk/09-00006H Dated- /21u1.1999 • ' . • CS...ER(699-0208TR .. Dated 191ul f999 ' . . — . . . Subject Center Engine Support Side Panel Corrosion, Deb/ideation Requestor: 'HMCO (CP2) for The Limited (LH) Part Number/Serial Number. 65-17556 Model No.: 727-100 Serial No.: 20115 Basic No.: E22I8 Registry No.: N50014 Variable No.: E3704 Line No.: 735 Flight Cycles: 21643 Howl: 31835 Service Bulletin/AD: N/A . . • • . . 'HMCO telex with description of blindant end doubler repairs to corrosion and • deltunination areas at Station* /3711S: 13S7:85, and 1342.4. " Boeing reply that repairs aiditeuthiall)lideaciey With preiyefions. ...,. • : - ' ''•••• -.?.t• c. '. v. .. • ' . • . :•1Th4C0 telex witlisiaiemehtiliatiepafeliisi ()tea ChiliPleeeei Pei disieltition•aisitresjMesi' ' - ' • ' for form. • • • • . . ., . ; . ' • • PURPOSE OF DATA Structural Substantiation of Repair Plan • APPUCABLEREOUIREMENTS (List spec* naiatu) CAR 4b • Subpart C: 46200 through 46.202, 41).270 Subpart D 46.300 through 4b.304(a),46.306(a)44(b) tEFITIRCATION - Hofer of appoimment under Part 183 i have authority vested by (Erection of the Atbrdnistralor and In accordance with.condldoac of the Federal Regulations, data listed above and on attached sheets numbered been Guunined in accordancewith esmblished procedures and fouod to comply Regulations. Recommend approval of these data Approve these data and limitarions with applicable requirements of the Peden° Aviation I We) Tterefore O . elf SIGNATURFIs) OF DESIGNATED ENGIN NG FtEPRESENTATIVE(s) DESIGNATION NUMBER(s) CLASSIFICATION(s) 1). Joyner . DERY-635317-NM Structures FAA Form Form 81103 1-70) SUPERSEDES PREVIOUS EDITION Page 1 of SDNY_GM_02759551 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246773 EFTA01331236

SDNY_GM_02759852 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246774 EFTA01331237

07/15/89 15:54 FAX TURCO ENGINEERING • LAKE CITY Q002 US. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE July 12, 1999 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. . 727 TYPE (S7Fanas Rada HaFxtder. eta) Airplane NAME OF AppucANT TIMCO LIST OF DATA TIMCO E.O. 99-1190, Rev. l/R, Dated 12 JUL 99 TIMCO REPORT NO. S.A. 99-1190. Rev. VR, Dated 12 JULY 99 B727; SEAT TRACK: STATION 662. ROL 56 CORROSION BLENDOUT REPAIR. STRESS ANALYSIS; SEAT TRACK CORROSION REPAIR AT STA 663 RBL 54 END • NOTES: 1. This approval is for Northwest Delaware aircraft N505LS, S/N 20115 only. PURPOSE OF OATH In support of a Major Repair accomplished on aircraft S/N 20115. This approval is for design and static analysis only and is not Installation approval. APPLICABLE REQUIREMENTS rya *sae satiorte) FAR 25.301. 25.305, 25.601, 25.603, 25.605. 25.609 and 26.613. CERTIFICATION - Under authority vested by direction of dm Adrrirlistralce Part NM of the Federal Won Regulations. data Wad above and an wilt; estabeshed procedures and rend to comply van applicable requirements 0 Recommend approval adieu data I pm Planta* 0 Approve Mese data and In at:Cadence with conditions and Seed shoals numbered WA nave Ernitadcos ciappOintrnant inlet been examined In accordance • of Um Federal Aviation Reputations. MOROI/REM OF DESIGNATED EN&MEERING REPRESENTATIVE) DESIGNATIONsnatasts(al CLASSIFICATION(S) ti -)C3-- Wayne Fink DERT-510117-CE STRUCTURES en A Can.. 1111&L1 /.1.2.110i beaten ELECTRONIC FORMAT (449) SCNT_GM_02759853 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246775 EFTA01331238

SDNY_GM_02759854 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246776 EFTA01331239

a- J-UK 4.00 F$ ;bliedli. Z1 FKUUKAM 2/ U.S. DEPARTMENT OF TRANSPORTATION . FEDERAL AVIATION ADMINISTFtATiON STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE August 3, 1999 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727 _ TYPE (4apitme. Radio. lielicopeas dm) Airplane NAME OF APPLICANT Rohr, Inc. LIST OF DATA IDENTIFICATION TITLE ERDS Cl 036 dated August 3, 1999 -. B.. Cox Stress Analysis Dated August 3, 1999 • • Engineering Repair Data Sheet, Definition of discrepancy and VA545300-1 (AR Skin - Upper Skin Assembly) . Skin Disband VA545300-1 (Ref. ERDS C1036) repair design for P/N PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. APPLICABLE REQUIREMENTS (Ubisstific scams) (1) FAR 25.301 (1) FAR 25.307(a) (1) FAR 25.605(a) (1) FAR 25.619 (1) FAR 25.303 . (1) FAR 25.801(a) (1) FAR 25.609(a) (1) FAR 25.305(a)(b) (1) FAR 25.603 (1) FAR 25.613(a)-(d) .; • CERTIFICATION — Under authority appointment under Part 183 of Me NONE have been vested by direction of Pedant Aviation Regulations, examinee in accordance Regulations. ❑Recommend approval the Administrator and in accordance with conditions and limitations of data listed above and on attached sheets numbered with established procedures and found to comply with appreable of these data • requirements of the Fedaml Aviation I (We) Therefore Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING E ENTATNES DESIGNATION NUmeen(3) CLASMFICKnON(S) Structures (1) Jeffrey D.Shutrump DERY-805628-NM FAA onn 8110 11-70) SUPERSEDES PREVIOUS EDITION (rammer Serlostad try Rohr. inc.) SDNY_GM_02759855 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246777 EFTA01331240

SDNY_GM_02759856 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246778 EFTA01331241

RC/IMMO. ' ENGINEERING REPAIR DATA SHEET (ERDS) FORM 81103 REQUIRED cuiss Dux* M- al WSW. ci 036 PEV. PACE I OF 2 nIr n nu n tisnagantom Odavict.catirca otIn • me en ra WA REV. PART NO. VA545300-1 `.ART SERIAL NO. N/A SCOEL V727RE r liT kPONt AFT FAIRING -UPPER SKIN ASSY sERVCCE /CURS UNK S CUTOMER THE LIMITED REPAIR: OISCFtEPANCY: (8E SPEOFIC • PR WT CLEARLY) ITEM A. Repar. ITEM A. The upper skin on the AFT faring assembly, PIN .MA545300-1, on the #1 Engine position shows a disbonded UPPER SKIN REPAIR condition on approxknately 50% of the AFT surface, Including 1. Remove discrepant upper skh from any. Care should be two crescent shaged cracks on an existing repair (fiben2lass?). taken not to disband the lower skin of the easy. On this same are'on the lower surface of the panel, an area of 2. Fabricate anew upper skin from .032 gauge 202443 per QQ- material is also missing and fated as above. The lower reps& A-250/5. stops before transitioning to pan down of honeycomb. 3. Remove lower surface Clad (bonding side). Do not thin below See page 2 for sketch of location and description. .029. 4. Make sure all remaining "old" adhesive Is removed from core. MATERIALS: Clean and prep sldn (using PM or Pasa-Jefl 105) and exposed Upper Skin .032 2024-T3 CIO-A-250/5 core (using Pasa-Jell 105) on panel. Clean repair area per 727' Lower Skin .016 2024-0 QQ-A-250/5 SRM 51-40-6, Par. G(2) (SRM 5140-5). Heat treated to —T42 per MIL-H-6088 5. Pane bond side of skin and core with BR-127 adhesive Honeycomb .3103/16-10(5052) MIL-C-7438 primer, per manufacturer specifications. 6. Apply two coats of FM-73 adhesive material, per manufacturer specifications. 7. Bond replacement upper skin to core and tower skin per 727 SRM 51.40-6, paragraphs E, J & K 8. Perform Post Bond inspection by visually Inspection of periphery for evidence of adhesive bead, and tap test the whole panel for voids. ORnitiGailtaiAl annals' Is land Ink IP CW I 'REPASS) SY DATE AIRWORTKNESS APPROVAL .7----.._ CATE Don Adams 8-02-99 sT £ fr,A.r4c .P-_7 - ? 7 FORIINO SOW SDNY_GM_02759857 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 co g -a EFTA_00246779 EFTA01331242

SDNY_GM_02759858 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246780 EFTA01331243

R0HR.ING. 1.11) Won Whe oda VW CM* Mir-z» ENGINEERING REPAIR DATA SHEET (EROS) SUPPLEMENT SHEET RCS NO. C1036 &v. S.0. NO. NIA PAGE 2 OF 2 (brscerniver covriferea) (DISPOSMON CONIIUNUED) LOWER SKIN REPAIR 1. Remove existing repair (fiberglass) from discrepant area on lower surface. . - 2. Cut filler to size of discrepant area from .016 gauge 202443 per QQ-A-250/5. 3. Fabricate doubler from .020 gauge 2024-0, per DO-A- 250/5 to cove finer. Doubler to overlap filler periphery by 1.50 min. Optional to use 202443, no heat treatment required. 4. Form doubler to match lower skin contour per BAC 5300. Heat treat to -T42 per BAC 5602 or MIL-H-6083. Verify hardness per SRM requirements. 5. Inboard and outboard edges of doubler to be tapered to. .010 min. Care should be taken so the edges of the doubler land mid spaced between existing assembly fasteners. 6. Install doubler using steps 3 through 8 above. 7. Install new panel, filler & doubler using BIP fasteners to complete assembly. Apply sealant to edge of logo fight cut out . and sea all gaps at assembly. 8. Clear Abdine all external clad surfaces per MIL-C-5541, Class 3. hatred Ink When Ibis Steam ORIGINAL! DMILIET.... E EOM MI E7913.11 SDNY_GM_02759859 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246781 EFTA01331244

SDNY_GM_02759860 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246782 EFTA01331245

8- 3-99 4:55 PM ;SUPRA 27 PROGRAM • , BY B. COX DATE 08/02/99 enK131-5frefgrATE EROS cioss DOOM =El ROHR ROHR, INC. ; 5/ 8 PAGE 1 of 4 TITLE Skin Disbond VA545300-1 Us or d rc of chi: infonration ts subject to the Tottrietion on the utle. 3.0 or on the lint• of This document Super 27 I. Discropancy: Tho outer akin of the upper skin assembly of the aft fairing is disbanded and the aft edge of the outer skin has two cracks. See sketch below from ERDS. II. Proposed Disposition: Remove the outer skin of the upper skin assembly and bond on a new outer skin using FM 73 adhesive and BR 127 adhesive primer. The cracks at the aft odge have been reported to be along a previous repair that was filled with a fiberglass patch repair. The fiberglass patch will be removed and replaced with a metallic patch and doubler. All metallic materials will be the same as BP materials. III. Static Analysis: The aft faking is analyzed in section 10 of Reference 1. In section 10 of Reference the substructure has been analyzed to withstand all the aerodynamic loading without using any of the skin as affective. Therefore, this analysis will only investigate the capability of the adhesive to carry the shear stress to the core conservatively assuming that the skin will carry the aerodynamic loading. Strut Stress Analysis (VA-CR154 Rev. C) SDNY_GM_02759861 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246783 EFTA01331246

SDNY_GM_02759862 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246784 EFTA01331247

8- 3-99 4:55 PM ;SUPER 27 PROGRAM 8/ 8 BY B. COX DATE 08/02/99 CHK13 DATE EROS c1036 ❑❑❑1J KKKK ROHR ROHR, INC. PAGE 2 of 4 TITLE. Skin Disband VA545300-1 the or disclosure of this infant-stain ts subject to the restriction on the htle Age ce- 071 the stint page of this clxument The noted adhesive primer is compatible with the adhesive as shown in the excerpt of MIL-HDDK-337 at the end of this analysis. Conservatively assume all the aerodynamic load is reacted by a 1.0-Inch wide by 30 inches long beam that is simply supported between the fuselage and outboard edge. The core shear stress (L) is expressed by f c = V / hb where V is the vertical load being reacted at the supported end h is the centroid distance of the sandwich panel h = t/2 + to/2 + t b is the beam width From page 10.7 of Reference', the aerodynamic pressure (P) on the aft fairing Is .5 psi limit (.75 psi ult). Therefore the ultimate vertical load at one end of a simply supported beam is V = .75(30)(1.0)/2 = 11.25 lbs (ult). From VA545300, t = .016, to = .032 and t, = .30. h = .016/2 + .032/2 + .30 = .324 in f c = V / hb = 11.25 / .324(1.0) = 34.7 lbs/in2 From the certification sheet shown at the end of this analysis, the allowable lap shear for the FM 73 adhesive is 6.523 psi at 75° F. Since there is nu test data readily available for this adhesive system for core bond, a comparison of this adhesive system will be made to EA9649R (RMS 058). From figure 3.3.2 of Reference 2, aluminum core and face sheet with EA9649R adhesive has an allowable of 220 psi for the BP core configuration. Since the lap shear for the repair adhesive is significantly higher than EA9649R (2,838 psi at 75° F), it is reasonable to assume that 34.7 psi core shear Is acceptable for this adhesive system. The repair at the aft end of the faking is acceptable by inspection since the aerodynamic load is very little to nil at this location. IV_ Fatigue Analysis: Repair is acceptable for fatigue strength by inspection since the ultimate margin is high and there are no additional stress concentrations compared to the type design. Meth anIcal Design Allmables (RI IR 85 -013) SDNY_GM_02759863 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246785 EFTA01331248

SDNY_GM_02759864 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246786 EFTA01331249

8- 3-99 4:55 PM • ;SUPER 27 PROGRAM DODO 7/ BY B. COX DATE 08/02/99 DODO PAGE 3 of 4 cHXD DATE ROHR ROHR, INC. Tine Skin DIsbond EROS C1036 VA545300-1 disckme iefenurtton Ie HAdeci A, Me =Waft OA the thic OeMW on dlefintrast Of lath domanant j 44 812D4058K-337 1 Ammmber 2882 I III lit 1 i Ji I Si l € 4 E - . , 1 . i i, . .. 1 11 it 11 ill ... H i 1 1 g g :1 si 4 A i gx 1- I 1 s 1 I i 0 .z g li I- 0 i a # 2 i • -, 1 ; i i 8 i ri n 9. in k ii LIE iss , 1 i . I i 1 — = .-•-•. ≥ i 1 z • SDNYGivl_02759865 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246787 EFTA01331250

SDNY_GM_02759866 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246788 EFTA01331251

8- 3-99 4:55 PM ;SUPER 27 PROGRAM ; 8/8 av E. COX DATE 08/02/99 CHICO ERDS C1036 DATE DOM ROHR ROHR, INC. PAGE 4 of 4 TITLE Skin Disbond VA545300-1 use Qf nisch:num omit InnermatIon s rublect to the rowletIon on the tie. Pluto or on the Bntpax. of document = Willi am's saws Men S R akalg CBRTKrrewom COLD •111400-LARD CITY TO P.O. BOX 1909 LANK Clry YL. 32026 sale TIMC0-1.14102 CITY To =GMAT 90 EAST Zat.,TAZ =Ma 20uTE 19, NOR 1029 OOR ORDER IA= CITY 0023439/001 FL 32026 CUSTOMER DArm SHIpPRD ORDER 690376 06/17/99 pRoDucr BMW* 28CEIPTION . mix 49132 MS00101202 RECOOLMENDED GTORA23-- SWIM AT oR DZZOW rig 7111 .06 rSV 3 • ASR Flaw 12 Nouth0 FROM maw OP BETEMENT 0 negrsoo P --------....... 5 .00 ET7 DEA5 BATOR/OBIT MID BATCH// TIT DATE NUMBER NUMB= fratiljTACMXW (=WITT am 2742-037 aVS.13,1000 300.00 SF in 27402 TOTAL 1. WATCH OTT - sou.00 k TOTAL-, Ise TOTAL OTT 600.00 4.* ISIS CgRTIP2a4 TES DUITNRIA4 AT tD or 0131/e/0252 001052900; To APPLICABLE: MOT= USLOW. • P CROW 3 PR2/092 MOTES AS PART OF CYST2m- TUR-1 WITH TNS OR PIXTFEMX TD Aliti SEE CYTEC FOR I I? trgg DRNMINGS AND BectIFICATIOU3 SPECIFICATTOBg: MW-Ar/32 RSV B. TrAW-2 ran I CLASS 2 FORK 6747a 21132BEaVii OR ALv4EXPTANC72 PBSKIIRM2012 3 a Clic PART XDP2CIVII AE3 cemy TO BR USED mATC22K40 Arcarvt WADI CESTIPICAT/ON. 42928TM:ice.* 76 F LAP 9KRAR [iRs.9. stag, VTBIC:tir .061, .061, 9 /C : .-40224-Nalflal TEST A A 40 180 F 6704. 6622, 6122 Psx 4s3R, 4370, lave. 4260, Rsxs Pai .062 Par OA ADTKORI2RD SIgZIA.TORS e1/224ljl e/$2r 4r lAng7JVcr LZ )1gdng: Pid fre:C eg-C -g SONY_GM_02759867 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246789 EFTA01331252

• SDNY_GM_02759868 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246790 EFTA01331253

Work Order 43736. IfIII US Dopitimontol T importation wwwkoriwa idailalsin00. . MAJOR REPAIR AND ALTERATION"' 'a'. • "'"• " • ' • • (Airframe, Powerplant, Propeller or Appliance) - " " ' ' • • • - • • • . .... .. , Fonn Approved i . , 4. . OMB No. 2120-0020 ' • t •• For FAA Use Only Office Id ratification U % ot . T -; I ap'--.. • • ‘.. • INSTRUCTIONS: Print or type al entries. See FAR 43.9, FAR43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for InstrucUons and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penally not to exceed 51.000 for each such violation (Section 901 Federal Aviation Act of 1858). • • . 1. Aircraft Make / 1 r"'Ir .. Boeing Model •• . . •- • ..'.:. .. ,r: I N 727-31 j• 1• 1 • l • ” I Serial No. •4 : 20115 Nationality and Registration Mark •. N505LS 2. Owner Name (As shown on registration certificate) . j i., :4 Northwest Delaware Corporation. Address (As shown on registration certificate) .., . . , 1105 N Market St . • " Wilmington, DE 19899 3. For FAA Use Only -The data identified herein complies with the applicable airworthiness requirements and Is approved only for the above described aircraft, ••. subject to conformity Inspection by a person authorized In FAR 43, s Ion . 43.7 20fr %deaf / GL-CMH FSDO aura of FAA Ins cler fJetsus Zubia - Unit Identification 5. Type Unit Brake '. "a" h ' . 1‘ I. • Model . . , Seder NO. ' . Repair Alteration AIRFRAME ....... ..................... . Jetta:dee:We Kem 1 above)A.ri ,,,., , , c.o., ,„.....,. ? . . .. . . ... X POWERPLANT • • ' • - ' ••••. • • PROPELLER . . • • "..f P! 'n tr ;,. f ' • ". I . .. i i AI An.. • r.•:•' ":" ' • -rintsx,;• . A' ' 'IV • • APPLIANCE Typo ,. ' ' I • Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Cedificate No. ElectroSonkS • • 4391 International Gateway Port Columbus International Airport Cotentin, OHIO 43219 U. S. Certificated Mechanic Repair Station AE1R005K. Radio Class 1.2 8 3: Instrument Class 3, Accessory Class 3 Limited Altimeter Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair andfix alteration made to the unit(s) Identified in item 4 above and described on the reverse or attachment; hereto have been made In accordance with the requirements of Part 43 of the U. S. Federal Aviation Regulations and that the information furnished heroin Is hue and correct to the best of my knowledge. Dale April 28, 1999 Signature of Authorized indi • - • • - - • - • •-- - • • - 7. Appro al Rot Service l I - ' 4 Pursuant to the authority given persons specified below, unit id n item 4 was I spelled In the manner presented by the Administrator of the Federal Aviation Administration and is ID APPROVED 0 REJECTED i'.: ' I • BY FAA Fit SLindards InSpectot Manufacturer Inspection Authorization . rtz:: Other (Specify? . .... - • 1 FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group 1• . • I .1 ii. e • • 1 .• Date of Approval or Rejection q -di -"I i - - • - --- Certificate or Designation No. AE1R005K Signature (Authorized Ind hi I . — ' . , r • SDNY_GM_02759869 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024679 I EFTA01331254

NOTICE V. 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 shoots. Identify with aircraft nallonakty and registration mark and date work completed.) • . • 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKEJMODEUDE.SCRIPTION STATION INSTALLATION DATA 622-7203-101 3 Collins VHF-422b Comm 2. The following equipment was Installed In the aircraft. PART NUMBER QTY MAIEJMODEUDESCFtIPTIoN C37c, C38c TSO 450.0 • STATION 822-1115-001 3 Collins VHF-422c Comm C37c, C38c 450.0 523-0772719 3. The above work was accomplished IAW FAA Advisory Circular AC 43.13-16, Chapter 11,12 and AC 43.13-2A, Chapters 1, 2. 4. This work has been accomplished under ElectroSonics Work Order 43736. •. 5. Removed existing Collins VHF-422b corn's to accomplish 8.33lan modifications Collins S.8.17. Following modification, reinstalled as VHF-422c and performed a complete operational check. 6. A complete test of the installation of the modified unite has been conducted to confirm that other aircraft systems are free of interference as a result of this Installation. All tests found to be satisfactory. 7. Collins does not specify any new continued airworthiness instructions for the above equipment The owner/operator should consult the Boeing maintenance manuals for general avionics continued airworthiness requirements. 8. The owner/operator must comply with manufacturer's maintenance instructions to ensure continued airworthiness any time the above equipment Is removed and/or repaired and reinstalled. 9. The aircraft Weight and Balance is unchanged and Equipment List has been amended. 10. The aircraft must be loaded JAW the prescribed loading' Information from the manufacturer. END • 04 ti-Iffil 54 {4 C-2 A4 04 134 I *4 04 storm A3 AeR 2 8 1999 04 1 1A 04 34 4e 0-6 ..,..,s. COIULI10ON . 04 C-9 i C4 I65 1A41 11410 A-9 1,7 - 0-t A-/ 0-3 II-1 2 54 3-0 C-1 C.4 £4 44 . vans, . 7 .,Ni — 31999 . Al r i; 0-41 ii.f. kieto SC , ci,„ ,,„„ commas es 1-7 C-3 I C-4 C-S 311 A40 A-8 .A.7 04 All 0 Additional Sheds Are Attached r • U.S. GPO:1991-0-568-012/40035 SDNY_Glvl_02759870 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246792 EFTA01331255

vo• :•16 r.., : Work Order 43736. 01 MAJOR REPAIR AND ALTERATION''' •• • 1 , Form Appmved . • : r. •Ir • :. OMB No. 2120-0020 For FAA up Only ' US Departrnoce el (Airframe, Powerplant, Propeller or Appliance) , Pampa, Ike foams 440444 4eninfoneen • • • e.' . 27: -. GL07 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43Append& 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 • 1 1.•1 . Boeing . Model : ' t -4I' , ''..1 :k i. ‘11 . . . 727-31 Serial No. 20115 Natrona fty and Registration Mark • • N505LS 2. owner' Name (As shown on registration certificate) ::., Northwest Delaware Corporation.. . Address (As shown on registration credilicale) . . ..1105 N Ilarket St 11/11n4nOpp, DE19899 ' . .. • 7 . :: : c .. 3. For FAA Use orgy • • I" i :7 -The data Idenktred herein complies with the applicable airworthiness requirements and is approved only for tho above described aircraft,..., .. . ...,, subject to conformity Inspection by a person authorized In FAR 43, section 43.7 / 4 17 4 07 • did/ GL-Clitti FSDO . Dale tura , r Jesus Zubla • • • ' • ;,'• 4; Unit Identification S. WIN Unit . .,,.. Make ,:., .• .: f. •.,'• • r. ol . 4. :. - Model •.;i:i:.:. .StnialNo. Ntecation AIRFRAME . , . . . , • a deSeriberd ill lien, t above). et .17•I7..arr.”, .rr f • • ! , • . ; X POWERPLANT . .,,,gur•r• •••• .4 e 't ".' 1 PROPELLER APPLIANCE Type • .' '.• *. • • •• r• - '• Or • .. . • Manufacturer 6. Conformity Statement A. Agency's Name and Address. : B. Kind of Agency • • • - '' ''• t 1. ' • C. Certificate No. - • EledroSonics 4391 International Gateway Port Columbus International Airport Columbus, OHIO 43219 U. S. Certificated Mechanic Repair Station AE1R005K . Radio Class 1,2 & 3: Instrument Class 3. Accessory Class 3 Limited Altimeter Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I candy that the repair *miler alteration made to the nit(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 knondedge. Date April 28, 1999 Signature of Au orized Ind i ; . r.1 , .. ....> .—• / .. i N i i :. *c.-- . 7. Approval or turn o nice : Pursuant to the authority given persons specified below, the un Idea In m4 was inspected in the manner preacnted by the Administrator of the Federal Aviation Administration and is CIAPPROvED 0 REJECT@ ?. i ()poi :.) c BY FAA Fl Stanclaxis leSpectof Manufacturer Inspection Authorization Other , Other (S • ..; \ ; FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Lt- I Date of Approval or Rejection Li - 11 - 99 Certificates Designation No. AE1R005K Signa r of Authorized ' ual • -- - - --- - 'BM SDNY_GM_02759871 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246793 EFTA01331256

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 Conformfty 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. The following equipment was removed from the aircraft: PART NUMBER CITY MAKEJMODELJDESCRIPTION STATION 622-6520-005 2 Collins CTL-22 200.0 622-6520-005 '1 Collins CTL-22 • 259.5 2. The following equipment was Installed In the aircraft. PART NUMBER OTY MAKEJMODEUDESCRIPTID4 ill:) . . STATION. INSTALLATION DATA 822-1120-005 2 Collins CTL-22c • : 822-1120-005 1 Collins CTL-22c I i _ . . • The above work was accomplished IAW FAA Advisory Circular AC 43.13-1B, Chapter 11,12 and AC 43.13-2A, Chapters 1, 2. ' • • • ' ' 4. This work has been accomplished under EiectrOSonics Work Order 43736. . 5. Removed existing CTL-22 to accomplish the 8.33KHZ spacing modifications Collins S.B. 31. Following modification, reinstalled units'and performed a complete operational check. 6. A complete test of the installation of the modified unite has been conducted to confirm that other aircraft • systems are free of interference as a result of this installation. All tests found to be satisfactory. 7. Collins does not specify any new continued airworthiness instructions for the above equipment The owner/operator should consult the Boeing maintenance mahuais for general avionics continued airworthiness requirements. 8. The owner/operator must comply with manufacturer's maintenance instructions to ensure continued ; airworthiness any time the above equipment is removed and/or repaired and reinstalled. I . 9. . The aircraft Weight and Balance is unchanged and Equipment List has been amended. _ . • 10. The aircraft must be loaded lAW the prescribed loading information from the manufacturer. END C37c, C38c 200.0 523-0072719 C37c, C38c, 259.5 2.1.p 34 C-1I C.4 04 I 1S-0 I A-2 A-1 6 1 ctcf RI 0 A-3 Alit( 28099 A.4 0 . le5 0 ) A-7 ii, o J ..,„ 1500 COLO:ABU 014 0 ) C-3 I C-4 I C411.41 I A.I0 1.-9 0 1 A4 0-1 41-1 2 S•A S•0 C-1 C-2 A4 0-2 A-2 0-9 - SCW* .A.3 :•iiii ''' 3 ' A .- • GIN SDO• • •FOill. A ,, 4.. c.-a e-e, C4 A4I -1.-10ii.-9 it' , 0-7 1 04 i . • . O Additional Sheets Are Attached . U.S. GP0:1991.0-568-012140035 SDNY_GM_02759872 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246794 EFTA01331257

r MAJOR REPAIR AND ALTERATION Form Apprrsed OMB No. 2120-0020 uS OeParencs (Airframe, Powerplant, Propeller, or Appliance) For FM Use Only d Transportaion Federal Aviation AdmInIstreUen Oftioe Identification .e44. Asto-o 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 disco:Won of this foot This form is required by lay (49 U.S.C. 1421). Failure to report can mutt in a civi penalty not to exceed $1,000 for each such volition (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Mom Boeing 72741 Serial No. 20115 Nationality and Registration Mark N505LS 2. Owner Name (As shown on regStra0an certificate) Northwest Delaware Corp. Address (As 5/10W77 on registration cettiatte) 1105 N Pdaltit atrii .. WilmIngin, 98 1. 4 3. For FAA Use Only Alki 1 0 1C93 CM-DALLAS SW05 4. Unit Identification 5. Type Unit Make Mo0el Serial No. Repel( Altera= AIRFRAME described in item 1 X X (As above) POWERPLANT PROPELLER • APPLIANCE Type Manufacturer 6. Conformity Statement A. Agencys Name and Address B. Kind ofAgency C. Certificate No. Associated Air Center 8201 Lemmon Avenue Dallas, Texas 75220 V.S. Castrated methane TX2Ft203L Airframe Class 3 & 4 Radio Class 1, 2 & 3 Foreign Certificated mechanic X C,ertifcated Repair Staten Menvfackuer a i certify that the repair an/or alteration made to the unit(s) Identified in hem 4 above and described on the reverse or attachments hereto have been made in accords= with the requirements of Pal 43 of the U.S. Federal Aviation Regulatory% and that the information furnished herein is true and correct to the best <limy knomedge. Date 8/4/98 Signature of Authorized IndMdual ›rionjA 1141 O °— 7. Approval for Return to Service Pursuant to the authoritygiven persons specified bele", the unit Identified in item 4 a inspected m the reamer prescated by the Administrator of the Federal Aviation Administration and is @APPROVED 0 REJECTED BY FAA Ft Standards Inspector Manufacturer insponionAuthorizarlon Other (Specify) FM Designee x Rent Station Person Apfund ly Transpal Canadian Ainvalhmess Group Date of Aquae' a Rejection 814/98 Certificate or Designate No. TX2R203L Signature cfAuthatted IndiAdu.al 71i,a- 4/ 40 141.4rdler—• orrn 337 (1248) SDNY_GM_02759873 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246795 EFTA01331258

NOTICE Weight and balance oropereting 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 al more space is require; attach addoxial sheet& meow wen aircraft nationality and leglerallco mark and Ode work completed.) Aircraft: Boeing 727-31 Registration #: N505LS Serial #: 20115 Aircraft Total Time: 31,675.6 Aircraft Total Cycles: 21,567 August 4, 1998 The following alteration was accomplished at Associated Air Center, Dallas, Texas under Work Order 1565. 1) Mode "S" Transponder ICAO Code Strapping Change in accordance with AAC Drawing 1565-001 Rev A dated July 28, 1998, 8110-3 approved by D.E.R. SW-997, David A. ICimbrell July 29, 1998. The following repair was accomplished at Associated Air Center, Dallas, Texas under Work Order 1565. 1) Repair - L/H Horizontal Stabilizer Trailing Edge Beam at Elevator Station 156 in accordance with AAC Repair Drawing 1565-002 dated July --, 1998, 8110-3 approved by D.E.R. SW-810, Robert IV Manashi August 4, 1998. **************************END************************** K Additional Sheets Am Attached U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60167 SDNY_GM_02759874 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246796 EFTA01331259

DAK-98-089 OrlArnewr OF TautaPORTATION FEDERAL AVIATioN ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JULY 29, 1998 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE ( 41Irplano, Radio, Holleoptist, eta.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER DALLAS, TEXAS LIST OF DATA IDENTIFICATION 1TTLE 1565-001 REV. A 07/28198 MODE S TRANSPONDER ICAO CODE STRAPPING CHANGE ' I ... NOTES: TC DATA SHEET A3WE. ELECTRICAL DESIGN ASPECTS OF THIS THIS APPROVAL APPLICABLE TO B727-31 THIS 8110-3 FORM IS IN SUPPORT OF FAA : • iikl. DATA IS APPROVED. Sits; 20115 ONLY. FORM 337. PURPOSE OF DATA TO SUPPORT THE AVIONICS/ELECTRICAL MODIFICATIONS. APPLICABLE REQUIREMENTS (List specific sactrons) FAR 25.1301 (a)(b)(c) CERTIFICATION - Under authority appointment under Part 183 of 0 have vested by direction of the Administrator and In accordance with the Federal Aviation Regulations, data listed above and on attached been examined In accordance with established procedures and found Regulations. approval of these data these data conditions and limitations of sheets numbered to comply with applicable requirements of the Federal Aviation M Recommend I OM Therefore Approve SIGNA\URE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE/Si DESIGNATION NUMBER(S) CLASSIFICATION(S) DAVID A. KIMBRELL 7 SW-997 AVIONICS/ELECTRICAL i i a 7 -1:71/../ SYSTEMS ylo ... /L.-/e2ezber FAA Form 8110-3 0140) s. ‘FTIFS ',Remus Ecmom( COMPUTER GENERATED) GPO 1,01413 SDNY_Gtv1_02 759875 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246797 EFTA01331260

SDNY_GM_02759876 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246798 EFTA01331261

AUG-04-1999 10:39 ASSOC AIR 214 357 2845 214 357 2845 P.01 U.S.OEPARTmENTOFTPANsPoRTATION GEDERALAVIATIONADMINI8TRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE #98421 AtIO03T Oil, 1992 _ AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MARE 307.1NO MODEL NO. 727-31 TYPE (seats. was en) AIRPLANE (N5001.3) NAME OF APPLICANT A280CIATZI1 Alit - CENTER LIST OF DATA IDENTIFICATION TITLE ASIOCIATrD ALA Car= DUNI= NO. 1565-002 ASV. "IR', DATIO 07-29-1928 REPAIR - L/H HatazzoNTAL STAB:LIZ= T/t OPFER SIM - SLEW STA 136. (Slat 1, 2 AND 3 or 3). 140725: 1. THE STRUCTURAL A3PiCTS ONLY Or TEE ABOVE LISIID RATA ARP arrimmoo tronasn. suss APPROVAL 28 roil ens ENGIUMMIro DESZON DATA ONLY. 2. THIS APPROVAL 13 VA.= ONLY FOR HOEING MODAL NO. 727-31, AIRCRAFT 2/N 20125 AND Is ism= IN St719PCCRT Or A MAJOR REPAIR Or THY SUBJECT AIRCRAST. PURPOSE OF DATA IN SUPPORT OF A WAJOA AMUR ON HOEING )DOLL NO. 727-31, AERCFATI 3/N 20115. APPLICAELE REQUIREMENTS as %vox sae CAR 41).200 (a) , (b) , 41).201 (11) , (b) , (e) , tb.202, 4b.300, tb.301, 4b. 302, 417.903, 4b.304 (al , (b), 4b.308 (a) , (b), (d) • CERTIFICATION - Under authority vested by &U MW of limitations of appointment under Part 183 of Ma Federal sheets numbered ,J00C0000000000CCOOL have been found to comply w*h appliCable requirnmentS of the Federal the AdmIntStrator and in accordance Aviation Regulations, data listed examined in accordance with Aviation Reaulelions. data with conditions anti above and on attached establithad procachuta and INI Recommend Approval et these I (WI) THEREFORE o Approve these data aloNtrauRgiinoro ENGINEERINGREe 6EWATIMS) 0664NATIONNUMWM) cutiSSIFICATION(8) a t 8W-910 ariUnEvara Rama KAI i. ze 0 /.7C)10.1ZUZINS1 PASYLOP1 ISIM0N c_ri A -• r)e.e5 . TOTAL P.01 SONv_GIvi_02759877 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246799 EFTA01331262

SDNY_GM_02759878 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 0024680() EFTA01331263

• • 00...••••1 OP IIIMMOSTA.M= "aal...1•IMMUIONI STANDARD AIRY/00711MM C10111FICA72 • ••••••••••••./0 •••• =ten.. Weee•••• MOM BOUM 727-31 20115 122112PORS •••••••Pkir..0 0.10••••••4 B 07-23-90 cum FAA form 81004 oah T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA_00246801 EFTA01331264

SONY_GM_02759880 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA _00246802 EFTA01331265

• MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) of Transpartation Federal Aviation Administration FOOT, Approved Om% or se nly PAAGONLLAS A., MO; r \ (A/C- INSTRUCTIONS: Print or type ell 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 form is required bylaw (49 U.S.C. 1421). Failure to report can result in a cm penalty not to taceed S1,000 for each such violation (Section 901 Federal Aviation Act of 1958). I. Aircraft Make Boeing Model 72741 SCSI No. 20115 Nationality and Registration Mark N500LS 2. Owner Name (As shown on regisfration certificate) Northwest Delaware Corp. Address (As shown on registratbr: cofttecate) 1105 N Market St. Wilmington, DE 19899 3. For FAA Use Only 1. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteralion AIRFRAME described in item 1 X X (As above) POVVERPLAfT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A Agencys Name and Address B. Kind of Agency C..Certificree Nor- • Associated Air Center 8201 Lemmon Avenue Dallas, Texas 75220 U.S. Certificated Mechanic •• TX2R203L., .. • • • Class 3 & 4 Foreign Certificated Mechanic X Certificates Repair Stason Manufacturer D. I certify that the roper and/or alteration made to the wigs) identified in item 4 above and described on the remise or attachments hereto have been made In accordance with the requirements ci Part 43 of the U.S. Federal Aviation Regulations and that the inforrrigion furnished herein is true and correct to the test of my knowledge. Date 812197 Sig of Authorized kern OW . fi 7. Approval for Re Service Pursuant o the authoritygiven persons specified below, the unit identified tern 4 was inspected in the manner prescrited by the Administrator of the Federal Aviation Administrtmen and is (J APPROVED QREJECTED BY FAA FN. Standards Inspector Manufacturer Inspection Authortzation Other (Specify) FAA Detente X Repair Station Person Approved hy Transport Canadian Akworthmess Group Dale of Approval a Relection 8/2/97 - - - --- Certificate or Designation Na TX2R203L Signalise Individual S iore. .e_____ SDNY_GIvl_02759881 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246803 EFTA01331266

NOTICE • Weight and balance or operiling limitation changes shall be entered in the appropriate aitraft record. An alteration must be compatible with all previous alterations to assure continued contort:lily with the applicable airworthiness requirements. 8. Description of Work Accomplished Itl mere spice is rtio.iised attach adational sheets kin** with aitaart amount), and regiStatiOn mark and date work corn#eted) Aircraft: Boeing: 727-31 Registration #: N500LS Serial #: 20115 Aircraft Total Time:31,471.2 Aircraft Total Cycles: 21,468 August 2, 1997 The following work was accomplished at Associated Air Center, Dallas, Texas under Work Order 1476. 1)Repair - Airstair Door Actuator Attach Clip in accordance with AAC Repair Drawing 1476-001 IR dated July 16, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 2) Repair - #1 & #3 Pylon Corrosion on Forward Engine Mounts in accordance with AAC Repair Drawing 1476-002 IR dated July 17, 1997, 8110-3 approved by D.E.R. SW- 916, Jim Martin July 22, 1997. 3) Repair - #8 Leading Edge Slat Crack at 1/B Slat Guide in accordance with AAC Repair Drawing 1476-003 IR dated July 17, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 4) Repair - Corrosion on R/H Wing Upper Surface at WBL 70.5 Between Str. 1 - 14 in accordance with AAC Repair Drawing 1476-004 IR dated July 21, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 5) Repair - Floor Beam BS 600, RBL 25 Figure $ Hole in accordance with AAC Repair Drawing 1476-005 IR dated July 22, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 6) Repair - Aft B/B Door Interior Structure Cracked in accordance with AAC Repair Drawing 1476-006 IR dated July 22, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22. 1997. 7) Repair - Wing to Body Fairing Damaged Dome Nut in accordance with AAC Repair Drawing 1476-007 IR dated July 25, 1997. 8110-3 approved by D.E.R. SW-916, Jim Martin July 25, 1997. 8) Repair of Center Engine Exhaust Nozzle in accordance with Rohr, Inc. Engineering Repair Data Sheet No. C0625 Rev. A dated July 23, 1007, 8110-3 approved by D.E.R.(s) NM-2731, Jeffrey D. Shutrump for Structures, NM-738, Tony Bradlaugh-Dredge for Powerplant and NM-2182, Michael August for Special Administrative July 23, 1997 and AAC Repair Drawing 1476-008 IR dated July 25. 1997. 8110-3 approved by D.E.R. SW- 916, Jim Martin July 25. 1997. S eAddsonal SIvrais Are AlleNte0 U.S. GOVERNMENT PRINTING OFFICE: 1992.769-012/80157 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, SDNY 027591382 15, and 17 EFTA 00246804 EFTA01331267

Aircraft: Boeing: 727-31 Registration #: N500LS Serial #: 20115 Aircraft Total Time:31,471.2 Aircraft Total Cycles: 21,468 August 2, 1997 9) Autopilot Interface Unit Modification in accordance with AAC Drawing 97-2211- 210 IR dated July 28, 1997, 8110-3 approved by D.E.R. SW-880, John W. Goswick July 28, 1997. END SDNYGlvl_02759883 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246805 EFTA01331268

SDNY_GM_02759884 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246806 EFTA01331269

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22J97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Alrotene, Radio, Helicopter. etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-001 4-- REV. IR 7-16-97 REPAIR - AIRSTAIR DOOR ACTUATOR ATTACH CLIP THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (Ust specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 ..303 .307(c) .300 .304 CERTIFICATION • Under authority vested under Part 183 of the Federal Medico Regulations, exemined In accordance lab established procedures by direction of the Administrator and In accordance data listed atom and al attached sheets and found to comply vAib applicable Recommend approval of these data Approve these data with conditions and britallons of appoirtment numbered el oe oC have been requirements of the Federal Aviation Regulations. MI I ) Therefore .00 I= SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 57.: . ._..., JIM MARTIN SW-916 STRUCTURES _.. _ GPO 901-613 SDNY_GM_027598B5 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246807 EFTA01331270

SDNY_GM_0275.386 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246808 EFTA01331271

ARC.11.IS1 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane. Radio. Helicopter. etc.) AIRPLANE NAME OF APPUCANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-0021" REV. IR 7-17-97 REPAIR - # 1 & # 3 PYLON CORROSION ON FWD ENGINE MOUNTS THE ABOVE DATA IS APPROVED ONLY. FOR AIRCRAFT S/N INSPECTION FOR THE STRUCTURAL DESIGN ASPECT 20115 PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrate' and In accordance with conditions and ambitions of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered te. se 41 have been panned In accordance se established procedures and found to comply with applicable requirements lathe Federal Aviation Regulations. Recommend approval of these data BEI I Therefore Ve4 rXi Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) 7r -76 JIM MARTIN SW-916 STRUCTURES _.. _ ...._ _ ... _ GPO 901.813 SDNYGIvl_02759887 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246809 EFTA01331272

SDNY_GM_02759888 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246810 EFTA01331273

AitiC•17. ISE U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-00317 REV. IR 7-17-97 REPAIR - # 8 UE SLAT CRACK AT I/B SLAT GUIDE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECT\ ON PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .308 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance under Part 183 of the Fedora/ Aviation Regulations, data listed above and on attached sheets comined in accordance wilts established procedures and found to comply vieh applicable (=Recommend approval of these data I 20) Therefore Approve these data with conditions and Imitalims of appointment numbered re 44. re have been requirements of the Federal Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 7 : JIM MARTIN SW-916 STRUCTURES _.. _ can (11-70 EDITION) GPO 9014313 SDNY_GM_02759889 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246811 EFTA01331274

SDNY_GM_02759890 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246812 EFTA01331275

RAC•c11.15 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane. Radio, Hetcopter. etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-004 L." REV. IR 7-21-97 REPAIR CORROSION ON R/H WING UPPER SURFACE AT WBL 70.5 BETWEEN STIR. 1 - 14 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INS? ECT ION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 -.303 .307(c) .300 .304 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Reptile/king, examined in accordance with established by direction of the AdmInkstrator and In accordance data listed above and on attached sheets procedures and found to comply vett appdcable Recommend approval of these data Approve these dela with conditions and riflery; of appointment numbered SC. at re( have been requirements of the Federal Aviation Regulatiors. NM I Therefore (Wic) II 9 SIONATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) " -e JIM MARTIN SW-916 STRUCTURES -- - - -- -- - -- - GPO 901413 SDNYGlvl02759891 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002468 I 3 EFTA01331276

SDNY_GM_02759892 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246814 EFTA01331277

ARc•ii. lac] U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1478-005v REV. IR 7-22-97 • REPORT NO. 1478-005 (.--- REV. IR 7-22-97 REPAIR - FLOOR BEAM STA. 600 RBL 25 FIGURE 8 HOLE STRUCTURAL SUBSTANTIATION - REPAIR - FLOOR BEAM STA. 600 RBL 25 FIGURE 8 HOLE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL ONLY. FOR AIRCRAFT S/N 20115 INSPE CTION DESIGN ASPECT PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REOUIREMENTS (Ust swift sections) CAR 4b.200 .301 .305 .201 .302 .308 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested under Pad 183 of the Federal Aviation Regulations, ermined h accordance %Nth estabEshed by direction of the Admiresbator and in accordance data fisted above and on attached sheets procedures and found to complyWM applicable Recommend approval of these data Approve these data wilh cations and limeations of appointment numbered are ex" al have been requirements of the Federal Aviation Regulations. MN () I Therefore 9,0 I l SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) f.1 7e JIM MARTIN SW-918 STRUCTURES arm 81103 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901413 SDNYGIvl_02759893 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246815 EFTA01331278

SDNY_GM_02759894 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002468 I 6 EFTA01331279

lifiC•il• Ito I U.S. DEPARTMENT OF TRANSPORTATION • FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Ratio Helicopter. etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER UST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476.006 4-- REV. IR 7-22-97 REPORT NO. 1476-006 4, REV. IR 7-22-97 REPAIR - AFT B/B DOOR INTERIOR STRUCTURE CRACKED SRUCTURAL SUBSTANTIATION - REPAIR - AFT B/B DOOR INTERIOR STRUCTURE CRACKED THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List spectfto sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 .303 .307(c) .300 .304 CERTIFICATION - Under authorfty vested under Part 183 of the Federal Aviation Regulations, examined In accordance with established by direction of the Administrator and In accordance data listed above and on attached sheets procedures and found to comply %Oh applicable Recommend approval of these data Approve these data web conditions and ImIted:res of appointment numbered 60/ ree d have been requirements able Federal Aviation Regulations. No I 0 Therefore 0 a) SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) g 7.—te JIM MARTIN SW-916 STRUCTURES orm 81103 (1 • EDITION) GPO 901-613 SDNYGivl_02759895 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246817 EFTA01331280

SDNY_GM_02759896 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002468 I 8 EFTA01331281

fIRC.97, IL. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/25/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio. Helicopter. etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER UST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-007 •-• REV. IR 7-25-97 .---- REPAIR - WING TO BODY FAIRING DAMAGED DOME NUT THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (Ust specific sections) CAR 4b.300 .304 .305 CERTIFICATION - Under authonly vested under Pea 183 of the Federal Aviation Regulations, earnined in accordance vats established by drecdon of the Administrator and In accordance data listed above and on attached sheets procedures and found to comply vith applicable Recommend approval of these data Approve these data HIM anditions and limitations of appoinbnent numbered o 44 mr- harm been requirements of the Federal Aviation Regulations. MI I Therefore Opfi; Ui SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTAT1VE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) f -al JIM MARTIN SW-916 STRUCTURES FAA Farm 8110-3 (11-70 SUPERSEDES PREVIOUS EDMON) GPO 901413 SDNYGlvl_02759897 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246819 EFTA01331282

SDNY_GM_02759898 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246820 EFTA01331283

RAC-J(11. 1CA) . U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/25/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Ain:sane Radio. Helicopter. etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER UST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-008 (---- REV. IR 7-25-97 REPAIR - OUTER SKIN NOZZLE CENTER ENGINE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 Mic l f^, , , ;,..- c-• PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (Ust speak sections) CAR 4b.300 .304 .305 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Regulations, examined in accordance with established by direction of the Adminislratce and In accordanoe dab fisted above and on stincned sheets procedures and found to comply all applicable Reconmend approval of these date Amon, dust data with conditions and lirnitathns of appohtment numbered De t‘ d have been requirements of the Federal Aviation Regulations. imi I We) Therefore 12g) SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES FAA Fonn 8110-3 (11.70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 SDNYGtvl02759899 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246821 EFTA01331284

SDNY_GM_02759900 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246822 EFTA01331285

JWG 97.084 U.S. DEPARTMENT OF TRANSPORTATION . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JULY 28, 1997 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. I 727-100 TYPE (Airplane. Nolan. Helicopter. etc.; Airplane NAME OF APPLICANT Associated Air Center UST OF DATA IDENTIFICATION TITLE Drawing No. Autopilot Interface Unit Modification W/D. ----------------------- Note: (1) The above data is approved for the electrical/ electronic avionics design aspects only. 97-2211-210 ,---e" Rev -- Date: 7/28/97 and PURPOSE OF DATA To Support Major Alteration on S/N 20115 Only. APPLICABLE REQUIRLAIhNTS (Dot specific sections) FAR 25.869(a), 25.1301, 25.1431(c). CERTIFICATION - Under of appointment under Part 183 X X X X X X X XX have been authority vested by direction of the administrator and in accordance with conditions and limitations of the Federal Aviation Regulations, data listed above and on attached sheets numbered examined in accordance with established procedures and (mind to comply with applicable Regulation,. Recommend approval of these data Approve these data requirement, 01 the Federal Aviation I (MIS) Therefore tEl sionATune(S) OF DESIGNATED ENGINEERING REPRESENTATIVES) DESIGNATION NUMSER(S) CLASSIFICATIONS) 94 -rA r—L"—C SW-880 Systems & Equipment ' John W. Goswick SDNY_Givl_02759901 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246523 EFTA01331286

SDNY_GM_02759902 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246824 EFTA01331287

7-23-S7 3:19 PM ;SUPER 27 PROGRAM -• • 6196912232;e 2/ 5 U.8. DEPARTMENT OF TRANSPORTATION PEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE July 23, 1997 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Altplam, AMA liellcopor. et) Airplane NAME OP APPLICANT Rohr, InC. LIST OF DATA IDENTIFICATION TITLE Rohr Inc., EROS C0825 l/ Revision A dated July 23, 1997 • Engineering Repair Data Sheet INSPEU n TI CIN PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. APPLICABLE REQUIREMENTS gmrspeotosectody (1)(3) FAR 25.301 (2)(3) FAR 25.805 (a) (1)(3) FAR 25.303 (2)(3) FAR 25.609 (1)(3) FAR 25.305 (a)(b) CERTIFICATION — Under authority appointment under part 153 of NONE have been vested by direction of the Administrator and In accordance vAth conditions and limitations of the Federal Aviation Regulations, data listed aDove and on attached sheets numbered examined In accordance with established procedures and found to comply with applicable Regulations. Recommend approval of these data Approve those data requirements of the Federal Aviation I (We) Therefore SIGNATURES) OF DESIGNATED ENGINEERING REPRESENTATIVES DESIGNATION NUMBER(S) GLASSIFICATION(S) (1) Jeffrey D. Shutrump NM-2731 structures ifite (2) Tony Bredlaugh-Dredge NM-738 Powerplant (3) Michael August NM-2182 Special Administrative to O•Mfatee br RotV, a a, SDNY_GM_02759903 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246825 EFTA01331288

SDNY_GM_02759904 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246826 EFTA01331289

.4 44,0•44404.440144.4 INIPAMOR C4,14416•04./10 ,4—MPOW. .4.4440.114.114:44 STANDARD PiRWORTHINEES CERTIFICATE 44.0414044.44001.014. 4. 4 G41,40044 05001.3 DODD 727-31 20115 ?DISPORT 4.4 ROa • ,...9•Nocagor.• tll rI•reaut) 07-23-90 LEE R. TR 7 0107 mn ra DM .....04 ./I 4M/P 44, Cm, to. 4144.4.0014= 4.14:4414[0.4444424* FAA Ferro D00.2 ow, o.., ••••••• SONY_GM_0275990.5 TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA _00246827 EFTA01331290

i SDNY_GM_02759906 T TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, EFTA 00246828 EFTA01331291

• ge • MAJOR REPAIR AND ALTERATION CS Onrcsttrco Powerplant, Propeller, or Appliance) • Form Approved OMB No. 2120-0020 For FAA Use Only Office(dentification ,4 ?7 CA 0 a sovccomon (Airframe, hews sewn= . e areUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequ nt revision thereof) torinstructions 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 exceed51.000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Modes 727-100RE Serial No. 20115 Nationality and Registration Mark NSOOLS 2. Owner Name (As shown on registration certificate) NORTHWEST DELAWARE CORPORATION Address (As shown on registration certificate) Mig ign i,DE. 1;899; 3. For FAA Use Only • 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) x r PROPOSER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. THE LIMITED INC. 4387 INTERNATIONAL GATEWAY COLUMBUS, OHIO 43219 X U.S. Certificated Mechanic /A301541619 Foreign Certificated Mechanic cenificated hermit Station Manufacturer 0. I certify that the repairand/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 requirements of Part 43 of the rAdigion Regulations and that the information furnished herein is true and correct to theaat.ot my. nowledge. . 9:1) 1.11.‘ Date L>, I.- ( s March 11, 1998 ! Signature • 'z IA al . . . Richard R Cady II 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is • GI APPROVED 0 E TED FAA Fit. Standards Inspector Manufacturer X • Inspection Authorization er (Specify) 40 FAA Designee Repair Station Person Approved Cana by Transport -worthiness Grou Date of Approval or Rejection Certificate or Designation No. Si natu of onzed I vld..al • March 13, 1998 IA2185934 . T.W. RITCHIE FAA Form 337 riz-sei SDNYGivi02759907 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246829 EFTA01331292

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirement& 8. Description of Work Accomplished (If more space is required, &trash addltionatsheals. Identify with aircraft nationality and registration mark and date work completed.) REMOVED THE FOLLOWING EQUIPMENT: 2EA. HONEYWELL DIGITAL AIR DATA COMPUTERSP/N 7000700-962. INSTALLED THE FOLLOWING EQUIPTMENT: 2 EA. HONEYWELL DIGITAL AIR DATA COMPUTERS P/N 7000700-662 WITH STATIC SOURCE ERROR CORRECTION CURVE INSTALLED IN ACCORDANCE WITH AES DRAWING .LIST NO. 97-727-500 REV. B, DATED NOVEMBER 3, 1997 PER SUPPLEMENTAL TYPE• CERTIFICATE ST09364sc. FAA APPROVED FLIGHT MANUAL SUPPLEMENT, DATED OCTOBER 27, 1997 IS REQUIRED AND INSTALLED ON THIS AIRCRAFT. WEIGHT S BALANCE NEGLIBLE. COPY OF STC ST09364SC AND MASTER DRAWING LIST ATTACHED. CONTINUED MAINTENANCE PRACTICES INCLUDED IN THIS PACKAGE. END Additional Sheets Are Attached •U.SGsemeet0665Cnalsa035 SDNY_GM_02759908 • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246830 EFTA01331293

THE LIMITED UR0859 RECEIVED U.S.IDepartment of Ttansportation Federal Aviation Admlnistradon -• - MAJOR REPAIR AND ALTERATION (Aidrame, Powerplant,Propeller, or Appliance) Form O AP M8 Int .05;1996 For -AA Use Only °"grIA.001)2k141iiki.S SWO5 /Ctr..- C- INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9.1 lor subsequent revision thereol) for !omwallens and disposition of this form. This report Is required by law (49 U.S.C. 14211. Faiture to repen con result Ina dvil i penalty not to exceed 01,000 for each toch violatIon (Station 901 Federal Aviation Act of 1958). _ . .4. 1. Aircraft Make Boeis g Model 727-81 Seniel No. 20115 NS/3~4y end Registration Mark N50015 2. owner Name (As shown on registration conilicate) Northwest Datawire Corp Address OM shown on registration certilicatot 1105 N. Market St Nilmington, DE 19899 3. For FAA Lise Only 4. Unit Identifieadon 5. T pe Unit Makt. Model &dal No. Repelt' Altaration ~FRAME -------- -----(As descnbad In Item 1 above) POWERPLANT PRATT & WHITNEY Turbo Fan Engine JT8C-7B P654373 X PROPELLER APPLIANCE rype Manufacturier 6. Confornity Statement A. Agenty's Name and Address 8. Kind of Agency C. Certiflcate No. Greenwich Air Services - Texas, LP 9311 Reoves Street Dallas, Texas 75235 U.S. Cartificated Mechanic • RA1R445K . Powerplant Class 3 Accessory Class 1,2 and 3 Foreign Certineated Mechanic X Cenificated Repair Station . Manufacturer D. I certily that the maak endnor alteration made to the unit( ) identified in Item 4 above and described on the reverse or attachments hereto have been made in accordence with the rei:lui:amens of Part 43 of the U.S. Federal Aviation Regulations and that the Informatica furnIshed heroin is true and correct to the best of my knowledge. Date /c) - 3 .0-7 Sin I, Authorized Individual 24,47,1--- 7. APoroval Return To Service Pursuant to the authorlty given persons specified be w, the unit identified in item 4 was inspected in the menner prescribed by the Administrator of the Federal Aviation Administration and is Exil APPROVED n REJECTED BV MA Rh st-evas mouw« aterstessw asmoren Aulhonvelen orer Iltmayl , MA gedane* x filIPM• §. uilen ~os isoweed °T Truien Canada Afrwereeent Onno Dato of Approval or Rejection / O-30 -fr i.‘ Certilicate or Designation No. Signa f Authothed in ividsal RA1 R445K .---- de' • SDNY_GM_02 759909 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024683I EFTA01331294

ZE89N:00- Vin LT Pue 'ST 'OT '6 '8 7. SHdV2IDV2:1Vd 8302:10 3ALLD31021d 011J3f8fS 01.66SLZ01^/0ANOS 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 Of more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) • Engine S/N P654373 was removed due to "SERVICE BULLETIN COMPLIANCE." • Engine was disaSsembled, inspected, repaired as required in accordance with Pratt & Whitney JT8D Engine Manual (P/N 481672), and Greenwich Specialized Unit Repair Workscope which are data approved by the Administrator. Inspected/reinstalled Combustion Chamber Outer Case P/N 542155, S/N 243, T.T. & T.C. Unknown, in accordance with P&W Alert S/B 6228, Part I and Part II and AD's 87.11.07 & 95.08-15. Ps4/Drain bosses require reinspection within 6000 cycles and at each Engine shop visit. Rear flange requires reinspection within 12000 cycles and at each Engine shop visit. Case meets inspection requirements of Part III of P&W AS8 6228. Continue timed combustion chambers. Complied with P&W Alert S/B 5729R2 and AD 87-14-01R1; immersion ultrasonic inspect C2 fan blades. Complied with P&W Alert 6038R5 and AD 94-20-01; corrosion inspect high pressure compressor disks. Complied with Pratt & Whitney Alert 5/8 6196R5; #5 bearing seal assembly. Improved oil return & compartment sealing configuration. Complied with P&W Alert S/B 6110 and Alert S/B 6131, AD 94-20.08. This terminates -reinspection requirements for P&W Alert S/B 5913R6, AD 93-06-05. Engine was preserved forshort term storage IAW Pratt & Whitney JT8D Engine Manual (P/N 481672). Engine was subjected to a test run; a post-test borescope inspection was performed and Engine was accepted as serviceable. Engine TT: 32939.0, TC: 22557, TSR 00:00 CSR 0000. Pertinent details of this repair are on file at this Agency under W.O. UR0859 .2 n ADDITIONAL SHEETS ARE ATTACHED FAA AC 72-4906 EFTA01331295

Og, MAJOR REPAIR AND ALTERATION us Demmer* ClbetzgaMen (Airframe, Powerplant, Propeller, or Appliance) Iredsoviitelellat AdmitMilan Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification SO.FSDO-°9 INSTRUCTIONS: Print or typeall entries. See FAR 43.9, FAR 43Appendix B.endAC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49U.S.C. 1421). Fadure 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 Boeing Model 8727-31 Serial No. 20115 Nationality and Registration Mark N500LS 2. Ovmer Name (As show,, on registration certificate) Northwest Delaware Corporation Address As shown on registration certificate) 1105 N. Market Street Wilmington, DE 19899 3. For FAA Use Only 4. Unll Identification S. Type Unit Make Model Serial No. Repair Alteration AIRFRAME *(As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer S. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. ST Mobile Aerospace Engineering, Inc 2100 9th. Street, Brookley Complex Mobile, AL 36615 U.S. COMM:Sled Mediank MZAR013L Airframe Limited Foreign Cenifiatee mechanic X Calif kated Repair StallOn Manufacturer D. I certify that the repairand/or alteration made tothe un t(s) identified in item4 aboveanddescribed on the reverse orattachments 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 November 25, 1995 Signature of Authorized IndivId Clarence Spencer im.......______ 7. Approval for Return To Service 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 SO APPROVED 0 REJECTED BY FAA Rt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection November 25, 1995 Certificate or Designation No. MZAR013L Signature of Authorized Individual ---.. Christopher J. Hil • FAA Form 337'1245) SDNY_GM_02759911 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246833 EFTA01331296

• 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.) Installed DeVore Aviation Corporation tail flood light installation in engine pylons in accordance with De Vore STC ST09113AC dated 26 May 95. DeVore Top Drawing List #72700003DL Rev "A" dated 5-30-95. Installed Valsan Wmglet Modification in Accordance with Valsan Master Drawing List #VA000007, Rev "N" dated 17 April 1995. STC SA59381%1M. Aircraft Inboard and Outboard Aft Flaps and Ailerons rigged to endure fimctionality and conformity. Aircraft weighed after modification. Weight and balance data provided to customer. Aircraft total time = 31,197 hours. Total cycles = 21,345. END'. O Additional Sheets Are Attached •USGPO:199OO4011-012/400O4 SDNY_GNI_02759912 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246834 EFTA01331297

O AND ALTERATION Fs.", APPrOved OMB No. 2,20.0020 MAJOR REPAIR vlosemen Fot FAA the endy Olicreasso. (Airframe, Powerplanl, Propeller, or Appliance) 11141•6111fill•••• iilleil•MISI, 15472 ,11:flo i INSTRUCTIOIRt Plint CWIY00 tutentriet Sn FAR OA FAR 43 Append.. B. and AC43.9-1 (Ortubsequient nnision thereof) tor instroctkons Ona 014.01.06on ol Mai loin. T ho rop0,11•18.410nln bylaw (401.1.S.C. 14213 Fe luntIO report Canmolt i • cml palony not io oliaila $1.003 kw Mól SKI% allabOa (Section 901 Faleni Aelobon Act ol )9:43 T. lee eaCiA/6- Yodel 237.r7 - leb Seed Mt r; o H s••••••• Nosionety end Reoisliotion Mark A/52 , 04. 5 2. Oa Nas (As *Own on tivairgn cartitIcS) 4 4" ha tata /401..D/445. . . , - Si (As shown on regettrollon catraltalit) r.O. ?ok 1138 aii.sverifinv 31e. /9A3 S. For MA URI Olik - • . '..' ":. •:;•4\3, .N.3.;4-34 N:O ..tib4.!`7':•. • ' , . . 3,4 A ','. ,, \..r,e tr.'34. •.• St .7!, ...r. : t .. . 3. • ' • — 4. llell Idiellsellso • '''' ' e. 'TYPO Unit Melee Rend Mention . —.., • (As in ban I 4000VJ AdiFRAUE tbactited '.. . • POWERMANT r • -.1.4. . :-.*„"..- , ..... • PROPELS r !... .\".. , -`2."09,16 ...C!.:., • . - MMMCI 9brs . epOtt iOret' /IYA, 4406 OW 49 V (ATA 160 '1106 173 e ? X la ri lryea CCOnlornilly 414ffileard A. Agency* Moe and Adding * . t Kind of Arony C. Condlcolo No. -gr Zatirefaisti . • • us c........ mowne ,...............c . 1 :V3e2 s/a.. ........... s.. .2,7 ..) Je 593 5 ari-4393uś ofĄ0 4132 /t ..,..,.,,„. D. lennon‚ aha %hemom ondier alletetIon made w the tainl(s)idonlilOP3 him boon ~Je in occortlance 4/41. the niqUinlonntsb Ismonvd Iwon 4 eve ona correct to UV 0•01 01 toy In ItOfn 4 •00•• woO °flatbed on OW rOvIna• of anocnnwonungrolo ol Pen 43 of de U.S. Popersi Anaben asouleeone ano Inst IM vuoimation ..._.... • . De onW 71779 (i .. Ind, - Apr *epilog RetuniNo Softies . PUMAMI. 10 Ule solne/ay gnom poisons sooplied bolos. the r identiliain kun 4 was inloo0441 in the manno/ plesenbod by Ow Assmovonnoo eino Fas Anilan AdnIOWal N. lOn end. APPROVED O REJECTED PAA Ell.Slenderds illvaiponbr MOnolOant" X InKfOCOOn Aillh041/MiON Oltor (SPOIW BY • FAA Delligre• Ropier &OCR Pelson pea by TunsOon real. Awto one i auta O•uperArrernereasposon 7 /9/ 9 Cił Grafitowe/ Dronation No. _1.4-a iss.-crw . mew um fled :non. ... - . .. • ........... .... __ . , I i i. o. ...Je m, ba. ... '••••• anKaisi".••antaflahDealtataelefaagialikraggvi , 1• 01hal SDNY_GM_02759913 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246835 EFTA01331298

FAA AIRCRAFI REGISTRY CMIEIU R0. 3 DATE: je/r/i NOTICE Weight and balance or °fleeting limitation changes shill be entered in the appropriate 'bore t record. An alteration must be compatible with alt preyiOus alberstoons to assure continued conformity with the apPfloalg• allwOrthatods redulremenld 0. Description of WO* Accomdlisned (II more space teound. attach addaronat sheet Identity wen aircraft nalOneary end reaustralson matt snd ale work COmSdritd -rev 9,04,4,bio—ri -kierhse.39--Ar alvise.,4-oet• 72) A- 74, 10660/0.- 964 (Roza.) 3y••:;9—: -. zugatotrestnver • Mmc- yevetz_ c4:2462;m5-.544-1. 4..--‘ atirGefre-D Ai INC fririctIle2> /1/4 44Xtralbvar 23e 4)/ 7VP. A.Z. Grit -0 /-041 t . • - .Sys77W a 345) oPerOrieWhia, Cifeezetzn SS. *Sow -34-Seat• 'rev 1 mere) ..1747/984. 440e.hg- nov.focc.Av hearrAte" la-v2...05 awely 27.9,4). ?A .M4' or AD 90-eil-osi dew. 59 -8784.:. "Ok.14,4400,9- 23422.-er 11,46" ihraelle 4.7). 317-/illgaTt. Aveat-Penem-Ver: einoy. .ofi 755s. AD. n 774,- Aay.4.rr- reisor Afthink_ SIAlatoar. egnade 17e- .177-4e- web r407- c6rrez. Affiedyrami6 I II:1' APPArtall_ or Agent•Wer mews err" CeilPtionvete • i i... • Oaf ' I t-:.• . tn. Alt Fit.) e j l , • • )' " LING.es\ \,-••, %)"O1\1:\ -7" Te1/4 Se t' • 031'•••• ••• • '<Irv, • •* t.o to...eh/v.101 no tetiliC irdpoe ront • moil . ::(ti "aIdot sbora CyilOvl ervoibro rt. • nrns mil 1. I4In tnnItInn41* i• i In St nn,' stilt" I roil Alio minas, , obits. ' sr-S`c‘o: yvi to Roe frL PI 13411:0 . el tin...mi.. i .it • SI\ t Of yd lortlioolovi Winos yeti toniiitgrol µw p NO .v Die;g1tt wit v soss..0 711 .11.7/1 Lt Ont'Oliqua is• a WIC driloiltbeilIDS 1I *VA p.atn - • "- 7. I X ; tooii AM tm { .11Wrt. ri1C;TPi 6131.1• • n;s its..„„,"0 . I...mm. 4 Ain •• Oberon entoiAiSioo4J .0.7y-oz o nit to;ii..;;;Col Or nom SWAM dakalidnrisQ4 Sri • " ‘• 1n., • SDNY_GM_02759974 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246836 EFTA01331299

FAA AtitteAFT REGISTat CAMERA No . ,3 DATE t y/r/fr TRANSPORT AIRPLANE DIRECTORATE AIRCRAFT CERTIFICATION SERVICE 1.04iANSELES AIRCRAFT CERTIFICATION OFFICE f. • A229 EAST SPRING STREET LONG SEAM CALIFORNIA 40006-242.3 Honeywell Inc. Air Transport Systems Division ATTN: Mr. F. W. (Will) Lynch " 21111 North 19th Avenue Phoenix, Arizona 85021 References: a) Honeywell letter, dated Fe5hary 17, 1994 b) Honeywell letter, dated March 1, 1994 • Approval of an Alternate Means of Compliance • ig response to your letter of March 1. 1994, our review of.the data submitted fh'support of a proposed alternate means of compliance with paragraph C. of AD 94-01-04 regarding Conversion of Honeywell TCAS II part No. 4066010-901, -902 and -903 (My Mod) to part No. 4066010-904 (Mos G), has been completed. We concur that method and procedures outlined in your revised Service Bulletin 4066010-34-SW16 Revision 1, dated February 17, 1994 provides an acceptable level of safety in accordance with paragraph C. of AD 94-01-04 Docket No. 93- MA-68-AD; Amendment 39-8786. further question, please contact Mr. Abby Alan Y. Shinseki Manager, Systems and Equipment Branch 1.% SDNV_GM_02759915 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246837 EFTA01331300

FAA AIRCRAFT REGISTRY . CAMERA NO. 3 -. DATE; -90,/f/ir IT01264Ili 331V*2 V.O/T477.1CH.1:1 ;:!;:7.:51;f4 :!1.31.144 tfLt DItTr.M.:" 771S-a01:;;' .1O".39 A:10.1 • • W.t. r VxvaI.1;41PU • re..?".noli14. • nonotrAlo^lh'i nri0cm::-rtn:A. .': II:fit A: . CS2C! •srioshr. ... .. • v•Hon- r: /0 Ltig';.!* :74.scrtnlifit.bpiooll. 5 to .71tc,!ur ;Cr ‘• ;0:4 a9)1! II WI II:4rcsr.O1:1.6 'notroinoT ottirzgrr : .bn,nIcco? notqi fl.d uel)':•912-0103":". .cr-hng (1123‘a10_,:cr:- • atiurruti nty-H2 betl..401.iuoi nt nnntf;uq zvinnzinicf•iiisiboil/Orn indf :Own ofgetqq”c 1t flasittil( Mir Klcrviv% b1sb :f .r171 III.12-'+C-0100itC) •••:?•.on neteutr.o-ttr fil, nt •••.,,,t/.... 10 fi v9! • • F ,7;1!I.V.: .1 ".t.C!, bns SDNY:NA02759916 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246838 EFTA01331301

• dew. FAA AIRCRAFT ltGISTZT CAMERA MO. ,3 DATtt "6/9/11 5- sit -; : anitwoRTfitiiEss DIRECTIVE FLIGHTSTANDARDS SERVICE REGULATORY SUPPORT DPASION olTransportMon P.O. BOX 26460 Federal Adage° • OKLAHOMA an. OKLAHOMA 73126003 Admits's:n*6On •••••••... 0•••••••••111. Ow /SS *OS Mkeittet aisSio• a s•r ar r 0.1./SAMmak•Paosea 0 . 0 ,m•••• • ...i.e. sea bass mow we as IlkeSts dolmans". es•Snip•••• sialeaussl i•••• •••••••v__ amt... IP. PO pawl WIMP mai bluer milemo••••••0•••••••••••••••• ••••••••••••••••••4 es sq.•••••a0kahm 0••••••• Mary 94-o1434 HONEYWELL: Aniersdnicist 39-8786. Docket 9$411.1.68-AD. Applicability: Traffic Alert and Collision Avoidance Speen (TCASHI computer units: pert numbers 4066010.901. -OM. and -003i as installed on, but not limited to, the goliowtragittrpiiia testthested m an category: • Airbus Induatrie Model A3OO-6OO. A31O-2OO. A31O-3OO. A32O4.OO. and A34O Maim Mrptusees Boeing Model '727.100 and -200: 737-100. -200. 400. -400. and -500: 747-100. -200. 400. -400 and 747SP 757.200: and 767-200 and -300 aeries enplanes: Cessna Citation Model 0550 end 0560 eerie, airplanes. and Omens Citation Ell and VU series airplanes: Canadair Challenger Model a-800.2516 and -2.0112 saics airplanes: British Aerospace Model 125-8OOA: OM/stream Model GIL 0 LLB. CIO. and GEV Genes airplanes: -:• • 2r47, Lockheed Model 4101 l series airplanes: McDonnell Douglas Model DC-9-1O. -20. -30-. -40 and -50: DC./ 0-10. -15.30. and -40;.,,:4 MD-11: and DC-9-8O series airplane& and Model MD-88 airplanes: . . • Dassault Aviation Model Mystere•Paloon 50 and 900 arias airplanes: . i I • Short Brothers Model 603-60 series airplanes: de Havilland Model DHC-8-1OO and DEIC-7 series airplanes; iiti f Fokker Model F27 series airplanes: and Corporate Jets ]lotted Model BAe 125.8OOA and Brio 125-1OOOA series airplanes. —••••• • Compliance: Required as indicated. unless accomplished previously. • To prevent collision, or near misses caused by isionnpatibility between the TCAS U prooraeors and the current au name control system- accomplish the plowing: (s) Before December 31. 1994. accomplish the requirements of paragraph, latilnuad • . al(2) of this AD in accordance with Henri/ell Service Bulletin 4O66O1O-34-SWI6. -dated 3. December 20. 1993. • Iii Remove ranting Honeywell TCAS U computer units. part numbers 4066010-901. -902. and .903. and replace those units with new units that incorporate updated CoMskin avoidance system ICAS) logic, kleuttiled es Version 6.O4A in Mitre letter FO46-1.4O69.id dated September 21. 1993. • • L21 Modify the computersuricIllance {ogle on Honeywell TCAS II computer units, • 1 put numbers 4066010.901. -902. and -903, to ensure that these units accommodate Mode C • altitude input o( 1OO-foot increments and that the system will be tracked and coordinated by Intruding aircraft when the Mode S transponder CA field Is act at CA•7. • (bl-WPrtor to Anther' flight 'after accompUshin,i the requinneents- otperageapir (eat this?. -.W.—nrylle di/ ittinrie. night -Maittlitl"ant) 'ol'AFM- Suppleoient. hing'dthees l °Obit paragraph (bX II or (On) of this AD: (1) Revue the Normal Procedures Section of the AIM to include the tiFiroPelete TCAS operating ellaniCtertst1C relative to the modifications required by paragraph (al of this AD. In acconianee with a method approved by the Manager. Los Angeles Aircraft Certification OOIce (iCO). FAA. Transport Airplane Directorate. Or 12) Revise the Normal Procedure Section of the AFM. to include the following! TCAS operating ellaineterbtle relative to the modification rundrod by paragraph (a) of this AD. This nay be seem:mit/had by Inierting a-copy of this AD in the AFM or AIM Vi e: • 1' . F 5. SDNY GM_O2759917 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246839 EFTA01331302

)3. • .• . . • • . l',',4 1,3 .4'istg;141r3totA!anizailaaas;y: . : It • T...., fx • • . ' 'All Resolution Advisory (RAI and Traffic Advisory (TM aural asesstallea arc Inhibited at altitude of less than 1.100 feet above ground Iced (Mal daubing. and leas than 900 fed AGL deweealing er1 An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used If approved by the Manager. Los Angeles Aircraft Certifleatiota Office IACOL FAA. Transpert AlrpLaae Directorate. °pennon shall submit their requests through an appropriate FAA Principal Avionics Inspector. who may add commenta and then send it to the Manager. Los Angeles ACO. NOTE: Information coneenang the cdretosce of approved alternative methods of compliance with this AD. If any. may be obtained from the Los Angeles ACO. (dl Special flight permits may be bowed in accordance with PAR 21.107 and 21.199 to operate the airplane teaks:an= what the requatments of this AD tan be earorepliaD•A • (el The replacement and modification shall be demo in accordance with Ploneywell Service Suntan 4068010.34-5W16, dated December 20. 1993. This Lacorparalloa by MkSIZEkte was approved by the Director of the Federal Register is accozdano: with 5 US.C. 5521a) and I CM Part 51. Copies may be obtathed hem lioneywell Inc. Commercial Flight Systems Group. Mr, Transport Systems Division. P.O. Box 21111. Phoenix. Ancona 85038. Copies may be inspected at — the FAA. Transpen Airplane Directiemtc. 1601 Lind Avenue. SW.. Renton. Washington: at an FAA. Transport Aftplarie Directorate. Lee Angeles Marna Certification 01110t. 3229 ,East Spring Street. • Loos Beach. California: or at the Ofnce of the Federal Register. 800 North Capitol Street. NW.. suitc 700. Washington. DC. (0 This amendment becomes effective on February 4. 1994. FOR FURTHER INFORMATION CONTACT: Abby Melina. Aerospace ringloo•e. Systems and Equipment Branch. Mitsi-l= FAA. Transport Airplane Directorate. Los Angeles Aircraft Certification Ocoee. 3229 East Spring Stmt. Long Beach California 90808.2425: telephone (31019M-5351; fax (310/988-5210. Tall No. Prod. No. Aircraft/APO Hours • Aircraft Fligftts Date CJCe %O. MI . GI GI I Gill MX. . . • . - NOT APPLICABLE - COMPLIED WITH - DEFERRED UNTIL .,, - . THE ABOVE ITEM IS DUE ON PLEASE COMPLETE THIS FORM MO SE1O IT IN WHEN THE ITEM IS COMPLIED WITH. . N sammum • • 14. 4 1 1 S4 7;* - • - 'off /1•1.fttr:ill pat t • t - • •-• I • •i, • • Tr.e` . :Anil ' al bt , ;:4kini., WI Ha' . 44 ••• • —876/0.4-ffg§ar --- S UBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15,o and 17 EFTA 00244Z:1n EFTA01331303

•IAA AERCEAET RECISTRT CAMERA NO. DATE 8 a- - 0 MAJOR REPAIR AND ALTERATION . Oanoweni ohmomowv (AMrame, Powell:4ml, Propeller, or Appliance) Nowntrateiten m........ - Fenn eaneveg OMB No. 2120.0CE0 Per FAA Lem Only °tilt...V:14'9110-15 INSTRUCTIONS:Print or late eat entries. See FAR43.9. FAR 43 Appendix EL end AC43.9-1 for suissequent revision thereof) for instruction and disposition of the form. This moon is moulted by law (49U.S.C. 1421). Failursto reportcan resort in aciriNnalty no110exceed $1.000 for each such violation (Section 901 Federal Aviation Act of 1958). , 1. Altar Make BOEING Model N. 727-31 : I Soma No. 20115 Nationality end Rsoesustion MW NSOOLS 2. Owiwor Marne (As mown on tegISNIAIOn artflkika) NORTHWEST HOLDING CORP. Address (As shown an migration cortzikats) 1105 N. MARKET STREET WILMINGTON, DE 19899 3. Far FAA Use ofty 4. Unit identification 5. Type Unit WM Modal Serif No. Repair Alterman AM RUNE (AS described in hem I share) . X PCNIERPLANT • PROPELLER . • APPLIANCE Type • Mansdalurer IL Ceniareity Itatemme A Agency's Herne and Acklins O. lid A Agency C. Cirtificade No. PAGE AVJET CORPORATION 9809 TRADEPORT DRIVE ORLANDO, FLORIDA 32827 U.S.Cesiikated easchame ' OSORA25M Foreign Ceslareo sfecherde X Consume Am.' Slay. Menuleconer D. I certify that the few and/or alteration made to the un't(s) 'dent,' ied in item 4 above and des< ' me reverse or attachments hereto have been infra in accordance with the requirements of Pan 43 of Ow U.S Federal Ana egeta end information furnished herein is use end correct to ihe heel of my memos.. Date • • 20 79) err /9944 Signature of Authorized Indi --..„, e.i....iragmbge- va.,,,) • 7 Approval ler Ran To Sereloe Kaye 1 to the authority Oren persons specinsa below. the It identified in kern 4 was. Inepeeled in the monster proectibed by Bp Apronistnnor or he Fothemi Ayisnion Administration end le I APPROVED 0 REJECTED - FAA Ft Standards Inspector MSnufsctunor Inspection MAhorizetion Cam (wry) BY FAA Desiree X Repair 51.1105 Person Approved.by Transport Carod y rross Group ... Retention Cenamtte Strew. Author:LS DM* of royal o 0 g / C/ - g or Ossigneho- No. 0S4R4251( geedrictms as ) C „ •-•• SDNY_GM_02759919 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024684 I EFTA01331304

CAA NO. 2/1 DATE: !U-/h2- yr.[ I FAA AIRCRAFT REGISTRY NOTICE Weight and balance or opera NV limitation changes shall be entered in the apPlaCdiste Wiesen secede:. Satirisation must be compatible with all previous ShOhniCteNrro assure continued conformity with the applicable airworthiness reptanaments. & Deoctiption of Mot Amontplehed mote space is requited attach Additional sheets. hawses with circlet naliOnelay ens 1 registration mw* end date work completed.) 127-31 S 20115 peas 1. INSTALLED A DOANE 6 MARGOLIN EMERGENCY LOCATION TRANSMITTER (ELT) SYSTEM IN ACCORDANCE WITH PAGE AVJET REPORT. PR 41-22 REV. A, DATED 8/15/94 AND ISDI. - 91 -02 REV. 8, DATED 8/10/94 AHD APPROVED PER 8110-3 BY DER MARION SHIN, SCE-339, DATED AUGUST 16, 1994. SUMMARY: 1. PROVIDED WEIGHT E. BALANCE UPDATE. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. 4. ALL PERTINET DETAILS OF WORK ACCOMPLISHED ARE ON PILE AT THIS REPAIR STATION' 0S4R425M UNDER WORK ORDER 60298, DATED SEIMMNBER 2, 1994. • - - END-- a Addlibrolli MOMS IWAIIIChed 0.0041•61-044•01..:03: SONY GM 02759920 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246842 EFTA01331305

-FAA AIRCRAFT IEGISTRT CAMERA NO. DATE: - 4:, . MAJOR REPAIR AND ALTERATION 0 mwmmon wanes- w .• (Airframe, Powerptant, Propeller, or Appliance) • '---Si Miniywow. FormAproosi O1W No. 2120-0020 Few FAA Use Oaly McletePIDO -15 MSTRUCnONSMmt or type all me Mc Sn FAR Alt FAR 43 Anendia & and AC 43 94 Or submmuent mean thateW kw Malmmtims and dimmsitim 0 Mis Wm. T his mpon is maMted bylaw (49 US.C.1421), dims to mph um remit In a WM pmelty ma te encmW WAX kw sun such violation Mecum 901 Envoi Aviation Act 04 1WW. 1. Minna Maim Boeing WWI • - 727-31 Serial No. 20115 Nationality and RegisUstion Mork NSOOLS ' 2. Chimer Nwrie Ms shown on mgoVehon Vindicate) , NORTHWEST HOLDING CORP. Andress (As aeon OM SO 9Wa rtOn ceninhan'n • , 1105 N. -Market Street , Wilmington, DE 19899 1 For FAA Use 4. Unit iderellowdm S. Type ...-, Um Man Model Sabi Nlo. Week Alleinikin AIRFRAME described ,n hem 1 anon) x (As P0WERPLANT MOPELUM APPLIANCE Tam Mensdettwor S. Onsformity StMetnerd A. Arnall Neer and Sam B. Kind of Agency C. Ovulate NO. Page Avjet Corporation 9809 Tradeport Drive Orlando, Florida 32827 ti.S.Ceniecattecl tAichank 08,18425M , Foreln Certinuted klechanie X n Swa Cetered nape. im , Merhttectutet D. I certify that ham been furnished the repair and/or in etwation made to the UMW identilied in item 4 above and den with the tectioliennliti oiPanOot the US. Feder& AN collect to the best 0 my noolnew. mode accordance het0n Is true end Date 2, StPrEivIaa 1993/4 Signature 0 AvenorM0 MOM eaellegre-LAAUT el) L Awmowl kw Rolum To Swaim SICAI Pursuant ACIMM4tistor BY o R. wAnollY Onin persona kinifin Wow, the unit WentilM0 in AM' 4 was Inspect In the manner prescribed by the el 1M Federal Aviation Administration AM is CI APPROVED 0 REJECTED FAA n Standards Mrprct d lor Mmolonum Mg*CtionAulterOWNm aver Minivy) . FAA Desire* I X Rep* Station Cmwda Werair= Date 01Appeoval Or Rejection 2 SEPT: 93/4 toniticoto Or .. Designation No. CoS4R425M SPriat el AO In . A a-- .1 i .esoc÷gL e fr om ... rit1 41 01 ! SDNY_GM_02759921 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246843 EFTA01331306

-FAA AIRCRAFT REGISTRY CAMERA N0.3,:/ DATE: /0.-Ig.-/I4 a. NOTICE Weight and balanceat Oporatind lineation changasShall be entered in the &uproot's"( t advertise-owl An aneiation must be compatible with all previous alunanons to assure continued conformity with the +Placable airworrhonas mammon's. • bescrIption el Work Accomplished Or more space le toptinad. Minh OddrtiOnal shNn. identify with waren nationality and rogweration maw and are work compiled.) • 727-1k SIN 2011 psoor.s. 1. REPAIRED CORROSION ON THE LOWER FORWARD CORNER OF THE AFT CARGO DOOR BEAR STRAP IN ACCORDANCE WITH PAGE AVJET E.O. NO. 53-30- 02838 DATED 8/11/9a AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339,' DATED AUGUST 22, 1994. 2. REPAIRED DOUBLE DRILLED HOLES IN B.S. 940 MOD KIT BRACKET IN ACCORDANCE WITH PAGE AVJET E.O. NO. 53-10-02839 DATED 8/10/94 AND APPROVED PER'8110-3 BY ORR MARION SHIN, 50-339 DATED AUGUST 22, 1994. SUMMARY • 1. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION 054R425M reIDER WORK ORDER 60298, DATED SA Pr. cit. END 0 Additional Shafts Are Allhched cadwadieleModiavOU --- MbNyaoffcg9i2 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246844 EFTA01331307

-FAA AtSCRAFT REGISTAr tahERA No.,W DATE: jogg-,44 fr • 0 MAJOR REPAIR AND ALTERATION scaraienes a bresenceot (Airf faille. Powerplant, Propellor, or Appliance) leasemensis• •••••••••140 Form ApprOved 01•13 No 21204020 For FAA Use Only OffiASIOn DO— 15 INSTRUCTIONS. Pnnt Or fee ail envies. Sae FAR N.Y. FAR 43 Appendix ELandAC43.9d (or subsequent tension thipreog frif irsiruclIons anthespositionol Mb tarn. The report is rewired by law leg U.S.C. t421). Failure bravest can result in a civil penalty not to emceed Et .000 for Nen such vielellan Mattoon 901 Fedorel Armen Act al 19581. • was Boeing Nodal 727-31 Ertel NO. 20115 NatIonelity end Alma?. 2. Owner Nan* (AI Mown on registration aveldicata) 'NOR1MWEST HOLDING CORP. MIdnissIt iftrrIgginrInteE Wilmington, DE 19899 . • t Far FAA Us • Owls • .. .: A Unit Ideallikellee 5- Ins Unit Make Model Wet NO. Etna Mango' IJAPPAME denuded ... in flare I - X (As abere) POWEIIPLAPIT • PROPELLER • V ANUANCE Type . d 0 • Manuesturer • • 11..Cegforolef Illeleibeed A. Agency's Name and Ades . 8. KIM Of Arty C. Cartillosla No. • Page Avjet Corporation , 9809 Tradeport Drive Orlando, Florida 32827 A U.S. Caretcara keer sic OS4R425H . F Cerliscased aschank X Carriatanto Pup it t s andart lianulacktor 0. Id0r1Ity that 1.00 mink and/rmIllt010000m04010 the yogis) klentilied in item 42Snenddescribed have teen nets in &cordon:* with the requirenteints of Pan 43 of the U E. 44410•1Aylati futnished hadan A Ind and correct to the Wee aity luta...WSW on the revere. or Miedunents hereto. Ind that m ion ' .e - DOI ; 2. 6 EP7E/raile. 14; 9 3‘ egnelura of Authoring' Inevid 4,3,6€21"7.4.0>2 ei 4.,/ "it L Award for Ran To Bake Natu011110 Administrator SY IN 101100117 of the Federal persons specified Administration below. Vie unit Mobbed in item 4 was I Win 100 manned prescribed by Ma Xl APPROVED O REJECTED rat Aviation and 'e ' . FAA Ft Standards Inipscior Manulecturet . leveler. Autharialien Othe (Specify) FAA FAA Desiree. X Ramie SeliOn Person by Transport Canada Group Dee of Approval or Refection [2. SEPT 90 Cordlivile or Designation No. OS4R425M Signal ol Auth, 4" gew7i-itn "4 • FAA Ions 337 Ma, SDNY_GM_02759923 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246845 EFTA01331308

•PAA A&'CRAFT REG/SERI CAMERA .:n, ?Ai NOTICE Weight and Mattel or operating limitation changes shall be entered in the appropriate aircraft record. An alteration "lust be corneal:We with elf previous alterations to assure continued conlormily with the applicable airworthiness requirements. a. Owalption of Work AccoorpWhof I mote *KO Pi required. Sank addolsOnal SAM. Identity wan akentt nalkallety and iaglaustion mark and data work compered.) 727-31 S/N 20115 N5001 1. RELOCATED ACCESS PANEL FROM B.S. 1183 TO B.S. 1350 LH AND RH BETWEEN STRINGERS S4 TO S7 IN ORDER TO FACILITATE ACCESS FOR FREQUENT INSPECTION TO TERMINAL FITTING IN ACCORDANCE WITH PAGE AVJET E.O. NO. 53-30-02837 DATED 7/428/94 AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339 DATED AUGUST 22, 1994. SUMMARY 1. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION OS4R425M UNDER WORK ORDER 60298, DATED .2.S.6Pri744 •♦ O Additional Shoots Are Matted eflOPW.9010-61WWilaWDS • • SONY GM 02759924 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246846 EFTA01331309

FAA AIRCRAFT REGISTRY CAMERA DATE: /- 93 0 MAJOR REPAIR AND ALTERATION us innmi alemo Otis demn (Airframe, Powerplant, Propeller, or Appliance) nersammaaa miammatin Fore Amend OMS No. 2120-0020 For FAA Use Only Office Identification 51-ISB0-15 meittiOn ImallO) lor insmmtions a CivilPenalty not to exceed S! WC INSTRUCTIONS: Print ortype all•MnesiSee FARM.% FAR 43Appandk B. and AC 4.19-I (Or subsequent end dig osit on ol MO Ner This mport ra requited by law (41I U.S.C. I421). Falleml0 moon can result i tor sect such violation (Section 901 Federal Aviation Act Ol 19540. d ,ASR Make Boeing Model 727-31 Sera' No. 20115 Netionauty and Registration Math N5001.5 A Owner Name (As shown on cogiartarknarPfloa) NORTHWEST HOLDING CORP. Addrena (AI Shown on respitnnion ['Waken') 1105 N. Market Strut Wilmington, DE 19899 a. For FAA Use &Ay I. tha IderAlkatlen : Unit Make Meal Serial No. Repair Alteration AIRFRAME • • fitadretliddlamie ',teen R '-«, POWERPIANT , PROPELLER APPLIANCE Type -Manulecturer liy.eneerealty 9~ A. Agency's Plante and Address & Kind ot Agency C. CerlAket• No. Page Avjet Corporation 9809 Tradeport Drive Orlando, FL 32827 us. cee~ hum« OSeR425M • Fame/ Ceninesma Immune g Ceramic., name Saloon limulson D. I Certify inn thermal/ and/or iil ttttt ion msd• to the un tO) identified in dem 4 above and insonom on the reverie of attachment* hereto hove been made in eteoidente with the requirement* 04 Pest 43 of the U.S. Federal Aviation Regulations and AN the hrikanation !tarnished herein is IAN end correct to the bath el my nowledge. Date • g l i /S 3 Signature eked Individual /Pbenflt.my V. etc.,,' Y iei‘0 04-; • % 7. Ice serww , Pursuant ' AdmIMstrator Dy tc. the authority given persons awaked below, the unit Identified in hem 4 was InsO/cled In the manner prescribed by the of the Federal Aviation Administration and a 10 APPROVED 0 RE ECTED FAA Flt Standards klepeClor Mainulachow InsORCHOn niAreillizenOn own (Spurr/ , Mk glengen x Repel( SUNK _ Peon AppriAM ini by TranSpen Carsnnes «Mm Gram Date.' royal w emection r.25-/f3 7 CortIlkete or DesIgnellon No. 0S4R425/1 Signal sol Authorised / r oat IC*" di gmea, A -A./Pot vi . '3 FAA Fom 337 Fiat, RDNY_Ohl_O2759925 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246847 EFTA01331310

FAA AIRCRAFT REGISTRY CAMERA NO. IN DATE: 1,9* NOTICE WeightandbalanceOr Operating limitation Changes shall be entered in the appropriate aircraft record. An alteration must be compatible, with all previous alteration: (0 assure continuery conformity with the applicable airworthinest requirements. .5Z 0 U. DeseMpt ono R. Acconosbed (If more space is required. attach echlaionar sneers. Wady with aircraft nationaufrand regatranon mark and dare wore comp...4dd B727-31 • 'SIN 20115 - .N5OOLS 1. INSTALLED HONEYWELL SCAM II SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA309450. • SUMMIT: AIRCRAFT WEIGHT AND BALANCE UPDATED ACCORDINGLY. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS INSTALLED OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. 4. ALL ENGINEERING AND WORK ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION UNDER WORK ORDERS 7492, 8112 AND 9301. 5. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. • • M • '!4!.)21.!:, ' AdeNioneu shateswintaine *US PRINTING orncc, inl-ali-.01210117' MONYMA4_0 926 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246848 EFTA01331311

FAA AIRCRAFT acCISTAT CAMARA ND. 2,r4DATZA 1/ - 4 - 9a • • .- 74% , • MAJOR REPAIR AND ALTERATION vs waine's .. o bovecnoinn (Airframe, Powerplanl, Propeller, or Appliance)`' ' ...•• 4.4,4•4 • ...../........ . Form Approved OMB NO. 2120-0020 For FAA Um Only Office mantill as lc • HP INS trivet IONS: NMI or type all entries. See FAA 43.9. FAR 43Appentli, Band AC 43.9-I (Or subsenuentralsIon thereof) Mr instrucdons and cintioseion oldds Iona This Minn Is required by law (49 U S.C. /42n. Failure to report an coattail a civil penally not toeaceed 31.000 loi tact' such violation (Section 901 Federal.A.Sation AO ol ISM. I. Newel mote . Boeing Model 727-31 _- Serial No. - 20115 Nationality and Registration Mark N5OOLS 2. OsnWI Name (At gammon isolAitallOnnellikalo) r. I Northwest Holding Corporation Address (As shown on rooISItallon OnlificolO) P.O. Box 7138 Wilmington. DE 19803 - 3. For FAA Use Only 4. Unit identification L Type Unit Mae Model Soria No. Rep, Alletstion AIRFRAME (A 0 0 0 I 442, X / POWEILPI.ANI roproun APPLIANCE l ype • • emdochnel 4 CORIOS IllalaiM•II __.., RA ' ,.. A AyusiErs. Mane Mid &Muni. El Kind of AElencY C. Cadilitlite No. u s Caner-nee mown Page Avjut Corporation tent. cmainared meehanic 9009 TY a tItfiius' I. I)i. i VI3 3 entm‘neennmustam • 0S4R425M Orlando, Florida 223327 . - hilmw4clumw • I) I curio, mai 4i..c.4-)Mei aalign ..IIV.400.5 MOO PO Rig imill(4)6026Itilmed ri...e wen ...Jo k a...no... e anis he rectuliammla is....t.Ai swop'. ib buy aid 4.4.0:l to die WM ol my - In item 4 moon and doomedon Int ieverse or allachmentahmoo or Pon 430 Me U S Fmmerd Aviation Regulations and that U.. 4404414H011 knuelcd(le • . ineiv . „5_11LAICr ) •i+ 1 2 17? Sly, owe Le A. i hs...duel 4 met, .KWrigiti- • 7 al km Rouen To Service ewe., to Inc 4,4,....., Ione pqa...4.4 sprcilkad Wen'. the RINI adetiliblia in Awn 4 *es anpacred in ma manner gultricribed by the Adinnisti.oei or the I ouni.a An Iwo AdmInialrallon and Es . ft .AFINSOI/ED 0 Mt EC I 30 az. I AA I II $4440444I. lowalul M.Rlielatluott InilputIANI Aull'OMMICIO °V14, ISPOC.4) LP? I- AA llestonw X !grime Station NOM, AIIPIIned Or IlltinPart Canada Ait *tinniness Grove Vole LA A. Iluvalut Ihneconsit ..:11 NfilLeSt lillip- CcitthCalt Of Demenation No. '0548425H Skilialuly Of AillA00110 Individual fN/ .. a.o.:O hi aer--nant--1 51.0.0 it Lfrnni-sr SDNY_GM_02759927 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246849 EFTA01331312

FAA A/ RCRAPI REGISTIE CAKEIA NO. 3PATZ4 //-4-4a • NOTICE Weight and balance or operating limitation Menges shall be entered in the appropiiale aircraft record. An alteiatron must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness reutorements. g n arl) et Watt Acceenollshed &pee et neutral attach edehloOnia Sheets. Identity with *heist: naloOnahly and reeilltelopn milli and dale were teingthled B723-31 ' 5/N 20115 1. MODIFIED SECOND BATTERY SYSTEM PER PAGE AVJET CORPORATION STC SA309250, MASTER DRAWING LIST PIDL-91.-37, REV. A. 2. MODIFIED ED 805 EFIS PER PAGE,AVJET CORPORATION STC MASTER DRAWING LIST MDL-91-44, REV: A. 45001,5 SA3085S0, • 3. MODIFIED FMS-800 FLIGHT MANAGEMENT SYSTEM PER PAGE AVJET CORPORATION STC SA3089SO, MASTER DRAWING LIST MDL-91-43, REV. A (NZ-9112 SOFTWARE). SUMMARY: 1. PROVIDED WEIGHT AND BALANCE UPDATE. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. 4. ALL PERTINENT DETAILS.Opk. WORK ACCOMPLISHED ARE ON FILE AT PAGE AVJET CORPORATION UNDER. WORK ORDER 9286, DATED AUGUST 31, 1992. END 0 Additional StoatsAte Attached O •• SDNY GM_02759928 -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246850 EFTA01331313

PAK-AIRCRAFT REGISTRY CAMERA no. Zit DATES q- 9a, • 0 " MAJOR REPAIR AND ALTERATION . uSOwaserate atoracarron (Airframe, Powerplant, Propeller, or Appliance) Newt smarim AdwatIvann Form Approved OMS No. 2120-0O20 For FAA tfoe Only 011ice Idenolicauon 30-fS00-15 _ INSTRUCTIONS:Printer rye el entries. See FAR 419.FARA3Apkodis ill. and AC43.9.1 (or subsequent revision Memo() lot insloudions end Oisposnion Of thi4 (atm.This report 4requited by law (49 US.C.14211. Failure IC NOON can topsoil❑in spoilpenalty not lo escood 61.000 for each such viola6on (Section 901 Federal Aviation Act o119541, I. Aircraaal Mee Boeing Model 727-31 Serial No 20115 Notionalily and Registration NW N5OOLS 2. 0•044 Name (Al shawl on rogisitanencerrificon. • ' Northwest Bolding Corporation • - • A4Onass (As shown on enistestion calif aft) , •P.O. Box 7138• - -. - • Wilmington, DE 19803 ... Fee PAA Mee Ord/ - • . ' . . . 4. UnR Identilicalion S. Try. Model swim Met' mention AIRFRAME • -, (Asa bad I I fl own • X ROPtrotAsir . . - • Menem& . APPLIANCE Type WNW B. Conlon ally Slalemeni A A or 4 NOM and &Mem B Kind of Agency C. Conflict,' No. Page Avjet Corporation 9809 Tradeport Drive Orlando Florida 32827 U S Catainataa mautente O54R425M rw«gn Catoicatto hlecninc X Cott/caw Roam stalwn leNectiov D. I Gently Owl Ube tepair andfot alteration made to IN un li at idenithed in ileni A altrotli And deMeibed On UN (erne Or •INCliments Nnolo hate been mod* In eccenwice with iho taqvleornenla of P 11 43 tat Ina U.S Fecletat Aviation RintulaboM and that IN sat ininiOn • Banished baton is his and cot tool to the INN of my nuatledge Dole , •-.-:- 2- SIgnelwe e JOH., 1- at all Nir 7. Ann, Retro To Souk* Pu want to Inn authatity Oven persons IIPICIPod below. In ml Al•ntilta0 in nem 4 was inspected In the manner YeelKbbei by let ib Adauflealat of the Fedei al Ac onion Administration and a (1, APPROVED 0 RE ECTED FAA Fit Standards ilitspuder anulacturer Inapoc000 YonlObiaben BY /AA Charm I Repair Shallots Pet son stormed by rtansoon Cam& AlretifINness GIOIA r ISpOeligi Dale al Apµ Oval et RegicUon Zt JA ), $2 N Cot IbiCed• 04 Designation No. 03411425N SI lure of Aulhonzed I - Ad ak..4.- _MOM H I-frill-tat • AA Fenn la/ •• me . • ' SDNY_GM_02759929 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0024685 I EFTA01331314

NOTICE Weight end balance or Operetta g limitation changes shall be entered in Ms appropriate aircra If record. An aneration moil M compatible with ell previous alterations ro enure continued conformity with (he applicable airworthiness requimments. a. Oneripoon of won iktemopoolloo qt mom space is required. attar, eddilionsl sheets. kleatty with arced, nationally and regiataion m✓t and dew wort comolearil E727-31. LAN 2n1li 1. INSTALLED SUNDSTRAND MARK VII WINDSHEAR DETECTION/GROUND PROXIMITY WARNING SYSTEM (GPWS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA311350. SUMMARY: 1. AIRCRAFT WEIGHED AND NEW WEIGHT AND BALANCE COMPUTED. 2. EQUIPMENT FURNISHING LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS INSTALLED. OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. 4. ALL WORX ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. 5. AIRCRAFT TEST FLOWN BY CUSTOMER AND ALL SYSTEMS CHECKED NORMAL. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. 0 Addition& Shims No AMC'S SDNY GM 02759930 OleneefltieeleIVIII SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246852 EFTA01331315

FAA AIRCRAFT REGISTRT CANCRA NO. iv DAM _ 9 07_ I 0 MAJOR REPAIR AND ALTERATION , usosonses wkwasavown (Airframe, Powerplant, Propeller. Or Appliance) tedani Mamas mi.... Form FIPProved OMB 51).21204Xr20 FAA Only F LNG " or Onkel rhilicsiion 90:1100 -15 . INSTRUCTIONS:PARof type ellantries.Se1FAR 411 FARbAppercla 0. and AC 419-1 (or Subsequent owision thereoll Tor instructions and disposition of this icon This report Isnquhed by low (49U.S.C. 1421). Failure to foetid can result In *civil penalty not to **coed 51.000 toe *fah such violation (Section 901 Cedes* AMNIA Act 01 10!1). 1 likaell Make Boeing Model 727-31 WM No. 20115, Nationally and Regialialscw Mock • . ., N5OOLS 2. /Nome !ulna (As shown on flu mica C•StitiCarin Northwest Holding Corporation Aadtaaa (As *P0PP on geplOration citrialcoN) P.O. , Box 7138•..i.. ! - Wilmington, DH 19803 . 3. Pei FAA Use Only I. Unit klenttlIcelless R 1114/ Unit Mad Model I SOAPING, 'Repair Alteration AIRFRAME , (As OM tad ' Mae I above) X POWERPLANt • i PROPELLER . *FALANGE TYPO Mobilactueer • t Conlertint Ilabtrosel A Agency's Myna end heltinnif fl. Kind 01 Agency C. CeRilltate No. Page Avjet Corporation 9809 Tradeport Drive Orlando Flor da 32827 u I. CA...lawny waving OS41142514 I wow Ovulated Mycboroc x C....fain Raw pas.. . uswisckaa• D. I candy Malilia mow and/0, alientlion made to the unit's) idantilie0 in nano abOra and dantat006 on Ina Mafia 0. anaChinenis Imola have Wen made in atcuidanCts with the tagoLf•Mants ol Pail 43 ol the U.S Fadagoi Aviation Ragullatiani and Mat IN InkirinatiOn larniatiod herein is Ina awl CO4 MCI 10 thll best °tiny nowledge. Date • 22 4 . _AK!, lAtif 1 ..._9 9Z Sawatute ol *obeli/ad - _": Individual arnt.5 r. 191l1- Jr. . tor Rattan Te Sento, Po Mnbn.Ili BY manic ma stithtway &ICH Ones Fade, We Naar* specilied Mow. UM unit identilied in hem 4 was Inspeclad In the manner pintaibil4 by the I bvibliab AOMAIMIMIOn and is B APPROVED CI REJECTED FAA AR 51403.101 Instwv-Wr Manufacturer Inspection Aushorlowon ONMISANOW FAA Designee X Sept, SWOP.. bibtOn App pod by lialnyal Canada Airwoilhinem Gioup OMe ol noon:nal*. Reloction ,p.11.3rh-) (19a Cs/Inhale ea Crosignaton No. OS4R425H Sig Nee of Authoring Individual - .. 41-1,11-,,,,e.4 Ds.) F./ 1471/0/4 I'M% Yuan 337 .o mm e: SDNY_GM_02759931 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246853 EFTA01331316

SDNY GM 02759932- - FAA AIRCRAFT REGISTRY CAMERA NO. /,y DATE t _ q_. 9a NOTICE WHO: and balance or operating limitation changes shall be aniseed in the appropriate aircral record An alteration must be compatible with ell previous alteratiOns to mute continued conformity with the applicable airworthinen regiulatinentS. OneApliantitottAecompialed Of more space Is required. nown additional sheeti tclontily with WiciaknotiOnstity and regulation mark and We work completed.) A727-3I 4/A ,n115 1: INSTALLED- EXECUTIVE INTERIOR IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA313750. 2. INSTALLED HONEYWELL EDZ -805 ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EPIS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA308550. 3. INSTALLED MODE "S" TRANSPONDER IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA309550. 4. INSTALLED JAMCO SMOKE DETECTORS IN ACCORDANCE WITH PAGE-AVJET CORPORATION STC SA313250. 5. INSTALLED DUAL HONEYWELL AA-300 RADIO ALTIMETER SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3087S0. 6. INSTALLED HONEYWELL PRIMUS 870 RADAR SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3086S0. INSTALLED HONEYWELL PMZ-800 PLIGHT MANAGEMENT SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA308950. 8. INSTALLED DUAL COLLINS PROLINE II COMMUNICATION AND NAVIGATION SYSTEM IN ACCORDANCE WITH.PAGE AVJET CORPORATION STC SA3090S0. 9. INSTALLED HONEYWELL TCAS II SYSTEM PROVISIONS IN ACCORDANCE PAGE AVJET CORPORATION STC SA309450. 10. RELOCATED FIRE "T" HANDLES IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA311150. 11. INSTALLED FAIRCHILD II PARAMETER FLIGHT DATA RECORDER IN ACCORDANCE WITIOPAGE AVJET CORPORATION STC SA309180. 12. INSTALLED DUAL 40 AMP HR NICKEL CADMIUM BATTERY SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC 5A309250. 13: INSTALLED DUAL. HONEYWELL ADZ-800 DIGITAL AIR DATA SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA308850. 14. INSTALLED AES AUTOPILOT INTERFACE UNIT IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA309350. AddeVerurl SMell Am Anached SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246854 EFTA01331317

FAA AIBLEAZT ■oGIEUT cans so. i# 6_1_ 9a, rya. • ..a•••••• 'WIN* - PAGE 3 OF 3 - 15. INSTALLED HYDRAULIC ACOUSTICAL FILTER IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA313650. INSTALLED RSSENTIAL POWER SELECTION SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC 5A25985t, SUMMARY•: AIRCRAFT WEIGHED AND NEW WEIGHT AND BALANCE COMPUTED. EQUIPMENT FURNISHING LIST UPDATED ACCORDINGLY:, ALL SYSTEMS INSTALLED. OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. ALL WORK ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. AIRCRAFT. TEST FLOWN BY CUSTOMER AND ALL SYSTEMS CHECKED NORMAL. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. • END- • _- - - _ SDNY GM_02759933 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246855 EFTA01331318

SDNY GM_02759934 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246856 EFTA01331319

• FAA AIRCRAFT REGISTRY CAMERA NO3 M DATE: 9 . Tam AppeOve• lot pt 100p1 APPLICATION FOR untpaine• AIRWORTHINESS - " koncesisa . ==•• coo /....9 CERTIFICATE INSTRUCTION1 —•••••••• typo 00 tool voila in 0.603vem.thete we lorFAA ISO*. dobed Ongietanmay an Repeektv4on• 11500bon0 IDKIIII•lqVire0.440snalladienimi 50FIDIC•iripmperrnA5C0,00115.ccw.th• ll among iall •55053•50.1. • . - t 8 LAIONITAA St) Sc II . ANZLA• rf•VILOI.010•MBE/005; --ti.obEiNG. • a main VOW. 000005/Cad 13.1 - 31 - 47* NM /961 IM 0.000".• _ , 1,389a in •t S§ • d • . ad, iir ir av ir utaldprat ia•te _ tt 2/4 4dniey tyrtr ... 1.1313M.00(h50 . -rrai. - sif t..ta go?C15,5' I. mAIOUI Of 0. 0110011.41II WilpIOS ;MC ou.se; l:^ HOZ/ la it MICOLOT RI "on 00005iM00 iad odr•VA ISIVAT •011JCATIOIIIII MUM 000( Ocin ;Cron aeico• 0•••0 A I r STAkrd0A05•050•04530:1011•Caltfreaston00; l' !NOWAK I I ISILITY I fACIC•Altrd.IIRAMPORI I 1OUCIa I I GALLOON • SI0C04 5.0•OlanalentadillICAIIIi0Intan.50•00••••au I 00.4501k E • RW,ISMYIodes, I COSS; 000 I 6.R. I • I JIGaitut USK PAO IIST•Orns05 a •0004.0•••••50 5 IOWA 50509041003 3 to te0044.0 4 MAUI 'Ws* a.25...... 5 PATI0155510 4 MATHER COP0405 I Co /00%04 Ow CARGO I 000 0050;r1 g . I aftiAgeit Am) 0100.0ftitra S AmaltUM PIALI I 00•4500•4 • LUIPlubil..P. ete005050.014.50 •M0.5.0.0 • 4 wan 5 adv;1154PaliC INIT St0irtY • 10.500.COuPvmdt min IASI I /MIN fLICHT ( 040•1005.50 15101.0.0,0 551105504500 S•0•505 311.054. 1000 Play0,500,0 3' IN/0.5051.1•••••••005 /5151)0•0130.5!•3151 ' eintia MI Iv MI v Ce•ScAra 0.. esevant • a S OMPAMON•adOISSOF ImantuCIATOCAlth Mae. Med ••••Cola • •••••••••• seer 4 •••••••0 CM WORT ' I II intact...woe Hsu.° • °MOW, DeVONWatICNI00005 C i• i 55/0100/09055010,0Stail•CAIC/Oret5•0.1 Ion•50000.0•0. ay Senn anon .55405•.• A.1000/0150 ••••••54 ass cm brake. • woes •••••••••••• II 0lata Pt a i la C wan aaerr #ozzmue- deice'. Dab.EY3 /WA ' tre:sULK a>. ib. I:59X a 0 2.ecAmfer.-720,1 13a.k..mee ngica • N•CAUT 01000ICATC•1•550/C5N•mscawnott...tee.s. •••••••••••..05~' • I .WWII VICMCATO. On HAI C5.070.CAIR WA bat; rdnI*5 04 04.4.5•005" A3We x kno00;m0dSS OwiLtUrtStOwatedairt..A0.(0•050.•••••••••;(00 --1,91)Yo -6)- -I ..,......a.......--- pit ta. X,X734. 1am 4'131v3 NM 1555“1051C.Alln.u..,.... et00•SICarowren il igzi 07-3, /99•0 NOCIt4/T 05•001105•••••••04051.44tt MOMS i C. Y X IVO, IN Sam 03. VIAL /aimed 0 0%00 .299/4. / v 53001.4.8145 MVO's. Non Ilwai.crsa.0.0.00+1 'slew "'" 5'44.7 AV,. 0. C0IIInCATIOlv - I...0; tvwv or I a 0. •••••00•••••••. ese......m.• ad ••• sown atw•••• at". mI me 0.a Ateseaserson nact4.00.••••• 5.0...• IC 004 (.0./.....••••••••0•A MA •••••••••••••Isid 5...05.5kinsiett_ 00 *fa 00 0960 ••• •••• '-'•'•••"••‘• nia.".:77Z-nhe 45. tresei 0 ••••••••0; •••• in• 5/000 5.0••• 544 int ..00005 •rt0/05500;a40 . < CIAll Of APPLICAVON " 0 ;MI ••• ....Pe" T1ucu501 3 i 99° A. He Alidaail 0.30•000•••vg 0.43. 519CCII0 MAD amicalmtlIr itsmalar in- . 4.0...IPAPIll ec. Atha ; . i 1 TARTAR,IZI,Idi in CIIII•CM Ki.04.4.5 CwWew a- COlli•CATICIROWICK.,* C•••••••••• LOMICATIDPU0.01/51000•••CanAta• len d • NICSJ t WNW ACIWCP i i a) .• nor e I tems ' ..c. .. .. - . ti• I Mil lenn•Al4 esvreanets. a dna 5 nee det IntC000ILAII ALOLII5150 • ••••••••d••••••••no41010 knee I la VII sm. re.0.550••• • sthamose•rf 04M001•0110. • 0 .0100 050 .0)40 •54,1055•05005 1. If 0. 405060•••0••t••• ly • 0155• 03•00SSealerel l ' 5.5 7 0•305CnIR 05040;55 s 0 .; I ••••••••0fi COII 1•CaCi NIC•55 • Walt W m M I Irma.. e Iasi f Pm li b I r" Mn 71.7 bfri 6 OGIACI 000 ir r ' .. kb e Uothe - - F5- I\I M , MAdtf••00•560440.015 . CAA mm 11106 ill el; -00145.EttS Pn&Y.OUSCOti SDNY_GM_02759935 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246857 EFTA01331320

FAA AIRCRAFT REGISTRY CAMERA NO) A' DATE: 9 - 27 - 97 • •73 :CM:MO-2U -471.10.1) Ai rir • .......ACTLPRO. - HAW • MS* I Migais 0 mooLICTIONCARTSCAlt IG ral•001010.4410.4~/ MIECEIttlf1OO1O611.y . ANTOVIDPII0OIXT011.1111C10. SYSTEM C.G.KOWITITTOP CIATIII0•113410,POWD101101ISTINOPWS 0•VrtO/AMICATICNI NMI I MO MU I40•00•0.0.01 serontuat 2 2 to 5 G 1 1 i I & .10 5 t A.0.5041P,ON OF AIRCPArt • 11.1t0IMAIDO•040 SWICCACM.0.1 .1.006 UMW MtIMISCR PlGtiTtAlttiMIN• • • 000.1•1010M10411 ji./ Tow otmoranva co WOWS O Kb +moose, To - . n 1101/2 11TURECIAtt . . r'-inaT O. C env Kowa° /0 OK4O.1 g 7.4. *scion Mailittfluthftpol . ' Inns I I COA.OT I IT* 00 I I Oint. rtate.y. 0 TN A.Cian Ott POT WO bit A/YMCAS" •••••000.naSS nCO2041•0114ASIOLLOWS .. . . . . . : ma. • 0. Lcm..G r.t.”.c1,0-....., cc,.....c..•• ..cciesan. 'caw. 24 ... o. ........... ........, . LT: . . ...PT "..... . I. ccranc,„0“_,.........1........s....„..1..0.,: e.a.; 11 4... . ...1.......:6L1.4.- I.' 1,94 nint." ..'S.a., '''' "erear."....."•Xidar...ar"...." .....t..?":..9.1!” ..,..4"..I.e-11.".” ....t r r i ; • .0•04.4 • . . • I. WI • C4.4" 0,-,-"Pnr, .,......^n NAME MO MU WSW 4,, Val 0 C.4..../. *mak • , . ^ O...loir I *a GIMI.Sp.r ~11G1fl IM' . AA fem030•614019040.20400~0.- sl I g f ti el 3168004.<re ' • s . , O . . g . . , . 0 , O s : : : • - o n -I . . : : : : : : : : 7 4.. A.- 1".b. ar- al?It ..""4".. . °"1"4- it aty-m-a -a.. . .. 4-11 A Cons 0 Wpm 6,4 11.Y.-0 iftwouate 0.....i a natal • r La row-emboss V 41••••••••••..../AlemeoMM 1...1), Gareth ~wean .„ a 00.... la... ••••• ."1/4 1.aine• .0 -21 1 1 lf.K1SI4esibe• Mani linos f rut • I Kew woke -Mb . _ „P- spir-f .ctiS§a43 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246858 EFTA01331321

•••••••.— FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 27 :91 IMMO Malt Op 614.e.• eitPARTMOIT OF TRAMIPCSITATION-MOW. AVIATION ADIAOUSTRATION “. • STANDARD AIRWORTHINESS CERTIFICATE. . I Pr lawn , NC I ONOISAC7100I1 WOK N505C BOEING 727-31 3 &SCA.? MIt Wa41. 20115 TRANSPORT ▪ NJTMORITIPMO &WS roo. MUNK, • lidelaalnes aiit• pothmal IOW fed**, ..1104•13 of II] II int [Mg. pap net um*. Omura we w ow. le • 110 Moog M l••• •••••014 rel !oar icresor rem bype •••••N•It Peeler Not a 'a wn. vo OS I. ••• TS or..e. M..* ........P 00" ^"K"C•••ef e,a• • • •••• • • by Seems eta re Grew .ak.nertrweat ON Mare* @..p Si roma Peon t emplet* ▪ WIWI reb CObriTCrl Yrs MOW surnames use,. ar.••••. IV • 06•Imii••• Iona 011•••••• nianann et.N ...ay.... at •••••••••••••••••••• • e•C.• a W fl ew PairlInns eristra••• Oman. Dna •Caleit•••••••••2 a Nati oneeareA.seanopow••• as into* seal •••• I ....Wad ! DATE CSIOLYNCE switire•ar 'A Mt 7/23/90 WING C. CHIN 13t1GNATKINNWOVI DAR-61-FS-NN . lOpeAS.0.4. fir ...And Monica. ow a•pardiSI• 1, <Of Crailp40.000. •atnelela33, Tait r sn THIS rrrrr CATC WS, Ni DYWID • INC Allieltall N ACCOSCONCt %min Met011it 'IMAM • TantlIULMIC•45. FAA Fona $3100.2 SDNY_GM_02759937 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246859 EFTA01331322

FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - - 91 SDNY_GM_02759938 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246860 EFTA01331323

a , MAJOR REPAIR AND ALTERATION 0•00,P.,1 areverves • (Airframe, powerpient, Propeller, or Appliance) Sams ban lavirsenvien Form McKeelel OMIINer Z120-0020 foe FAA the Only Mee lelenDlic p 5 .73 C>A I R ..- 0— 0 / INSTRUCTIONS. Print am* NI ectuns.See FAA 43.9, FAR 43 APPONI,x. E. and AC 43R-I (Or Weerant irnsiOnewneolI lot instruction, end eseemiien Minis lam Misreport's/poem:toy Irm I4R U.S.C. 14211. F ;ere to Tr:Demean noun in • enelperolty nauseated 31.000 for each turn vrotegOnlannon 901 Fedora Adobes ACt of Ise). -1 I. Alston Was B0E1AD Mott* ' . 727 -10D.• Udall No. 20115 i Natiameny ono Registration talwa. N5OSC 2. elite. ton (As Mem 00 tegatstrettoncedlikan). NORTHWEST HOLDING CORPORATION - Adds* IA: abort ors regrstradon cenidcond 1409 Faulk Road, P.O. Box 7138 • Foulkstone P Dela laza, SuitI8a2 Wilmington. ware 1 3. kirsauarosi . t . .. . A IAA monialcoruso Iv TM Unit MO* ,A0001 - Weft. Prep* • Attention AIRFRAME /AS Ss< tea ISM I DOH) , X 1 POWCRPLAtir PROPELLER • — •----• - --•,— 4,,t(ANCE TTIM Manureclurer & Caraway sear -. A. Agency, Anoint) Adore!. e. WOO Of Asiore C. Ceti tate No. North American Aircraft - U.S. Ceneemrameetene , Airframe Class 4 Rockwell International Corporation Fere", Cameos) Alecene Limited Powerplant 2825 E. Avenue P X CAnecerel Reset Serer Class 3 Palmdale. Cat 93550 _Mmuerawer ' NXAR688K 0. lawny mettne repaltenWoralterinne made 10 Oa unite) klenageoln dem oaten end ciliated On On sews* or alteCnmento norm hen Veen Merle in emeorctince Rah Vie leillaftri• of P alt 4341Ine U.S. Federal Avineri ReeuraeMmi Mel I mionnatien (visioned Minn le true and correct to ma bar of my nomMelee. i \ Oslo July 20, 1990 7, anwewe Signature of AuMortal inelnvOlial D. A. Perazzo I Rerun. To Senna. Pursuant to the ountored given Demme umocatect Wow. our urn nennied in Rem 4 as Maker* in lecleenner prime/as' by TO ACITISSItIllOr ol the F•0001 Aviation Aaninimmeon and is 0 APPROVED 0 REJECTED ... . . FAA Fn. SIMINV011 VOSPOCIOf l Menulactiver Other tattecOn Findocuon Aumenzahon . • Y FAA Qesign" k Ian" Swan I iCnrn anadlaAnitsntiVess bYTEG( har cwi ve . r i1 .....:,..,„,„,A.,...on }Cornmeal* a of AUNDIUM) Meteorite, I ' ' / ) . 01H19141/C41 No. ' July 20, 1990 ... NXAR688K U. A. Perazzo' i , . • SDW-GtA 0275993r -- SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002461 EFTA01331324

FAA AIRCRAFT REGISTRY CAMERA NOJ N DAIE: 9 - 27 - 91 • - - SDNY GM 02759940 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10,-15, and 17 EFTA_00246862 EFTA01331325

FAA AIRCRAFT REGISTRY CAMERA NOJ N DATE: 9 - 27 - 97 Is • NOTICE • • • Weight and balance or operating limitation changes Snell be enteral in the aOProprial• aircraft morel Pri alteration must be compatible with all previous attentions to assure Continued conformity with the applicable airwortniness requtramantS. U. oteecnpnon et Went Acton (II mote Ana 4 /.dewed, Identity with aircraft nationality and fit* trati0n mem an; lo completed.) A. Modified Boeing Model 727-100 , Serial Number 20115, in mental type certificate SA4363101, amended September 1, 1. Valsan-Boeing 727-200 Re-engining Document VA000001, 15, 1990. 2. The following drawings and engineering orders (E0's) aboVe document: NOTE: "VA" denotes Valsan Drawing. a. Chapter 24 ELECTRICAL POWER ' . VA240000 A Llectrical System Intl. - Strut E.O.: 003A, VA240007 E Panel-Load Control Center Modification E.O.: & 006 '"-- b. Chapter 28 FUEL SYSTEM INSTALLATION, STRUT VA280001 8 Tube Assy - Fuel Strut Feed Thru E.O.: 100 c. Chapter 48 MISC VA48I100 A VA481200 C VA481300 C VA481324 NC VA481325 NC. d. Chapter 53 FUSELAGE VAs30001 B VA530003 C VA530004 NC e. Chapter 54 NACELLES VA543000 C • 1A543100 D accordance with supple- ' 1989 as follows: Revision F, dated January are in addition to the 101 003A, 004, 005, Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 Frame Assy Sta 1263 E.O.: .101, 103 Fuselage Skin E.O.: 106, 114A, 114, 116 Intercostal Assy - BSTA 1223 lo BSTA 1243 W/L244.39 E.0: 106- Intercostal Any - BSTA 1223 to BSTA 1243 W/L234.06 E.0: 105 STRUCTURE Ballast Weight Installation E.0: 100, 102 Ballast Weight, Support Structure Assy. E.O.: 002,100 Ballast Weight Instl. STA 312 - 360 E.O.: 002, 100 & PYLONS Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 Firewall Rib, Side Engine E.0: 36A, 003A f.' Chapter 71 POKER PLANT. . VA/10000 Mt Power Plant Instl. - Engine Pod V7Z7RE E.O.: 002, 1058, 109, 108, 001A, 104A, 005A, 004, 110, 003, 111, 006A g. Chapter 73 ENGINE FUEL AND CONTROL VAJ32301 K Approach Idle Solenoid Wiring Diagram E.0: 002(Rev L), 002 (Rev. MI, 003(Rev. M) VA732303 0 Relay Instl. - Approach Idle Solendid E.O.: 103, 003, 1008 VA732304 0 Switch/IND Light Instl - Approach Idle E.O.: 002, VA732310 A Switch Instl. - Nose Gear Position Approach idle E.O.: 103 VA732315 NC Relay instl. Pilots Overhead Panel E.O.: 100, 002, 101 h. Chapter 76 ENGINE CONTROL VA7SUUOU A Engine Controls Instl. - Strut E.O.: 002A VA760014 A Drum Instl. - Eng. Controls E.O.: 100, 101 VA760015 A Bracket Assy - Pulley ESTA 100 E.O.: 105 In Aeldattonal Sheet Act AMMO • BUSCIOI•6110443 lit -e SONY Ga4-027-549;i1 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246863 EFTA01331326

SDNY_GM_02759942 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246864 EFTA01331327

FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 97 (2) DESCRIPTION OF WORK ACCOMPLISHED (Continued). Serial No. 20115 1. Chapter 77 ENGINE INDICATING 9A771005 NC Indicator Engine Pressure Ratio EPR, E.O.: 001 j. Chapter 78 ENGINE 11A780000 B VA783010 E VA783011• F VA783013 D VA783017 J VA783024 B VA783028 A VA783101 C. • EXHAUST • Engine Strut Controls Instl. E.O.: 002. Fit Deck -Indicator Instl. T/R Sys. E.O.: 003, 004 Thrust Reverser System Wiring Diagram E.O.: 002 (Rev. G) Support Bracket Assy - T/R Control Valve R/S E.O.: 100 (Rev. E Placards E.O.: 007. 008 Relay Instl. - Thrust Reverser Control E.0.: 003 Mixer. Exhaust - Instl. 727E E.O.: 100 No. 2 Engine T/R Wiring Deactiviation E.O.: 002 • k: Chapter 91 CUARTS VA910002 • A Instl. - Electrical Wire Harness E.O.: 003, 004, 005,006, 007 • VA910008 NC : Wire List V727RE E.O.: 001, 002. 003 •NEW DRAWINGS ADDED TO MODIFICATION • B. Boeing 727 Service Bulletin 727-53A0171, dated December 14, 1989. Subject: Fuselage - Station 1182 Pressure Bulkhead web, Crack Repair and Preventive Modification • C. D. The aircraft empty weight and center of gravity was revised in accordance with Boeing Weight and Balance Manual D6-21100. Weight and Blanace Manual Supplement, VA-CR279 is attached. VA000003, Rev. A, Dated 4-4-90 is equivalent to VA000001. Rev. F. dated 1-15-90. END • SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246865 EFTA01331328

FAA ►IRCRAFT REGISTRY•, CAMERA M0I M. DATE 27 - 91 SDNY_GM_02759944 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246866 EFTA01331329

FAA AIRCRAFT REGISTRY CAMERA NO.? t DATE: 9.- - 27 . 97 . STATKIN 13t - WEIGHING RECORD & CHECK LIST DATE AIRCRAFT MODEL h 72.7-- kV REG. NO. 1 9-19- 5 - C TER. NO. NC INTERIOR CONFIGURATION /Of 44/eiteil AC /eta/We - - T. PERSONNEL ACCOMPLISHING THE CHECK LEST WILL INITIAL LACK IT tra In IN. Amount..... CLOCKS NOT APPLICABLE TO A/C BEING WEIGHED. . 2. ALL BOTTLES (02102.1420) SHOULD PE IN NORMAL OPERATIONAL CONDITION. 3. ANY DEVIATION FROM THIS LIST MUST SE COOR DINA ES WITH CHIEF INSPECTOR OR HIS DESIGNEE: & DR COMPLETION OF PARTS A THROUGH 0 THE FOR E mAN/LEAD MECHANIC OR A ssicp E 0 INSPECTOR WILL CHECK 6 SIGN FORM SE. PORE PROCEEDING WITH WEIGHING. ,-- -- T IC ) FLUIDS Checked rt:ILI r A B. LAVATORIES CLEANED • VACIJUMED • Chick. BY I. !iLLINO. OIL SYMMS • TANKS FULL se 4.) lIct. I.L.41' IV 2. ALL FUEL T KS DRAINED USING ORAI PLUGS WI PH AN AIRCRAFT Livia - mer iPi T. ALL MAGAZINES. NEWSPAPERS & SEAT SACK - LITERATURE REMOVED , y DRINKING 6 WASH WATER TA,IFILE DRAINED an FILLED I... I - sza ifit • .a PROTECTiNE ENTRY. AISLE a STAIR COVERS POISONED K. HYDRAULIC SYSTEMS FULL • • % O. WINDSCREEN STOWAGE EMPTY • CLEAN 'AP -A1= .1,411 tik ••/V ; 0/ 1 q,1 S. TOILETSSERVICED TO NORMAI: QUANTITY .sPrisoy .rf , A Fit ISM. 'STOWAGE COMPARTAIENTS0N FssOft AFT. LAY. '- . OULKNIATM EMPTY I & SEAPLANE&TELY DRAIN Wilt • WINO FLOATS COMPLE : ' • • . - (:) CARGO, LANDING GEAR a POWERPLANT (DI CONTROL CABIN 1. ALL INSTRUMENT PANELS COMPLETE 34 . 1. ENGINE FIRE SOTTLES CHARGED • , ALL MANUALS; CHECKLISTS. LOG BOORS, t FORMES OTHER WRITTEN MATERIAL REMOVED OClie 211# -1 .:Iiit Call sweilATf ACtr oLETE Virm SEAT BELTS • 44., .U.IT 2 ALL ENG HISS cOMPUTE ;E. ACCESSORIES. ' PLUMBING. ETC. FLIGHT ENGINEERSTAOLE EMPTY • ' CLEAN EXCEPT FOR STRETCHER KIT 9 2fig, . 3. ALL COWLING • PANELS IN PLACE • C) PASSENGER CABIN a . 'RAKE AIR 00171-1 CHARGED e sh. • REMOVE ALL ITEMS FROM HAT RACKS EXCEPT 1. MEGAPHONES. FIRST AID tut MOUNTED Oxlf. BOTTLES. DEMO OXY. MASK • UPS VEST IN " POUCH ti O S. ALL AVIONICS GOUIPMINT INSTALLED - is B. a CLEANED FWD. A APT. CARGO COMPARTMENT EMPTY ....Z.Z.; ...Y.; q Pf:1 ALL PASSENGER SERVICE EOUWMENT REMOVE*" . FROM GALLEY II w.S.11 MA OXYGEN SYSTEM SERVICED 2. . IM FULL 3. ALL SERVICE EQUIPMENT REMOVED FROM PRO. • APT. LAVATORIES --. - . - ALL GALLEY AREAS CLEANED a • VACUUMED glat 4 r4 SP; 4' ..) • & MAIN 'PATTERN • AUX SATTERY IM USED) INSTALLED O. yaw DoORS • SAWN= CLOSED • LATMEND 44. - :. ,.-- ' • G. PASSENGER PATEN CLEANED • NACtRIMED „r ip, , o. g ligi ulit INFLATOO TO OtaiLintiO _-W I. PARTS O THROUGH @ CROWD &COMMIE 2. STANDARD INTERIOR CONFIG. EQUIP. LIST COMPLETED r.AIRCRAFT READY FOR WEIGHING r .4 0/4.4 h MSS SIO OLON fredmaniteml Man. O. Paw Forwnw/Losol Mat O. hewn. Foteamn/Lse4 Meek Or Moque, SIGN OFF COPY PAGE I OF 3 • SDNY_GM 02759945 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246867 EFTA01331330

figlifliNigl"R"."4"147.4" . "bcfa*"'" *14 SDNY ;0271994:""ell SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00246868 EFTA01331331