8- 3-99 4:55 PM ;SUPER 27 PROGRAM 6196912232;# 6/ 8 BY B. COX DATE 08/02/99 CHK'D DATE ERDS Cl 036 DODE1 El= ROHR ROHR, INC. PAGE 2 of 4 TITLE Skin Disband VA545300-1 Use or disclosure of this information is suhicet to the restriction on the title page or on the first page oruris document The noted adhesive primer is compatible with the adhesive as shown in the excerpt of MIL-HDBK-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 (f6) is expressed by = 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 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, = .016, t. = .032 and t, = .30. h = .016/2 + .03212 + .30 = .324 in - = 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 no test data readily available for this adhesive system for core bond, e 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 fairing 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. 2 MecheiniU:11 Design Allowables (RHR 85-013) frnreqvo 1-46A- EFTA00277780

• • A • 4 • EFTA00277781

8- 3-99 4:55 PM ;SUPER 27 PROGRAM DODD 6196912232;# 7/ BY B. COX DATE 08/02/99 CIODO PAGE 3 of 4 DATE ROHR ROHR, INC TITLE CHK'D Skin Distxind EROS C1036 VA545300-1 Usc or disclosure of this information -3 subject to Me ie ti Iction on the title page or on the first page of this do:mai/sot ktEleliD331C-337 1 DEsosnlbe.r 1982 I . R PiA- i! i l i 1 1 I e e t 4•- t i t —6 It P V in ti iti. aci I-- la (. II i5 V 4 . la 5 m 1113 g 11 t g 0 Cs l! . --zi • t I g S t, i t ti 5 1 l 4 CC77 Q g cS a r , a v m I- tit - iii _ m , . E 6 14 — c% li 6 s :frt. Set • 0 A r§ E VIE g I IL b . u. rig . LL ag LL DS • _ = > i' = -g .2 I 1 .g " S. -1 i E • 4-4 1%7/1 Ilredi 8 EFTA00277782

• • EFTA00277783

8- 3-99 4:55 PM ;SUPER 27 PROGRAM -k 5198912232;# 8/ 8 BY B. COX DATE 08/02/99 CHK'D ERDS C1036 DATE DODO DODO ROHR ROHR, INC. PAGE 4 of 4 TITLE Skin Disband VA545300-1 Use or dIscIosure Of this Intbrinalion Is subject to the restriction on the title page or on tho first paio of this document CytliCFADAE1 ISICIFirstitowl swat Kowa to 0nu*. kfarSAM2107/3 CSR irrrICAT ON. sow TO VIMCO-LARM CITY PA LA O. BOK 1909 M criry PL. 32066 GRIP VIW2O-1M34 arrl TO EIC;iway 30 EAST • gizaxxnx. Mime= 2cluTE 19. BOX 1029 OUR 'OMER IA= CITY • 0023439/001 PT* 32025 WinOWNt OR131&R 598376 Br* BATaijOrriT taBeiBit 2742-13037 * 2742 B EtsweltjuzysT =Km= TOTAL 1* TEL - turrg 5111sSzo 06/17/99 wait • mAntwacTaRBD =maw UM aum.13,1$)9 500.00 DP taTeR OTY so0.00 t TOTAL OT? 500.00 Tas atinTrzse THE sumotrara AT Trbas op EIBIPMENT OONFORK0 TU ALEIFEXCIUMIK rtalaNGS AWD spEciFiCATIOVS NOT= =WC SpEterisratriarg: 1244-A-132 RSV B, TW(-2 TM x =Ms 2 POEM P GROUP 3 llama 21.O8392VS OR FRU= legrra ACCIPTANCe Bi2 PART or TIM Num 3tragensint rYtngst_ unri ARK ORGY TO metuow WXTR ThZ marumcgo AnCE0strva oapkvAER To Imam caRTnnemoN. saa CSC FOR ASsZ8117Was, * AM 2 ism TzsT D A A 75 P LAP MAR 6584. 5552, 61044 6522, 6122 PEI winGtilrr 061, .01, .061 FISF 8 /£ a:ZUMeggrg rormywn t3I1L3 180 453U, 437B, 405.5# 4368, 45t5 PSX tinDOVd Lz Nef 5S;'e 6B-r -g EFTA00277784

A 3 ..t... al.• • ••• I. S. EFTA00277785

.ra I Work Order 43736. , to MAJOR REPAIR AND ALTERATION iv L.,: c • : i, , ,. !Form Approved OMB No. 2120-0020 • 7- - For FAA Use Only . US Department of (Airframe, Powerplant, Propeller or Appliance) - " Transportation Federal Aviation Administration . Office Id ntification ir.07 ' • '; • r" 4 • . INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, 'and AC,43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make • - . - . ' Boeing .ri :-..,;!•=- ', - Model • • ., , :: 1.,..; :11-".1:1V.,' . ',.. ' • ' i ; • 1 , v 1 727-31 '' Serial No. " S. , •:. • • • 20115 Nationality and Registration Mark • , . • • . .N505LS 2. Owner Name (As shown on registration certificate) I . ' ' ; • i Northwest Delaware Corporation . . . , . .. Address (As shown on registration certificate) • — •• • • .. • • 4 • 1105 N Market St . 1 ' 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, se Lion ' . : . , . 43.7 . 2 z ../ _Zieee GL-CMH FSDO , . ate . . .i •i i attire of FAA Ins ecter esus Zubia • Unit Identification 5. Type Unit Make •• ' Model • • . •• l . Serial No. • - • ,. „ .• . Repair . • Alteration AIRFRAME • • % (As described n item 1 above) , ., 1 I. . • . •• , • 'v• . • , ". ..... .;• i ,:, •I ,li -, r -: r •:•1• •,• ::. i ,: • • • ' . .• X POWERPLANT . , • • . , . 4 • 1 • .••• , it i •i • . . ••• .0. "1. • .1 • . . a. ••• • :6 • •'' ' " t I • • s +'•;i•..••. • • • . . ' ' -. • I PROPELLER . - 5 .,. . Z I ‘, 4 )4" .g • '•`.. I ' .' i let; •qtr. ••• . :1 • .:" ‘:' ' • ••••rvzr;• ;* ' ' • I S : !I' •• . APPLIANCE Type • •,, - • . . • . - I' ' Manufacturer 6. Conformity Statement A. Agency's Name and Address . B. Kind of Agency C. Certificate No. ElectroSonics . . „ . ... 4391 International Gateway Port Columbus International Airport Columbus, OHIO 43219 U. S. Certificated Mechanic Repair Station AEI R005K, Radio Class 1,2 & 3; Instrument Class 3, Accessory Class 3 Limited Altimeter Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U. S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date ' April 28, 1999 Signature of Authorized Indiv• -- _, -• • . - - _ . ., _ • 1 . • • '• ' • . • . i r ..,. ; , ; I • t t • ' - 7. Appro al Ret Service i • - . ' - • • t Pursuant to the authority given persons specified below, th Oriitlid fie in item 4 was inspected in the manner prescribed by the •. Administrator of the Federal Aviation Administration and is. Q APPROVED 0 REJECTED ; ', ..- ! 1 0%,......"• O. BY FAA Flt Standards inspector Manufacturer Inspection Authorization Other (Specify) . : A'Irt‘''..V •. ...N. 1- 1 ' ; ' FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group ,— . ! '1 '1 . I . Date of Approval or Rejection 4 s al -i I - - - - --- , Certificate or Designation No. AE1R005K Signature of Authorized Ind* d al I . 1 : 0 • i • _ ..... • • Q8) EFTA00277786

NOTICE Weight and balance or operating limitation changes shall besentered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • 8. Description of Work Accomplished (if more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKE/MODEL/DESCRIPTION STATION 622-7293-101 3 Collins VHF-422b Comm C37c, C38c 450.0 2. The following equipment was installed in the aircraft. • PART NUMBER QTY MAKE/MODEL/DESCRIPTION ISO ,j= STATION INSTALLATION DATA • 822-1115-001 3 Collins VHF-422c Comm C37c, C38c 450.0 523-0772719 3. The above work was accomplished IAW FAA Advi'sory Circular AC 43.13-1B, 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 8.33Khz modifications Collins S.B.17. Following modification, reinstalled as VHF-422c and performed a complete operational check. 6. A complete test of the installation of the modified units 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 IAW the prescribed loading information from the manufacturer. END • 0-1 S-A S-0 C-1 C-2 A-1 FSDO SITFIVED Col IMBOS. OH C-3 C-4 C-5 A-11 A-10 A-9 A-7 0-1 ■ ;,'-1 C2 S-A S-0 C-1 C-2 A-1 ■ 0-2 , . A-2 0-3 . Ss-,..-,Eivro .A-3 - ... '''/A ' — 3 1999 . • 0-4 A5 ,; 0 5 " A • - 0-6 CM FSDO- COI LIMMIS OH 0-7 0-3 S C-3 C-4 -C-5 A-11 A-10 A;9 A-7 Ali K Additional Sheets Are Attached •• , U.S. GPO:1991-0-568-012/40035 EFTA00277787

p.* Work Order 43736. t . - • . • ;. .,, MAJOR REPAIR AND ALTERATION ' i ' ' • '''•• - ' Form Approved . . ',I • OMB No. 2120-0020 • :. ' • For FAA Use Only l•••'''' - - - • US Dopartmant of (Airframe, Powerplant, Propeller or Appliance) ,, • Transportation ._ . 5.. , . .-,..- . . . - , .. ,..*:.,,,.•••,-- Federal Aviation Administration Office Identification Lk,: QL • - - ' GL0 7 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). ' • - , -, ' - . , 5, , • -, • • • 1. Aircraft Make .,i 1' 1P-ti :.?:; Boeing - - Model , , ' 727-31 Serial No. 20115 Nationality and Registration Mark ; • i , , ' - N505LS 2. Owner * Name (As shown on registration certificate) .. Northwest Delaware Corporation . , , , . - Address (As shown on registration certificate) • .* „1105 N Market St • - . :t., • 1 . Wilmington, DE 19899 ' • 3. For FAA Use Only • 1 ,; . 'The data identified herein complies with the applicable airworthiness , . . requirements and is approved only for the above described aircraft, ,•.• ,- . 7 , -.., 7; • . , subject to conformity inspection by a person authorized in FAR 43, section , .::**,'; I. . 43.7 / • I 24' 77 • —,,(//g" GL-CMH FSDO ' Date . ..4 tr , nature of FAA I sp I Jesus Zubia - ' "." ' 4. Unit Identification 5. Type Unit , Make , - ,I.,, , " r - i ' • ''',.'4, . . .t, :. Model .;r:::. -, .Serial No. , Repair Alteration AIRFRAME , .. (As described !I.!' Item 1 above),, ,. :;1. .. .,..:i.., t ,..,, , ., , - i t X , POWERPLANT • ,,. 1! 5, --- • 1 J.,,, it* ' ‘ ' 't I PROPELLER . • I • 1 t s • , ' • 1, • ' r...1 ' • .; .' • . 1:1 . APPLIANCE Type , , . , . . ., ' . • . , • . • -, 1,, • , ' I Manufacturer 6. Conformity Statement A. Agency's Name and Address, ••" B. Kind of Agency . . " — ' i • ' C. Certificate No. • ' ' ' ElectroSonics 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 certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U. S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date April 28, '1999 Signature of Au orized Indivi i I , • -• ...., , ....... .. .e-- i i , , , , 17..., i , f . i ) 7. Approval or turn o rvice - - Pursuant to the authority given persons specified below, the unit Administrator of the Federal Aviation Administration and is identi •./ in tern 4 was inspected in the manner prescribed by the APPROVED K REJEL ILI) . r q.?1•I --..: C BY FAA Flt Standards Inspector • , Manufacturer t Inspection Authorization Other (Specify) 1...:- t. • -• i • v i • FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group . . I Date of Approval or Rejection i t - ). i -19 Certificate or Designation No. AE1R005K Signa r of Authorized idual ; . , • - . FAA Form 337 (12-88) EFTA00277788

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (if more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 1. The following equipment was removed from the aircraft: .71 Ss, PART NUMBER QTY MAKE/MODELJDESCRIPTION STATION 622-6520-005 2 Collins CTL-22 622-6520-005 '1 Collins CTL-22 2. The following equipment was installed in the aircraft. PART NUMBER QTY MAKE/MODELIDESCRIPTION s .• „ • ; ' , 200.0 259.5 • •'':: i .r; 4 • • INSTALLATION TSO STATION • DATA 822-1120-005 82271120-.005 2 Collins CTL-22c C37c, C38c 200.0 523-0072719 1. Collins CTL-22c .1' ' C37c, C38c, , 259.5 • • .1.„ „. . , . , 3. 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 adcomplished under ElectrOSonics 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 units lls been conducted to confirm that other aircraft systems are free of interference as a result of this installation. All tests found to be satisfactory. I t i 7. Collins does not specify any new continued airworthiness instructions for the above equipment. The owner/operat0r shoUld consult the Boeing •mairitenanc4 manuals- for general avionics continued airworthiness requirements. i I i t 1 i 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. , • .r• ,; .., 10. The aircraft must be loaded TAW the prescribed loading information from the manufacturer. •• 0 0.3 0-4 0,5 04 S-A S-0 C-1 C-2 A-1 A-2 crcrivto , Al l(281999 CMH FSDO C-3 03 , COLUMBUS. OH C-4 C-5 A-11 A-101 A-9 A-3 A-4 A-5 A-7 A-8 END. - •fl" • t It ; 0; • '7 ., •!.C. 0-1 m-i -2 S-A -i.) 6-1 C-2. A-4 0-2 - • . ' - 4 .. . * 1 . • I A.-2 r.ZF.CEIVE'D -• JO 0-3 , ! • :. • •1.iiii,..1.-.3 ' A50.1-0' , 0_5-- ••. • • • - A75 .t-i•IJ ' A 0-6, L. • • 1 • 'MUSKY' ^ • • CORIM•Bliz Oh 0-7 ' C-3 - b=d, c-5 ik:.ii. • ".4-161 i'•9 At7 LL ,......___-_, - 0-8 . • t, . , : tr i • . I • ,-.. .i ,..1.J.:; O Additional Sheets Are Attached , - U.S, GPO:1991-0-568-012/40035 EFTA00277789

MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) of Transportation Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification .e.y.f4.4 490 ,3- 0 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This form 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 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 shown on registration certificate) 1105 N PA S Wilmingtioh; p 93 i 3. For FAA Use Only AUti 1 0 1098 FAA-DILLAS SW05 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME avoraveswer4*~~~0~4•0 (As described in item 1 above) 410010.41~111001~111~~10•4114111 X X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A Agenciis Name and Address B. Kind of Agency C. Certificate No. Associated Air Center 8201 Lemmon Avenue Dallas, Texas 75220 U.S. Certificated Mechanic TX2R203L Airframe Class 3 & 4 Radio Class 1, 2 & 3 Foreign Certificated Mechanic x Certificated Repair Station Manufacturer D. 1 certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 814/98 Signature of Authorized Individual >7# 7b4JWA lvd ri' l— 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is F:i in item 4 was inspected in the manner prescribed by the APPROVED K REJECTED BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee x Repair Station Person Approved by Transport Canadian Airworthiness Group Date of Approval or Rejection 8/4/98 Certificate or Designation No. TX2R203L Signature of Authorized Individual 7-i7, -.49/ti- A- FAA Form 337 (12-88) EFTA00277790

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.) 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. Kimbrell 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 M. Manashi August 4, 1998. El Additional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE 1992-769-012/60157 EFTA00277791

DAK-98-089 DEPARTMENT OF TRANSPORTATION 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 (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPUCANT ASSOCIATED AIR CENTER DALLAS, TEXAS LIST OF DATA IDENTIFICATION TITLE 1565-001 REV. A 07/28/98 MODE S TRANSPONDER ICAO CODE STRAPPING CHANGE • - -••-•• .--- - - ,-. - • . - 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 - --- - .., DATA IS APPROVED. S/N 20115 ONLY. FORM 337. PURPOSE OF DATA TO SUPPORT THE AVIONICS/ELECTRICAL MODIFICATIONS. APPLICABLE REQUIREMENTS (List specific sections) 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 n Recommend I (0) Therefore Approve SI NATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) DAVID A. KIMBRELL ( SW-997 AVIONICS/ELECTRICAL , --- :ni :f1 ; SYSTEMS FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS Eornont( ( COMPUTER GENERATED) GPO 901-813 EFTA00277792

4 t b .., EFTA00277793

AUG-04-1998 10:39 ASSOC AIR 214 357 2845 214 357 2845 P.O1 (1.3. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE #98421 AUGUST 04, 1999 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOZ.ZNO MODEL NO. 727,-31 . TYPE No.& 'to.. hokopasf. rz) AIRPLANE (N5OOL3) NAME OF APPLICANT ASSOCIATE) AIR Cwt LIST OF DATA IDE1471 !CATION TITLE ASIOCIATED AIR C/D1TER DRAIN O NO. 1565-002 REV . "2R" , DM= O7-29.1933 REPAIR - L/ft HORIZONTAL STABILZEER T/E Tipp= REM - ZZXV STA 136. (SKUT 1, 2 AND 3 07 3) . NOTES: 1. THE STRUCTURAL ASPECTS °NIA or THE ABOVE LISTED DATA X= Abl5A0v2D =Man. Titio NW/WV/Lt. IS TOR TEE IINGINIZZRING D191024 DATA O'NLY. 2. MIS APPROVAL IS VALID armY FOR 8=130 MODEL No. -727-31, AIRcRAPT S/N 2O115 AND Is IssuzD Itt SIMPORT OF A MAJOR =PAIR or THE SUBJECT AIRCRirT. PU - - 468E OF DATA IN SUPPORT or A )0JOR REPAIR ON BONING 14013EL NO. 727-31, AIRCRAFT 3/N 20115. APR_ z REQUIREMENTS pa vials; airasom) CAR 4b.20O (a) , (b) , 4b.201 (a) . (10 . (a) , 4b.202, 4b.3OO, 415.901, db. 302, 413.303, 4b.304 (a) , (b) , 4b-3O6 fa) . 04 , (d) . CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered )0000000(XXXXX00004 have been examined in accordance with establithed pnneadunes and found to COmply with applicable requirements of the Federal Aviation Regulations. 0 Recommend Approval of this data I (W) THEREFORE El Approve these data • Illij=gaityk,uzjite,,AL4,14:rivii-ut'ertl- -v 6ENTATiVE S SIGNATioN NUMBE frY4s 0 .. 0 . ek. A SW-910 STRUCTURES Roam — . • •• .. — • ------ 0 .7Q) aupERSIMes PREvIOUI trirrioN ..J a209314I3 TOTAL P.01 EFTA00277794

4 EFTA00277795

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATiON STANDARD AIRWORTHINESS CERTIFICATE . 1 NATIONALITY AND REGISTRATION MARKS N50SLS 2. MANUFACTURER AND MODEL BOEING 727.--31 3 AIRCRAFT SERIAL NUMBER 20115 4 CATEGORY TRANSPORT 5 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that. as of the date of issuance. the aircraft to which issued has been inspected and found to conform to the type certificate therefor. to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein. Exceptions: NONE 6 TERMS AND CONDITIONS ,, Unless sooner surrendered. suspended. revoked, or a termination date is otherwise established by the Administrator, this airworthiness certificate is effective as long as the maintenance, preventative maintenance. and alterations are performed in accordance with Parts21. 43, and 91 of the Federal Aviation Regulations. as appropriate, and the aircraft is registered in the United States. DATE OF ISSUANCE R 07--23-90 TATIVE t DESIGNATION NUMBER ____. GLO7 Any alteration, reproduction. or misuse oft C itti e may be punishable by a tine not exceeding S1.000. or imprisonment not exceeding 3 years. or both. THIS CERTIFICATE M ST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) 1 * U.S.G.P.O.: 1994-568-762 EFTA00277796

EFTA00277797

, .:11, MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, of Transportation Federal Aviation Administration or Appliance) Form Approved omeApre or se my Ifo LAS t S 'iAJOc / (A/C_ INSTRUCTIONS: Print or type all and disposition of this form. This form for each such violation (Section 901 entries See FAR 43.9, FAR 43 Appendix (49 U.S.C. 1421). of 1958). B, and AC 43.9-1 (or subsequent revision thereof) for instructions Failure to report can result in a civil penalty not to exceed $1,000 is required by law Federal Aviation Act 1. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N500LS 2. Owner Name (As shown on registration certificate) Northwest Delaware Corp. Address (As shown on registration certificate) 1105 N Market St Wilmington, DE 19899 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in item "I above) sessesseasseareis X X . POWERPLANT PROPELLER APPLIANCE Type - . - Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. -Certificate No.:- • Associated Air Center 8201 Lemmon Avenue Dallas, Texas 75220 U.S. Certificated Mechanic 7- TX2R203L‘i a • Class 3 & 4 • • Foreign Certificated Mechanic x Certificatea Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified have been made in accordance with the requirements of Part 43 of furnished herein is true and correct to the best of my knowledge. in item 4 above and described on the reverse or attachments hereto the U.S. Federal Aviation Regulations and that the information Date 8/2/97 Signatur of Authorized Individual 4fr it-7--,- i 7. Approval for Reyirn Service Pursuant Administrator BY to the authority given persons specified below, the unit identified of the Federal Aviation Administration and is - item 4 was inspected in the manner prescribed by the REJECTED 0 APPROVED K FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Canadian Approved by Transport Airworthiness Group Date of Approval or Rejection 8/2/97 Certificate or Designation No. TX2R203L Signature of uthorized individual .4-169-4-c--- - Orin (12- EFTA00277798

• wo• 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 (tf more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 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 I/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 8 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 BB 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. SrAdditional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00277799

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la- r EFTA00277801

ARC' 91.1 f. 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. 1476-0011-- 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 NSPEC-1-01\ 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 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 with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered ,/ V X have been requirements of the Federal Aviation Regulations. MI I ( ) Therefore 171 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) 7: JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277802

s I a EFTA00277803

AAC-110 IS-1 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. 1476-002 REV. IR 7-17-97 REPAIR - # 1 & # 3 PYLON CORROSION ON FWD ENGINE MOUNTS 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 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 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 with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered V L7,( oe have been requirements of the Federal Aviation Regulations. I ) Therefore 71 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 1.7 . 4.' JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277804

• II • ... EFTA00277805

RPC°1-1.1SB 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. 1476-003 REV. IR 7-17-97 • REPAIR - # 8 UE SLAT CRACK AT 1/B SLAT GUIDE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 t°41SPFC1-\°N 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 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 with applicable Recommend approval of these data these data with conditions and limitations of appointment numbered Z / pL have been requirements of the Federal Aviation Regulations. 1 J I ) Therefore r-- .Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 7- -7 . e/ JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277806

• . • EFTA00277807

AfIC•91,15. • 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, Helicopter, 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 STR. 1 - 14 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 iNIS?E_CION 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 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 with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered 0‹. ("<' have been requirements of the Federal Aviation Regulations. I ) Therefore 71 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) ,,, JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277808

..9 • S • • EFTA00277809

Af:IC,.91. ILO 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. 1476-005 (. REV. IR 7-22-97 REPORT NO. 1476-005 c- . 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 DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSpECTION 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 Regulations, examined in accordance with established I ) Therefore El by direction of the Administrator and in accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data these data with conditions and limitations of appointment numbered Z 0.., have been requirements of the Federal Aviation Regulations. ji-i6Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES orm (11-70 PERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277810

i, • • EFTA00277811

iL 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. 1476-006 `--- REV. IR 7-22-97 REPORT NO. 1476-006 (V 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 IN R P F CT 1 0 N 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 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 with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered a/ oe have been requirements of the Federal Aviation Regulations. I Therefore 171 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 7— e JIM MARTIN SW-916 STRUCTURES • _ FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277812

r • • • EFTA00277813

fiRC>97' 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 LIST 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 G 'OC) \ s ‘ s, PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific 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 Administrator and In accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered ,24" pZ of have been requirements of the Federal Aviation Regulations. I 04 Therefore SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 57 ,.,,,, JIM MARTIN SW-916 STRUCTURES • FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277814

• • • • EFTA00277815

RAC, crl, ILL . 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 LIST 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 JA/Ch L--,(Th ,_, .... PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific 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 Administrator and In accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered oe 1/ oc- have been requirements of the Federal Aviation Regulations. I (ye) Therefore i- 1 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277816

• 0. • EFTA00277817

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. 727 - 100 TYPE (Au-plane. Radro. Ilelicopier. etc.) Airplane NAME OF APPLICANT Associated Air Center LIST OF DATA IDENTIFICATION TITLE Drawing No. Autopilot Interface Unit Modification W/D. END Note: (1) The above data is approved for the electrical/ electronic and avionics design aspects only. 97 - 2211 - 210  Rev -- Date: 7/28/97 PURPOSE OF DATA To Support Major Alteration on S/N 20115 Only. APPLICABLE REQUIREMENTS (fist 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 X X have been authority vested by direction of the administrator and in accordance with of the Federal Aviation Regulations, data listed above and on attached examined in accordance with established procedures and found to comply Regulations. Recommend approval of these data Approve these data conditions and limitations sheets numbered with applicable requirements of the Federal Aviation I (326) Therefore x SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) SW - 880 Systems & Equipment // John W. Goswick V orm - EFTA00277818

a • . •• • • EFTA00277819

7-23-27 3:12 PM ;SUPER 27 PROGRAM 5125912232;# 2/ 5 U.B. DEPARTMENT OF TRANGPORTATION FEDERAL AVIATION ADMINISTRATION I STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE July 23, 1997 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) . Airplane NAME OF APPLICANT Rohr, Inc. LIST OF DATA a------ IDENTIFICATION TITLg • Rohr Inc., ERDS C0825 Revision A dated July 23, 1997 • Engineering Repair Data sheet INSPEU k • _.. PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. _____ APPLICABLE REQUIREMENTS (List SpecOo Sections) (1)(3) FAR 25.301 (2)(3) FAR 25.605 (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 the Federal Aviation Regulations, examined In accordance Regulations. of the Administrator and in accordance with conditions and limitations of aata listed above and on attached sheets numbered with established procedures and found to comply with applicable of these data requirements of the Federal Aviation I (We) Therefore Recommend approval Approve these data 8iGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVES DESIGNATION NUMSER(S) CLASSIFICATION(S) (1) Jeffrey D. Shutrump e -, NM-2731 Structures ,. . v• (2) Tony Bradlaugh-Dredge •-•-‘. NM-738 Powerplant (3) Michael August ".Z -t. NM-2182 Special Administrative _ . --- FAA Form 81104 (11-70) SU RSEDES PREVIOUS EDITION (Computer Generated by Rohr, Inc.) EFTA00277820

• pep 40 EFTA00277821

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD PiRWORTHINESS CERTIFICATE • I NATIONALITY AND REGISTRATION MARKS N5OOLS 2 MANUFACTURER AND MODEL [ 3 AIRCRAFT SERIAL NUMBER BOEING 727-31 20115 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and ceatties that. as of the date of issuance. the aircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to rp,set the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention oh International Civil Aviation. except as noted herein Exceptions 4 CATEGORY TRANSPORT NONE 6 TEAMS AND CONDITIONS Unless sooner surrendered, suspended, revoked. or a termination date is otherwise established by the Administrator, this airworthiness certificate is effective as long as the maintenance. preventative maintenance, and alterations are performed in accordance with Parts 21.43. and 91 of the Federal Aviation Regulations. as appropriate, and the aircr t is registered in the United States 4111. DATE OF ISSUANCE Replacement) 07-23-90 FAA REPRESENTATIVE LEE H. Till DESIGNATION NUMBER GLO7 Any alteration, reproduction, or misuse of this certificate m. a by e froI exceeding S WO, or impnsonrnent not exceeding3 years. or both. THIS CERTIFICATE MUST BE DISPL THE AIRCRAFT IN ACCORDA CE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) GPO 892-804 EFTA00277822

1 5 ... r a e• .fr 4 ili EFTA00277823

. O - • - MAJOR REPAIR AND ALTERATION . Form Approved OMB No. 2120-0020 For FAA Use Only US Dew titija ca-ortp«vmAl - (Airframe, Powerplant, Propeller, or Appliance) ' Federal Ar iaflon Office dentification -- -P i --7Z--40 ) I u RUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model- 727 —100RE Serial No. 20115 Nationality and Registration Mark N500LS - 2. Owner Name (As shown on registration certificate) NORTHWEST DELAWARE CORPORATION Address (As shown on registration certificate) ggYIA4,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 POEFIPLANT PROPELLER 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 IA301541619 Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of Ihe ,. -,Eede rMigion Regulations and that the information furnished herein is true and correct to thei,,beq.of my-knowledge. 1 '•; !.;e: :I .... i„ .3"L Date ii . March 11, 1998 , Signature ' ze-r 1 divi a • Richard K Cady II 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item wa inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is - t APPROVED O JE' TED FAA Fit. Standards Inspector Manufacturer X Inspection Authorization • her (Specify) FAA Designee Repair Station Person Approved by Transport Cana orthiness Group , Date of Approval or Rejection Certificate or Designation No. Si natur of thorized I yid:al • March LI , 1998 IA2185934 . - ,x-e T .W. RITCHIE FAA Form 337 riz-aa) EFTA00277824

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 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.) REMOVED THE FOLLOWING EQUIPTMENT; 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 STO9364sc. FAA APPROVED FLIGHT MANUAL SUPPLEMENT, DATED OCTOBER 27, 1997 IS REQUIRED AND INSTALLED ON THIS AIRCRAFT. WEIGHT & BALANCE NEGLIBLE. COPY OF STC ST09364SC AND MASTER DRAWING LIST ATTACHED. CONTINUED MAINTENANCE PRACTICES INCLUDED IN THIS PACKAGE. END El Additional Sheets Are Attached *U.S.GPO:1991-0-568-012140035 EFTA00277825

THE LIMITED UR0859 RECEIVED U.S /Department of Transportation Federal Aviation Administration ti . ... MAJOR (Airframe, REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Apprptypdo OMB p( c 1,01d2-0192196 Irina For FAA Use Only CiffirAPPOALLAS SW05 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil : penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 1958). ..-.,. _ - 1. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality N500LS and Registration Mark 2. Owner Name (As shown on registration certificate) Northwest Delaware Corp Address 1105 Wilmington, (As shown N. on registration Market DE St 19899 certificate) 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME — --- — ----- — ------- -------------(As described in item 1 above)------------ POWERPLANT PRATT & WHITNEY Turbo Fan Engine JT8D-7B P654373 X PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic Greenwich Air Services - Texas, LP Foreign Certificated Mechanic RAI R445K .. 9311 Reeves Street X Certificated Repair Station Powerplant Class 3 Dallas, Texas 75235 Manufacturer Accessory Class 1,2 and 3 D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date /0 r 3 O --n Sign e f Authorized Individual , 7. Approval r Return To Service Pursuant to the authority given persons specified bel w, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is _ X APPROVED [1 REJECTED BY FAA Flt. Standards inspector Manufacturer Inspection Authorization Other (specify) • FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group In ividual Date of Approval or Rejection / or O - 9 4 Certificate or Designation No. Signa f Authorized _3 RAI R445K f-AA Form 337 (12.88) EFTA00277826

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.) Engine S/N P654373 was removed due to "SERVICE BULLETIN COMPLIANCE." • Engine was disasembled, 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 ASB 6228. Continue timed combustion chambers. Complied with P&W Alert S/B 5729R2 and AD 87-14-01 R1; 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 S/B 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 JTSD 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 fl ADDITIONAL SHEETS ARE ATTACHED FAA AC 72-4906 EFTA00277827

0 . MAJOR REPAIR AND ALTERATION uSDeporrpent atralwavarxxl (Airframe, Powerplant, Propeller, or Appliance) Filderolita*Mms Aderinharoftn Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification a_FSDO-09 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model B727-31 Serial No. 20115 Nationality and Registration Mark N500LS • 2. Owner Name (As shown 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. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME ......................".......; (As described in Item 1 above) ...............~............~........" X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. ST Mobile Aerospace Engineering, Inc. 2100 9th. Street, Brookley Complex Mobile, AL 36615 U.S. Certificated Mechanic MZAR013L Limited Airframe Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the 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 e.r....---- • 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 NI APPROVED D REJECTED FAA Flt. Standards Inspector Manufacturer inspection Authorization Other (Specify) BY 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 (12.88) EFTA00277828

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration rAust 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 Winglet Modification in Accordance with Valsan Master Drawing List #VA000007, Rev uN" dated 17 April 1995. STC SA5938NM. Aircraft Inboard and Outboard Aft Flaps and Ailerons rigged to endure functionality and conformity. Aircraft weighed after modification. Weight and balance data provided to customer. Aircraft total time = 31,197 hours. Total cycles = 21,345. END K Additional Sheets Are Attached *U.S.GPO:1990-0-588-012/40004 EFTA00277829

FAA AIRCRAFT REGISTRY CAMERA N0. 3 DATE: die/ fr Se— •••• ••••-2. ; • 9.: of y; E «. •1 :4 : • :: . ;I: • f: : . : P • • I •14fiS • ••: m.44. • ;• 4.4. .4 • •4444.4•444 • 0 MAJOR REPAIR AND ALTERATION • uSOtowirrwre or laracianomn (Airframe; Powerplant, Propeller, or Appliance) I said asionse ' isaverawiesies •• . Fc.rm Approved • OMB No. 2120-0020 For FAA Use Only i t5IdenNication 0 _„ 6- 7 revision thereof) for instructions a civil penalty not to exceed 51,000 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 03 Appendix B. and AC43.9-1 (or subsequent and disposition of this form. This report is required by law (49 U.S.C:1421). Failure to report can result in for each such violation (Section 901 Federal Aviation Act of 1958); 1. Aircraft Make • aiE7N6- Model 7.Z7 - - /,‘Z) Serial No. ' c; o d C . • , .. . Nationality and Registr,ation Mark N5 -6,04.5 , a. Owner Name (As shown on iegistratiqn certificate) /vagazder. 44D/4/6 Oieft-P. .. . . Address (.4s shown on registration certificate) te)..an-k -7435 . V/(14),(16few ..7)e: /912)5 3. For FAA Use Only :. • r . • .• . .. _ .• ...::.1 - •&i • ‘ V. '',\ S ce • c • .--7/.:45:: I. %J.: ... ._ , , . , .. . ., • .• ••• • • • 4. Unit Identification _ . 5. 'Type Unit ... • .. . ' ', ••'', Model • - ' /•• . Serial No. -• Repair Alteration AIRFRAME (As : . described in Item 1 above) -.. • _ , POWERPLANT r. . . , • - .-......., . • • '-: . PROPELLER ._ .. . . - ' - • \'. .\• •• -/I:'+IV '..".-'• 'i• • • 1 .•. . - - - APPLIANCE Type e 24-s untgar .' PA) Zia/6 00 - 90c l (.1,OD. 6-) ; 97405'-e°3 e i i > l< Manulpoturer _ b. 6714/ra, 6. 'Conformity Statement A. Agency's Name and Address . B. Kind of A enc • C. Certificate No. --rief Ziliire3 ..tvc_ y3e2 mt. -fink Coi_i,f6tri osielt.o 5132. pi' - , U.S Certificated Mechanic , • 1 -04...))e S-93tZ . Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the un i(s) identified in item 4 above and described on the reverse or attachments'hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my kno - - . --- Date . 7/i/9 41 - S natur of orized Indivi - Pu Administrator BY • ••• 7. Approval for Return \o Sonic* suant to the authority given persons specified below• the Loch identifieo'in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is APPROVED O REJECTED FAA Ft,. Standards Inspector •N . Manufacturer Inspection Authorization (Specify/ . ' .. • FAA Designee Repair Station Person pprov by Transport Cana Airwo hives recap Date of Approval or Rejection /9/9 (1/ Certilicate or Designation No. --.1.14-a ,acci-w Sig lure of uth zed t Individulther . , FAA Fors 337 Ia.'s) • • • 4 : 4. 1 • eft ri if . • • • 4 .1, •i• •.‘ :••• •4 .1 • , • . onor a,. so iwarr•Iina.se,,,,,,iggilia airman Ofifigam • ffs il t ' 4 16* t • • ••• • S. . • . : . • . ' • i : • • N • • t . i. f. 4. ;rt. • • •• • ail2Si • • EFTA00277830

• I J.4.10. i'••:.! . x•,•nk;ilh 1G hill?' c ' Oint,n;T: • "Yanlei, ;;• ;01.•• • f-mt...o'R • "''• CV C. CA NC., rc...1‘J • • • -• now r- j 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. . t Description of Work Accomplished (If more space is required, attach additiOnal sheets. Identify with aircraft nationality and registration mark and date work completed.) .I••• /: .......i • . ... ••. • • •...• of. .!•1 • . . I I ' . • •• -e. • i • neile ... aPee,47›,e-z• To 4 -71v Vo66o/0.-' 4964 . (fien).- a.) "By • ,xletreAcrearver , Nits/ere-a_ ..sla 41°660/6 - 34 i ertir&041-67) npic.c#&,_ 4(4.49-7eme,A./ ..cs 2),Exa-ivr. AI > 9st -o/-041 4.-.. :...._. ,.Sy nrit /6Z-I 3(60 oPetkriernhild/ 04?"-e-20 eloo.Zo/D adNeo. TevZ .?4,-75,> c-1- 41 sie • 4),/, c hi- Vi Er • AV 4-eargrAig ,ec-ve6-.• idg rE73/ 2,4-.4) • ..?,00-6.edsoht , air ,491.4P 90-a -oV Afro. 39 -- 878Lr .. got -6,za- 23(?)..,-erbe -7116- Aril &Al AZ • v3771 V,Lti - e c.c% • 74)40ee,oi_der-77A.?6-. a- am/ of s stn. AD. 4;;,/ riierwr /111-Ahnot -Warsqc re" 477-Xedieb riehtf- lerre;-,c krfirlerc-zdue,. <ale Affigenak_ Av MeroAr oc --- , .. ......; L• . __J .:. , -:... :. • .: • -. 'i . . .. - I. b14•• .lain til'ArtemoD :t - "‘ . ... • - . ee•Yd.rd: bi 4 • 831•1, • • --.. . r .." • •— -••• • -•• • , • • . " • - • • . ' • el r Itei P.,:i .-; :fle ;".::: ; 410 to•lovin erlInlibm1I14: 4i.4150r. -•••.,..:.1..! •- 4:1•..! 4 ki 14e.itil.:;L: td.(E).1i.loeti.tol Sbs In (*ifZ.1'31 GIO‘tine• itbiitt ro.t,iF. , • :. nc,14:71 iC-;:i. Mit :KM brilt 4....41-.. 461:4;•.r.:11•' ,IlbivA ;it i•,•;•, : it 1.I.;.;-•Ilo a')'iL'•13.11•17in.4telsiitiro!,•• -pt;1 milt b'...nnelysi...i.aepi store r• $ r ; g.,.. • • , ' . • . i .: &'.... :/ it \b '1 t 0 JZ6d.erif ci! Jr.:alio.; t)4::. ,:... d zi nir.brv.' 1 • • - • • ............... • ..%•• . ...... m• ••••••• d.;,.•• '''' ' : '"•••• • J., • ..m.....m. •••• A.. I:Mi. . • . ••• • =4 .. . . . • ... I i'a iV i tit il 46 ‘`: i i c ' ; . P. 4t 1-g ?tc l‘ i) ; 14.: ; 7. i • I . k • . . . • • . • . • • ' " raiviDE2O.T.ot; i.: ' • *:•••! 4, . • • • • • c.r!S vc! tiC•dittiz 1(1,1r.ittittrii ,i:tirill Loitz;ttitril otiw 1%. ratili rii !...:•Iiiii,; ,i., Si: : t i. 1.'.. .... ‘.••1:.ki.t.soli:•••.)cli e:norisr;, • .)*'1,:! vinc...0.;44P., Urn Vi. I714;,::‘• "•;..• i i.,:tt Ii0;10:1041,:t,.;11::- nc•it,.:-.6•A ;•7•.p.i..i.:k.",t•IA.10 mlitt!imiltsn. ' v . •.. I) rti3lan t.1 • (tvtior,:t...:-..,•'? ,. . - r . . . . - . ._ ...... (X‘V.11::.1?. iVil:51 • . . . . • I. . ;;.... tt 1: : : !. i < 71'.: L.... 5. t t; i :•:• -• . : , itglli!:10".:, ..1,0a • : 2.*'.11•‘triate-107 •434,,,i1.1.rAZI . 1 . • . • l'• • . : i'diti:dir.47 yd b loi.;';i lc:521.)g! • :- - - • • ' .. • . fIC;Irlc. lif191............ . i...:-. ..‘Octize!..• A Al • • • — . Mdiehriv3r4in lowilm is.e4.9.•,.. , ..._.... • ...•+...•.••••..... • ea .. aft ••••••••••••. .• ••••.••••=••••••••••1 •••••••••dmmini• •••.... ir••••• •••••• •••11,•••••••,.. ••• : , ••••••••7 .7 ...... ' , • • itii iivitini bt..1=0,4 lo 0,Lpap.. eta 1 . - t incl.,01D, . ritri)34,40,y., •:....,vzi.V, ... • • . i , A i i • • .. .., .1.., • , -, t. , • . i• . ..0.,110,. 7., ,r1.:Et...? " • \-,-: -O kddillo I ShilailicA6 Atiecheid .0';•Cr-')Ot • cL,:..477;:. • • :, :. • s,-;,.:..•. .:, . • ... "I: jti fat, • • 'a' •• • • • • I a' • EFTA00277831

FAA AIRCRAFT REGISTRY CAMERA NO. ,3 DATE: -41e/Ife/fY %."7.-:• 4- USDemamment ottranSpa-tationi Federal Aviation AdotinistratiaA • TRANSPORT AIRPLANE DIRECTORATE AIRCRAFT CERTIFICATION SERVICE LOSJANGELES AIRCRAFT CERTIFICATION OFFIC ; (,. (3229 EAST SPRING STREET / LONG BEACH, CALIFORNIA 90806-242S VAR CI 144 Honeywell inc. Air Transport Systems Division ATTN: Mr. F. W. (Bill) Lynch 21111 North 19th Avenue Phoenix, Arizona 85027 References: a) Honeywell letter, dated Feruary 17, 1994 b) Honeywell letter, dated March 1, 1994 Dear Mr. Lynch: ' Approval of an Alternate Means of Compliance " fp response to your letter of March 1, 1994, our review of the data submitted fivsupport 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, -90R and -903 (Any Mod) to part No. 4066010-904 (Mos G), has been completed. We concur that method and procedures outlined in your revised Service Sullitin 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- NM-68-AD; Amendment 39-8786. If there are any further question, please contact Mr. Abby Malmir at (310) 988-5351. Sincerely, ,‘ 7-/f r"—w.-c, - • Alan T. Shinseki Manager, Systems and Equipment Branch Lt.?: • , . • 4. .4, a_ • o • 7, • • F.-; 1 tt • _s=2 --tze;&,,,„6.smru.lua • ‘.. EFTA00277832

T. •MAKT:2131115; ;;„.(4(.1114 110124AST 33114W. TIARanZA,. "i'40 PPIT ;:•INI.751"A • .2.:1317T4A. • 1'.47Utr; °Muni! tatt • 4.1 , . . . Aflinirrlie3-:4(jkls ?./.1 ria3Dre)Ctritni moitctiyA -•• tr;nriTtz:nia.;:.71.. •• ¢. :iii. I f r. •C tr-H IQ ( iS) .1. . •7;4 ;1.110;4 111.1f: •t.Stfija.r.nosNA :; '-;Co'3110;:i• f ••••vivetno!f ;I • •.• r ±rib tioa t r•I ; V:• • •j:• ;. 0 i2 •• C• ••'• -ray • 0`;) s..1100::f. • • t • • TV.4q AO gr 5:00a tau? -Of0600:2W4 11::4N.3ro10 6 :golzssiVriorpiiii)21-415.1 ry thri/cOla0M/Vie-.0103Y214;;69-,,V7Ap cOM. • • . - 3f.lsifun -iec . v !mg Fiu6. ztriu.i.tboini•Ina. Itorifee,pr ;$35:30v.../31-; M0rfIce.):::)c, aiNz-fsc-oluaboA, ;10tio(J.j10--!.4.7-411i) Olt, 1.15 ,‘.1 •dirriEti-NrAz 'i.:}•zi's.;v1 71' • f. • • .. ft Ottieit* •'i$ 4-8a4;;;: ti •••••1'" • • zfff.:15.2.v.2 *i.ert,;%tr,;. EFTA00277833

I FAA AIRCRAFT REGISTRY CAMERA NO. 3 DATE: y1/4y/f5— • ;: 4 • . .4/ ?•:' , . . C • „ ra ' grakehigko& ..1 . • • t ' :••••••• 1.1... • '-'•• • • • • . • • • • eN1 I It/ •/. • . • ,• . AIRWORTHINESS DIRECTiVE FUGHT STANDARDS SERVICE REGULATORY SUPPORT OMSION P.O. BOX 26460 OICLAHOMA a-ne, OKLAHOMA 73125-0460 ; " ' ' • .• . • 't • • • - . • . • . • ' • , • . • • U.S. Depastrberd of Transpottation •, Federal Aviation Administration Th• Icameno te....,en••• Cara Sued by ea Fa A.td.r asatinieteent Si esimmes eel the eieplise• et reimnd flecsiodoaa east a *Plan a skint "sal d ..'" as " air ". ioulloos you Nonni' •441•Ianal Asinswrearts Pao a _it. sCs sod SO Picamlbale gnat fora losallcOm areka Yom •••• •••••caml RS re p.•. , wary tarn Si sistrellIntioli M Alrailla Oat* sp apasame Ilinseraren 01realre ••••••••S •...bomet 3•1.4. 04-01-04 HONEYWELL: Amendment 39-87843. Docket 93-NM-68-AD. Applicability: Traffic Alert and Collision Avoidance System (TCAS) II computer units; part numbers 4066010-901, -902. and -903; as installed on. but not hatted to, the following almlancs. certificated in any category: Airbus Industrie Model A300-4300. A310-200. A310-300. A320-200. and A340 'scales airplanes: Boeing Model .727-100 and -200: 737-100. -200. -300. -400. and -500: 747-100. -200. -300. -400 and 747SP; 757-200; and 767-200 and -300 series airplanes: Cessna Citation Model C550 and C560 series airplanes. and Cessna Citation III and. VII 1 • series airplanes: Canadair Challenger Model CL-600-2B16 and -2Al2 series airplanes: iJ I British Aerospace Model 125-800A: Gulf:stream Model Gil, GLIB. GIII. and GIV series airplanes- Lockheed Model L-1011 series airplanes; McDonnell Douglas Model DC-9-10, -20, -30-, -40, and -50; DC-10-10, -15..30. and -444 ;It s MD-11: and DC-9-80 series alrplazics; and Model MD-88 airplanes: . Dassault AV/S.111On Model Mystcre-Falcon 50 and 900 series airplanes; • Short Brothers Model 503-60 series airplanes; de Havilland Model DHC-8-100 and DHC-7 series airplanes: ' •Ri • '-; I .011 • Fokker Model F27 series airplanes; and Corporate Jets limited Model BAe 125-800A and EiAc 125-1000A series airplanes. A • s' • -1 2.0"4, Compliance: Required as indicated, unless accomplished previously. To prevent collisions or near misses caused by incompatibility between the TCAS II processors and the current air traffic control system. accomplish the {allowing: (a) Before December 31. 1994, accomplLsh the requirements of paragraphs • (aiel ) +and (aX2) of this AD in acconiance with Honctywell Service Bulletin 4066010-34-S*16. -dated December 20, 1993. • ' (1$ Remove existing Honeywell TCAS U computer units, part numbers 4066010-901, -902, and -903, and replace those units with new units that incorporate updated collision avoidance system (CAS) logic, identified as Version 6.04A in Mitre letter F046-L-0069.i, 1 dated September 21, 1993. (2) Modify the computer surveillance logic on Honeywell TCAS U computer united r.t. part numbers 4068010-901, -902, and -903, to ensure that these units accommodate Mode C altitude input of 100-foot Increments and that the system will be tracked and coordinated by Intruding aircraft when the Mode S transponder CA field Ls set at CA.7. • • (b) WPrior. to further -after accomplishing the requirements- of paragrapir (al- of tidal? AD.—revise the Airplane-. Flight Mniiunl (AIM) :AFM- SupiiIement by • either .+ paragraph (bXI) or (bX2) of this AD; (1) Revise the Normal Procedures Section of the AFM to include the aP13ropriate TCAS operating characteristic relative to the modifications required by paragraph (a) of this AD, in accordance with a method approved by the Manager. Los Angeles Aircraft Certification Office (ACO). FAA. Transport Airplane Directorate. Or (2) - Revise the Normal Procedures Section of the AIM. to Include the following! TCAS operating characteristic relative to the modification required by paragraph (a) of this AD. This may be accomplished by Inserting a-copy of this AD in the AFM or AFM Supplement::7 I! ' • • •• • •!• • et: ,. ere_ 4,4, fr • • ,': a,. 4 -• • 41 • • . 1.e :4i .• ' • • • • • • • • -••! ! - . • • • 0' , • , . • .• • . .• •• • 3 • T. . . . 'Ijk• 4.-0: 41'•;•-• • jsr, k.••;.Att4 7‘.• • EFTA00277834

FAA AIRCRAFT REGISTRY CAMERA NO. 3 - DATE: -y/r/i 2 94:0144 'All Resolution Advisory (RA) and Traffic Advisory CM) aural messages am ' • inhibited at a radio altitude of less than 1.100 feet above ground level (AGL) climbing. and less than 900 fed AGL descending t of the corap .' (c) An alterrtattve method of compliance or adjustmen liance time that provides an acceptable level of safety may be used if approved by the Nianager. Los Angeles Aircraft Certification Office (AC01. FAA. Transport Airplane Directorate. Operators shall submit their • requests through an appropriate FAA Principal Avionics. Inspector. who may add comments and then send it to the Maruager. Los Angeles ACO. • . NOTE: Information txtncerning the existence of approved alternative methods of compliance with this AD. if any. may be obtained from the Los Angeles ACO. (d) Special flight permits may be issued In accordance with FAR 21.197 and 21.199 to operate the airplane to a location whore the requirements of this AD can be a.coomplistux:L (e) The replacement and modification shall be done in accordance with Honeywell Service Bulletin 4066010-34-SW16, dated December 20. 1993. This incorporation by reference was approved by the Director of eel Federal Register in accordance with 5 U.S.C. 5.52(a) and 1 CFR Part 51. Copies may be obtained from Honeywell Inc-. Commercial 14-light Systems Group, Ar . Transport Systems Division. P.O. Box 21111. Phoenix. Arizona asoss. Copies may be inspected the FAA. Traiasport Airplane Directorate. 1601 [led Avenue, SW., Renton. Washington: at the FAA. Transport Airplane Directorate. Los Angeles Aircraft Certification Office_ 3229 ,East Spring Street. • Long Beach. California; or at the Office of the Federal Registers 800 North Capitol Street NW.. suite 700. Washington. DC. (f) This amendment becomes effective on February 4. W94. FOR FURTHER INFORMATION CONTACT: ' . .. Abby Nialn Aerospace ErIginCer. Systems and Equipment Branch. AMA-13216. FAA. Transport Airplane Directorate, Los Angeles Aircraft Certification Office, 3229 East Spring Street. Long Beach. California 90806-2425; telephone (310) 988-5-%51; fax (310) 988-5210. Aircraft Flights Date ode No. Aircraft/APU Hours GI GII Gilt GIV NOT APPLICABLE COMPLIED WITH • -• - DEFERRED UNTIL,. - E ABOVE ITEM IS DUE ON LEASE COMPLETE THIS FORM AND SEND IT IN WHEN THE ITEM IS COMPLIED WITHH. . 5 t..it 1 _ :t ; ::::::15.:ir.ii t'.' I.'111.1: L:,l, .“.• v u: .ti—', 1..1:;.! sc. ',.t.:: :1-.;z:-...'„•7, .i:.ti t:.r: 1.1:e'iilii:t2,'.;. Z:5 4.2,,t z .. tr:/5?:.) a JSOlil.Diltritt:1 J)trird f"!. :1••7••11,. ii:).3 . , . t;?7)v; U•1 Vi T.: '..1 -... i>ttioft I. •.); • , ,_Ali f" r. tit 1, cp :341:le 01 troll. :1;g-iFl. Itro .Jr. : 1 silt t• ....Lc.), : • • t •., . , •.- • . : rnr.. . • liwez • tti : ••-oh• +34K Mr?. (*--.11,11 ae: _101.?1:.0:11X.11.9 I CA ,;1117):"1 r.Pikr.t.:1"1::!t-strb r • • f. •t: Cr. 'grit 'to vr it .; ;,• matht• tztt 13•;71-.:tqrtr., •. tv: C:Uq• , a -an Onftilwls EFTA00277835

-FAA AIRCRAFT REGISTRY CAMERA NO. i it/ DATE: /0 -1R-94 • ( •••••• ••••• •1 it .7! 1 r a MAJOR REPAIR AND ALTERATION • Form Approved OMB No. 2120-0020 For FAA Use Only us Department nr frolsooncmcn . (Airframe, Powerplant, Propeller, or Appliance) riderdAriation , - AdrintenstIon (1)ffiC.Alrang.0-15 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (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 BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark NSOOLS 2. Owner Name (As shown on registration certificate) NORTHWEST HOLDING CORP. Address (As shown on registration certificate) 1105 N. MARKET STREET WILMINGTON, DE 19899 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 POWERPLANT • N PROPELLER . I. APPLANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. PAGE AVJET CORPORATION 9809 TRADEPORT DRIVE ORLANDO, FLORIDA 32827 U.S. Certificated Mechanic 0S4R425M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the un't(s) identified in item 4 above and described_on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S Federal Avia egulati and t information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Indi dual t2. 056-4-17 /996/- • 7. Approval for Return To Service Pt. suer: to the authority given persons specified below, the unit identified in item 4 was' inspected in the manner prescribed by the F...rnrhistrator of the Federal Aviation Administration and is at APPROVED O REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Ai rthiness Group Date of Ap royal o Refection Certificate or . Signatur Aril Authorized ivid 9 Ii-r/ CO g 2 -4 Designatior• No. 0S4R425M Affte/ 709,1) / Ati ti . ...t-C4-7.---7.-. FAA 'Form 3 1t2.88) A • • No ......Viecte •PC e l :ki t 14;: a aA11 1 ttii4Ty "rot. Aff:1,,a frft tP , - Ina Or ;et. •. , • EFTA00277836

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 requitements. • 8. Description of Work Accomplished . (If more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed:) . . . 1. INSTALLED A DORNE & MARGOLIN EMERGENCY LOCATION TRANSMITTER (ELT) SYSTEM IN ACCORDANCE WITH PAGE AVJET REPORT PR -91-22 REV. A, DATED 8/15/94 AND MDL- 91-02 REV. B, DATED 8/10/94 AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339, DATED AUGUST 16, 1994.. PROVIDED WEIGHT & BALANCE UPDATE. EQUIPMENT LIST UPDATED ACCORDINGLY. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. ALL PERTINET DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION 0S4R425M UNDER WORK ORDER 60298, DATED SEPTEMBER 2, 1994. . . . . . . . . . ••• ;:ot ; •• .1 :1; . • • EFTA00277837

e -FAA AIRCRAFT REGISTRY CAMERA N0.3k DATE: /0-/a- *L____ 4".• MAJOR REPAIR AND ALTERATION wspepartnem . of Tronspc- - or . (Airframe, Powerptant, Propeller, or Appliance) fekleterof A;dorkan Adnitrekstration Form Approved OMB No. 2120-0020 For FAA Use Only ittro_ 15 OfficeAtyf INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAB 43 Appendix B, and AC43.9-1 (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 Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N500LS Z. Owner Name (As shown on registration certificate) NORTHWEST HOLDING CORP. Address (As shown on registration certificate) . 1105 N. Market Street Wilmington, DE 19899 3. For FAA Use Ority 4. Unit Identification .5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME • .....~..................~..ww.... (As described in Item 1 above) X POWERPLANT PROPELLER ' APPLIANCE Type Manufacturer 6. Conformity Statement C. A. Agency's Name and Address B. Kind of Agency Certificate No. Page Avjet Corporation 9809 Tradeport Drive Orlando, Florida 32827 U.S. Certificated Mechanic OS4R425M Fore.gn Certificated Mechanic Cer,iticaled Repair Station Manufacturer D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above have been made in accordance with the requirements of Part 43 of the U.S. Federa furnished herein is true and correct to the best of my knciwiedge. er everse or attachments hereto d that the i ation and descri on t Aviatio egulations Date £ SEPT-6496E-2:- 1993/4 7. Approval Signature of Authorized Individ I 06g/ere-L-4 - for Return To Service -3491(C) - by the Pu Administrator BY suant to the authority of the Federal given Aviation X persons specified below, the unit identified in item 4 was inspect in the manner prescribed Administration and is IX APPROVED O REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Person Canada Other (Specify) Authorization Fl" FAA Designee Repair Station Approved by Transport orthiness Group Date of Approval or Rejection 2 SEPT: 9 1/ Certificate or Designation No. OS4R425M Signet of Author d Ind ual al -4y .,Sgy te.___CgotoPtiztrA,1 ) ere—ter:7r EFTA00277838

-FAA AIRCRAFT REGISTRY CAMERA N0.3,V DATE: joria rJyC - NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An altelation must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • . • . 8.- Inscription of Work Accomplished . (If more space is required,,attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) .- • . 727-31 S/N 20115 N500LS 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 8/11/94 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 DFR MARION SHIN, SO-339 DATED AUGUST 22, • 1994. SUMMARY: 1. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION OS4R425M TINDER WORK ORDER 60298, DATED • • • • g • • • .• END .. • . • E. - • .t: :•• "P- • '•`- ;•• :de. • ! . r • . • . 1 0 .• I. 4O; • . . • . • k • • - •• • 1:‘'? D Additional Sheets AreAttniched • 4 • ,-•“Iffet•t. .U.S GP0:1991.0-S8&012140035 • EFTA00277839

i -FAA AIRCRAFT REGISTRY CAmFRA N.i. :A/ DATE: 1O-1a- *it fi • ., • z, MAJOR REPAIR AND ALTERATION lis Department cc tronsocconon (Airframe, Powerplant, Propeller, or Appliance) Fedora Aviation Admintoanion Form Approved OMB No. 2120-0020 For FAA Use OTh offiASIOrtESDO INSTRUCTIONS. Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC43.9-1 (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 Boeing Model 727-31 Serial No. 20115 Nationality and Reg .lion Mark 00LS 2. Owner Name (As shown on registration certificate) NORTHWEST HOLDING CORP. Address (t i so_ivn on registration certificate) 5 N. Market Street Wilmington, DE 19899 3. For FAA Use Only 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) ---- X POWERPLANT PROPELLER 1/4 APPLIANCE Type 4 Manufacturer . 6..Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Page Avjet Corporation 9809 Tradeport Drive Orlando, Florida 32827 U.S. Certificated Mechanic OS4R425M Fo-eign Certificated Mechanic • X Certilicated Repair Station Manulecturer D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviatio furnished herein is true and correct to the best of my knowledge. on the reverse or attachments and that the inf hereto . ation t gulatt Date (2, S EPrE/Y)8Et /99 SZ Signature of Authorized Inc:livid ,ial 744a 7. Approval for Return To Service Pu Administrator BY suant to the authority of the Federal given Aviation persons specified below, the unit identified in item 4 was inspected Administration and is ' . g1 APPROVED LI REJECTED in the manner prescribed by the ..._ FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada • • orthiness Group Date of Approval or Rejection W 9' Certificate or Designation No. OS4R425M Signal . of Authorize ndivid Ccht; ge-4/ itfin At) ,----> /Wirfi ../A—,---A--; FAA Form 337 it2.ettn • l• • • I -- • • EFTA00277840

- PAA Al.cICRAFT REGISTRY CAMERA ?il DATE; . 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 spaco is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 727-31 S/N 20115 N500LS 1. RELOCATED ACCESS PANEL FROM B.S. 1183 TO B.S. 1350 LH AND RH BETWEEN STRINGERS S4 TO 57 IN ORDER TO FACILITATE ACCESS FOR FREQUENT INSPECTION TO TERMINAL FITTING IN ACCORDANCE WITH PAGE AVJET E.O- NO. 53-30-02837 DATED 7t'28/94 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 2.8,EPT934 • --3-END K Additional Shoots Aro Attached • • • • • . ..... . • . — . . . • • - • • . . • • • • • • • • • * U.S.GPO:1 9 91-0-568-01 2/4003 5 EFTA00277841

FAA AIRCRAFT REGISTRY CAMERA NO, DATE: 0-1 93 - 0 MAJOR REPAIR AND ALTERATION Form Approved OMB No. 2120-9020 us Deporrmtt Appliance) For FAA Use Only erifonteconeon (Airframe, Powerplant, Propeller, or Feigned Aylation Administration Office Identification S0-FS00.15 INSTRUCTIONS: Print ortype all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disp osition 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 91 00O for each such violation (Section 901 Federal Aviation Act of 1958). Make Boeing Model 727-31 1.' Aircraft Serial No. 20115 Nationality and Registration Mark NSOOLS 2 Owner Name (As shown on registration certificate) .,. NORTHWEST HOLDING CORP. Address (As shown on registration certificate) 1105 N. Market Street Wilmington, DE 19899 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model Serial No. Repair Alteration AIRFRAME (At described in Item I above) X . POWERPLANT , PROPELLER APPLIANCE Type ' Manufacturer • 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Page Avjet Corporation U.S. Certificated Mechanic 9809 Tradeport Drive Foreign Certificated Mechanic 0S4R425M Orlando, FL 32827 Certificated Repair Station _X Manufacturer D. I certify that the repair and/or alteration made to the un t(s) identified in gem 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 tat the information furnished heroin is true and correct to the best of my knowledge. • Date Signature uth•rized Individual 4 ,, f7/45, -1/ V. 4:09.e.c..v/ • itict.5/1.5 e.7.4.e.u,. 7. A for Rota • Service Pu suant 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 R.) APPROVED O REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) - BY FAA Designee x Repair Station Person Approved by Transport Canada Ayryrorthiness Group Date of Approval or Rejection r c2S- ? 3 Certificate or Designation No. 0S411425M • SIgnatu e'of Authorized Individual 7 2/CAAin ‘f/ey / .1• go")/e,enwr EFTA00277842

PAA AIRCRAFT REGISTRY CAMERA NO. 1 DATE: //'/- 93 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatibli with all previous alterations to assure continued conformity with the applicable airworthiness requirements. ?f-PLIZI 8. Description of W rk Accomplished ; (If more space is required, attach additional sheets. Identity with aircraft nationality-and registration mark and date work completed.) • B727-31 -N5OOLS I. INSTALLED HONEYWELL TCA8i,II SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3094S0. SUMMARY: 1 AIRCRAFT WEIGHT AND BALANCE UPDATED ACCORDINGLY. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. ALL SYSTEMS INSTALLED OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. • 4. ALL ENGINEERING AND WORK ACCOMPLISHED AT PAGE AVJET C_ORPORATI.ON_ 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. . • • I:0: .".: • ; . . ; .• • , is tlr,ill Ic, : 1"i • •: • . . . • . .„ . i•;.••-gz.:,••••6 f• ..,:,-, • \ - ' • ‘‘ I • .i,:f l t .',!,, • \;:!".::.. ''‘‘. .. . ...ft..... .......:......,. ...!. ... ../...... ......! .: 30....:...a...... --.....-- ......-- .); nth:A I 1'. .. .• ::12.1::4 l'c . • . • :. '...:7 Pi l'n .:),Pil..n. .6 .v i :n • j 1.1 t."-I:el• •I ...•.1 •)r•si sz.:•:-..! ;,:l. • .1.: rn:;..t...; it-p.i.j •,:. '141.2....10./I 1 . 0 .r. Oil is.: 1!-I .t: P. -. ••• 0.!.. .. ..t.k;ft •-...::.,,,•.• ... nt,.41,9:.:t) • • . . !. i i ..: . 2.,,LA.••• ''.. .: '' ‘1% ; • rtNi,.:xlIzi.14,A rioibo.lardi I .. ...);,74 gg.i-• . . ... • I I I,. c.:;.;,.- i,' : d ' . •';'.".i.,.A rtoe'll..li .....k: , ......:.i„f.: ,i,...)...4•; • • ..1 •:. .t.,.:••••:; ct 1: .\ . ,ivt:./i •.: ...::::,,..e.A .. .,....„ ., • . k • M. .' . . • %. i . \ littif..'11:110 i. ..•-.;ri‘t .1 •;%•..•••.71r>.k., 4) ..'‘, l• .;, .. . \. ." . t:'• . . . . . `t . e• • • •‘‘' , `,. i ..... . ''.• . - O •Addllional.Sheiti Are Attiched ...,:2i:-.;..:c!.;.. ; . • . a" ..":•; l d • ' • . • .. • *U.S. GOVERNMENT PRINTING OFFICE: 1892-719-012/60157' EFTA00277843

V. FAA AIRCRAFT REGISTRY CAMERA NO. 5r4DATES P - 4 - 9a • e• - t • . 1 .• • •• • ". .. e•-t • • I r r• • d . • .. . '• • - • 1 • • . .MAJOR REPAIR ANDcr ALTERATION OS Depot imeni ,• ei bcnseorioi.on (Airframe, Powerplanl, Propeller, or Appliance) ' . . ....Aviation Administronon Form Approved OMB No. 2120-0020 For FAA Use Only Office Identilithoysli o is INSTRUCT IONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix Band AC 43.9-1 (or subsequent revision thereof) for instructions and disposition ol 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 Federel.Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-31 Serial No. , 20115 Nationality and Registration Mark N500LS 2. Owner • Name (As shown on registration certificate) - i= i Northwest Holding Corporation Address (As shown on registration certificate) . • P.O. Box 7138 Wilmington, DE 19803 3. For FAA Use Only ' . _ • • 4. Unit Identification 5. Type Unit Make Model Serial No. Repair • r Alteration • AIRFRAME (As described In Item I above) ' ' • X POWERPLANT PROPELLER . APPLIANCE - 1 ype .r., ‘ i - • - , • Maimlaciui ei 6. Conformity Statement A Agen!.....y's Name mid Address Avje't Couporalion Trade-TWA_ Florida h int ilicieravi .milk). hem, mom: rk it, „woo, rivrem is um: 4 L11.2 9_12_5.+ . B. Kind ol Agency --. C. Certi icate No. • Page 9809 Orlando. D I 'Aoki) !ed..; umrushed • I !hire 3- 1 . - I/ Wive i, arlij lac 32827 - - X U s Certificated Mechanic I . 0S4R425M Furin9it Certificated Mechanic Certificated Repair Station Meintilacturer .. oil...Limon made to the ini i(s) identified in item 4 above arid described on the reverse or attachments-hereto, e with the requiremoids of Part 43 ol the U S Federal Aviation Regulations and that the Information ‘Ollad W the best ol my knowledge. ' • 22 Signature (---- ol Auth i d Individual 4 AMC,4 : 447 .90 --- 7 Pursuant AdillitirSilaWl UY ..... — . to lily at/Viunty Ul the I tide' di ••• ". - I AA I. It Sidnjoids inspector FAA Desynee ii.er A.I.Illuil • • X 7. Aoki:oval for Return To Service tau auirs specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administration and is • El •APPROVED 0 REJECTED MoilltlidditilUI ' Inspection Authorization Other (Specify) • . ' , . _ itemui Station Pelson Approved by Transport Canada Airworthiness Group Date ul Ai provid or illittClivil 2) Luc ' 4( 5 t . OS) Gelilk:Me or Designation No. OS411425M Signature of Authorized Individual .. a_a i 4 dLictzlz - n - . - f s 4 vth g tstrima' "• I" • EFTA00277844

• • FAA AIRCRAFT REGISTRY . • CAMERA ND. 3 AiDATE. // 70 - 9a • • • . . .. • lir.. . • • ". : • • • 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 (he applicable airworthiness requirements. 8. peeccIplion of Accomplished 1 firmara japcali required. attach additional sheets. Identity with aircraft nationality and registration mark and dale work completed.) D727-31 5/N 20115 • N500LS 1. MODIFIED SECOND BATTERY SYSTEM PER PAGE .AVJET CORPORATION- STC SA3092SO, MASTER DRAWING LIST MDL-91-371 REV. A. 2. MODIFIED ED44-805 EFIS PER PAGE-AVJET CORPORATION STC SA3085SO, MASTER DRAWING LIST MDL-91-44, REV. A. 3. MODIFIED FMS-800 FLIGHT MANAGEMENT SYSTEM PER PAGE AVJET CORPORATION STC SA3089S0, MASTER DRAWING LIST MDL-91-43, REV. A (NZ-9112 SOFTWARE). SUMMARY: 1. PROVIDED WEIGHT AND BALANCE UPDATE. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. el 3. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. 4. ALL PERTINENT DETAILS,Or% WORK ACCOMPLISHED ARE ON FILE AT PAGE AVJET CORPORATION UNDER WORK ORDER 9286, DATED AUGUST 31, 1992. • END • 0 ••••••••• •• • i • . • • _ . • - - • . . • • - • - , • . ! ! . . : t. • • rt..; A II • • • • ••••• .• ••• • . . . • • I r • '• • • • • • K Additional SheetiAre Attached • • • 411Serirt- OrOnMalal • - • i EFTA00277845

FAA AIRCRAFT ' CAMERA NO. bi DATE: th _ Qom, • t. • . 0 • MAJOR REPAIR AND ALTERATION ' usorpcsimens cr Ircesoorvorm (Airframe, Powerplant, Propeller, or Appliance) redone Aviation ediminisfrotion Form Approved -6020 OMB No. 2120 For FAA Use Only Office IdentWcation 30-f300-15 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR.43 Apkndix B. and AC43.9-1 (or subsequent revision thereof) for instructions and dispoiition 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 1. Aircraft I Make Boeing Model 727-31 • Serial-No: Nationality and Registration Mark N500LS 1• 20115 2. Owner Name (As shown on registration certiiicafe). Northwest'Holding Corporation Address (As shown on registration certificate) P.O._ Box 7138 • •• . ' Wilmington, DE 19803'" . 3. For FAA Use Only . si. • . • , ..• , . . 4. Unit Identification 5. Type Unit Make ?. • " Model . * Serial No. Repair • Alteration AIRFRAME • • • ..--- - (As described in Item 1 above) ' X _ . • POWERPLANT • • . " PROPELLER , • - APPLIANCE Type • • , • Manufacturer . 8. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Page Av jet Corporation 9809 Tradeport Drive Orlando/ Florida 32827 U.S. Certilicaled Mechanic OS4R425M. - Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the un I(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S Federal Aviation Regulations and that the information - furnished herein is true and correct to the best of my knowledge. Date • 2 Signature • A izer :' idu J O i-f r ) It: 14 Lt, ire (\.) 4- !Return 7. 'Approv To Service Pursuer I to the authority given persons specIlled below. th nit identified in item 4 was inspected in the manner prescribed by the Administi ator of the Federal Aviation Administration and is KI APPROVED O REJECTED FAA Fli Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group . Date of Approval or Rejection Zs JAL) i 5 Certificate or Designation No. OS4B425N_ SI enure of Authorized Indi dual . alt() . .hil-U/1) H L-Fr1 nil tqa--- PAA'Form 317 II; net - ••• I EFTA00277846

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. & Description of Work Accomplished • Of more space Is required, attach additional sheets. Identify with aircraft nationality and registration mark end date work completed.) INSTALLED SUNDSTRAND MARK VII WINDSHEAR DETECTION/GROUND PROXIMITY WARNING SYSTEM (GPWS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3133SO. ALL WORK ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. 003.4122044. EFTA00277847

FAA AIRCRAFT REGISTRY CAMERA NO. IN DATE: — q 9v2 - 'tar ••• • • ere CO REPAIR AND ALTERATION ..• Form Approved OMB No. 2120-0020 MAJOR USE/ewer:erg For FAA Use Only okinfosnorym (Airframe, Powerplant, Propeller, or Appliance) Federal AvIcalcin Acentrkstratton Office Identification so--Fs110-15 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix El, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Boeing Model 727-31 1. Aircraft Serial No. 20115_ Nationality and Registration Mark • N500LS • 2. Owner Name (As shown on registration certificate) • Northwest Holding Corporation Address (As shown on registration certificate) • P.O. ! Box 7138—_!... .: Wilmington, DE 19803 3. For FAA Use Only . • C. , ... • . • . . 4. Unit Identification S. Type Unit Make • Model Serial No. Repair Alteration AIRFRAME ' - (As described in Item I above) .- . a X POWERPLANT PROPELLER . % APPLIANCE Type Manufacturer • • • 8. Conformity Statement A. Agency's Name and Audi ess B. Kind of Agency C. Certificate No. • • U S Cerlilicatee Mechanic Page Avjet Corporation Ft:feign Certificated Mechanic :1 ' 9809 Tradeport Drive X Ceitilicated Repair Station OS4R42514 OrlandoL_Florida 32827 Manulacluier D. I certily that the repair and/or alteration made to the un have been made in accordance with the requirements furnished herein is true and cot rect to the best orsity knowledge. t(s) identified in item 4 above and described on the reverse or attachments hereto of Part 43 of the U.S Federal Aviation Regulations and that the information Date • I ?9r? Signature of Authorized Individual i4Afral.5 r. Writ* Jr. 7. A r I for Return To Service Pu suat I to the authority given peMbna specified below, the unit identified in item 4 was inspected In the manner prescribed by the Administrator of the Fedora) Aviation Administration and is 09 APPROVED O REJECTED FAA Fit Standards Inspector Manufacturer Inspection Authorization Other (Specify) i BY FAA Designee X Repair Station . Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection a0D. 3,ti-r) fici a Certificate or Designation No. QS4R4a5EL Sigr lure of Authorized Individual • it er:.6.4 Ds v11) bi 2.417/472#2 inn rum, 337 I I,girt c- • • II • ir • EFTA00277848

FAA AIRCRAFT ' CAMERA NO. /A./ DATE: 6 ) _q_ • i 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. Desalpilcin-otWolfaccomplished (If more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) 0727 -31, $/N 20115 1: INSTALLED,EXECUTIVE'INTERIOR.IN.ACCORDANCE.WITH.PAGE AVJET CORPO RATION.STC.SA3137S0. 2. INSTALLED HONEYWELL EDZ-805 ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3085S0. 3. INSTALLED MODE "S" TRANSPONDER IN ACCORDANCE WITH PAGE AVJET CORPORATION' STC SA3095S0. 4. INSTALLED JAMCO SMOKE DETECTORS IN ACCORDANCE WITH PAGE-AVJET CORPORATION STC SA3132S0. 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. 7,. INSTALLED HONEYWELL FMZ-B00 FLIGHT MANAGEMENT SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3089S0. 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 WITH PAGE AVJET CORPORATION STC SA3094S0. 10. RELOCATED FIRE "T" HANDLES IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3111S0. 11. INSTALLED FAIRCHILD II PARAMETER FLIGHT DATA RECORDER IN ACCORDANCE WITH'PAGE AVJET CORPORATION STC SA3091S0. 12. INSTALLED DUAL 40 AMP HR NICKEL CADMIUM BATTERY SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3092S0. 13. INSTALLED DUAL HONEYWELL ADZ-800 DIGITAL AIR DATA SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3088S0. 14. INSTALLED AES AUTOPILOT INTERFACE UNIT IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3093S0. El Additional Sheets Are Attached • *U.S.OP0:1989 a 803•17t O • EFTA00277849

FAA AIRCRAFT REGISTRY CAMERA NO. At • .DATE:' - PAGE 3 OF 3 - . • . INSTALLED HYDRAULIC ACOUSTICAL FILTER IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3136S0. . INSTALLED ESSENTIAL POWER SELECTION SYSTEM IN ACCORDANCE WITH .PAGE AVJET CORPORATION STC SA259(T!:. 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 WORK 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. 6. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. END 0010404411'. 77,77:,.1....4;b, . • EFTA00277850

4. 41wartentwasintemam - • • W Sta . , ~~rt1ZR EFTA00277851

• FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 91 0 ' . • APPLICATION FOR US Derainlent AIRWORTHINESS or Trompoisoico • Federal Motion 500 L-9 CERTIFICATE Admirilownion -,• • . • • INSTRUCTIONS —Print or type. Do not write in shaded areas; these are for FAA use only. Submit original only lo an authorized FAA Representative. II additional space is required. use an attachment. For special flight permils complete SeCtiOns II and VI or VII as applicable. Z t 0 it 1.REGISTRATI immt • N Sb St 2.AIRCRAFT BUILDERS NAME (Make? 'Bo et IQ 6- • e .. 1 3. AIRCRAFT MODEL DESIGNATION -61 '... 3 I . - 4. YR. MFR /96/ r FAA CITING 3 F Vo / o 5 C' cc u .., . — Ma 5. AIRCRAF • a 0 iis- 6. NGINE BUILDER S AME (P.LiAw effint iiimey 7:3ge/ /TEL Dc.CeTIOtria$0 ,17-3 b - c3-19C Carta C OR C53 0 / 6. NUMBER OF ENGINES 9. PROPEL/En BUIL LA S NAME /Maker 4, vi 10. PROPELLER MODEL r cIGNATION 11. AIRCRAFT IS rChecA ii app4seaDiel :4 . A/ 4- iv i IMPORT a APPLICATION IS HEREBY MADE FOR: (Check andfiCable 4lenisl A i X STANDARD AIRWORTHINESS CERTIFICATE !Indicate category) I !NORMAL I [UTILITY I I ACROBATICD1(1 TRANSPORT I [GLIDER I [ BALLOON • B SPECIAL AIRWORTHINESS CERTIFICATE (Chock appropriate ?Semi? 2 . . LIMiTE05, o 'Ai 5 ai PROVISIONAL 1 CLASS I s. Widmer. Clan; q i3 O CLASS W 1 AGRICULTURE AND PEST CONTROL 2 AERIAL SURVEYING 3 AERIAL ADVERTISING cc Z 3 RESTRICTED fIndoCale OporatiONS r 10 be conducted; 4 FOREST; Wildlife conservflione s PATROLLING 6 WEATHER CONTROL 0 r:. < 7 CARRIAGE OF CARGO 0 OTHER (Speedy( 0 7. 1 RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT 3 EXHIBITION cc . W 4 EXPERIMENTAL (Inciter* opersborest to to condo:WO • 4 RACING s CREW TRAINING MKT SURVEY . U • . 0 70 SHOW COMPLIANCE WITH F AR 1 FERRY FLIGHT FOR REPAIRS. ALTERATIONS. MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT ihrdicale 2 EVACUATE FROM AREA OF IMPENDING DANGER A A n. e oporet,ort lobo conducted. Wen complete Section VIM VII as 3 OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WEIGHT apphcablo On serene sycliN 4 DELIVERING OR EXPORT • r5 I I PRODUCTION FLIGHT TESTING 6 CUSTOMER DEMONSTRATION FLIGHTS C 16 I MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE 'Rest(t led Operation and 'Standard' or • L.noled as turr,cabie r A. REGISTERED OWNER (As shown on certificate of anCiall registration) IF DEALER. CHECK MERE 4 NAME VOVZICOEST" 6 10 4.2)./A)Ce e. d e+c, ADDRESS /may rev Cg - icAwerin, ,a> R, . ti(ne /Ss zfraiku4-(6-- /Foos B. AIRCRAFT CERTIFICATION BASIS (Gncc* anplitable Wachs arid COmpfetv items al indica ect) 1 S p 3 AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE DATA SHEET /Give No and Revision Nal 3 1J ,i4 fr AIRWORTHINESS DIRECTIVES iCtioca;a/ai:esvereabte latest AD No )4 O9O AD s complied with and gar 4) ._ a . C g AIRCRAFT LISTING (Gov pego nontoell ell /O A X,IPPLEQNT AL TYPE CERTIFICATE 1/4 8 l itifri (List number of earn S TC incorpcualoc0 !Twee/ 623./ /990 15 C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS t • 0 CHECK IF RECORDS IN.* COMPLIANCE WITH FAA 91 173 . TOTAL AIRFRAME Nouns . , cs, 94/4./ .. . EXPERIMENTAL ;5504.41 r 'ICI vans 51000 lass VII f; ONLY r -I c I Cale co reneiree4 D. CERTIFICATION — I hobby Cellily ItiAl I III the iegislesed owner (penis agent; til the ariciall deathbed above. mar 1/00 ancial1 Admonish/Ilion an accordance with Suchen 501 cil the Federal Mullion ALI 0119511.atin applicable Federal Avialion RegulattoiLs.tusd airworthy and eligible for the airworthiness ter Oman: rem •' rid .... ... . . . - 4,07— 40. Ttroir-- • is Thal 1110 iegisleted with the Federal *rialto° RIICIall has been inspected and is DATE OF APPLICATION E AND TITLE HUM It % . \ - SIGNAT UR (-c-, 774-4/ 0 , 3 / 990 (di. yl A. THE AIRCRAF I DESCRIBED ABOV I IAS ([LEN INSPECTED A D FOUND AIRWORTHY BY (Conn/few ;h... •••. .oti only if FAR 21.1671( I onseaf nr.thsptcrio AGENCY veRincemot I 4. '" FAR PART 121 OR 127 CERTIFICATE HOLDER (Give Cerrthesto No 1 3- CERTIFICATED MECHANIC (Girt. Cartrircale NO. I — - - - • 6 CERTIFICATED REPAIR STATION (Gat Certificate No 1 • AIRCRAFT MANUFACTURER ;Grre name of font? • — — - t _. . DATE . TITLE .. .... • .. _ SIGNATURE ' .. . . Whets ALL ,ipplicablo blocks in dents A a dB) THE CERTIFICATE REQUESTED A. yawl dial die anciall described in Section I or VII meets retarireinenis for. AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE 1. Z r. 0 B. Insociclion lot a special High: peed under Sect. 'FAA INSFIECTOR . ... ... . • —.. lr-„. AA DESIGNEE ot g vats conducted by. . . . CERTIFICATE HOLDER UNDER: FAR 65 [ _I FAR 121. 127 or 135] 1 FAR 145 g a > c iv ki w c U e ..• DATE **ID DISTRICT OFFICE • . RE A 1, : . DESIGNEE S SIGNATURE F5 .' N rIl ._. __ % 1Vvi D2. ... AI\ FAA INSPECTOR'S SIGNATURE • . . . . : ' .' • 3:71r 'n t;;Palt retir EFTA00277852

FAA AIRCRAFT REGISTRY CAMERA NO..) At DATE: 9 - 27 - 97 *U.S.CPO:1989-241473/90913 • . • ' • PROOON . . . . • .. 1 • Mt SPECIAL FLIGHT PERMIT PURPOSES'OTHER THAN PRODUCTION FLIGHT TEST VI . • • • FLIGHUCTI T TESTING • . . . - . • . .. . . . _ : . . . . .. . . - . .. . . A. MANUFACTURER. S NAME . .. . •• - . .. . _ • - ADDRESS - .. • . , B. PRODUCTION BASIS (Check applicable item) - PRODUCTION CERTIFICATE (Give reduction COW:Cato numbs') TYPE CERTIFICATE ONLY • .. . .. ............ .. APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE QUANTITY OF CERTIFICATES REWIRED FOR OPERATING NEEDS DATE OF APPLICATION NAME AND TITLE (Prop or typo) SIGNATURE A. ' ... • • . DESCRIPTION OF AIRCRAFT REGISTERED OWNER ADDRESS • • s BUILDER (MAW MODEL: SERIAL NUMBER . • "•- ,. . . - • . • REGISTRATION MARK • . B. DESCRIPTION FROM, OF FLIGHT • STONER DEMONSTRATION FLIGHTS l 0 jebeea d abolicabiel • • • ... . .... ,.. ... .. .. .,.. ,... TO • • .. ... . . .. .. .. .. .. . • VIA • . .. . . . . . . . . . . -. • . DEPARTURE DATE . . DURATION C. CREW REQUIRED TO OPERATE THE AIRCRAFT AND ITS EQUIPMENT.: -- \ : • • I PICOT COPILOT NAVIGATOR • OTHER /Speedy/ .13. THE AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS REQUIREMENTS AS FOLLOWS. .. . . . . . . , . . . • ' ' • • . • ". - . • . .' . . ... . .• • • . . _ . .... . . ..,.. _.. _ _ ........ . ....... ..... .. .. . . . . - •- ._ . • '. -.. • ...... : : "- -...‘. '.., CA:: • c •'' • : '` - i . „ . • s `.. -. 5.‘11.2.•,- . V i•-•• .' ..i.*:•• 7:i-: •• • ., • . . . . ..- • .. • .. .. •. . . . . .. I , r- , • . i ; , • • •• -• i . ' • .":•• .... . E. THE FOLLOWING RESTRICTIONS .ARE CONSIDERED NECESSARY FOR SAFE OPERATION ruse effacement ,0 necessary; ; • . . . ! i ; i I . 3 •,..... r" ... • • , . • • • ' - - • . .. -. - ....-....... „..--- - .. . . ...„ .. .. -..... . - -.... . ... . -. • - .. • : 1 I ; s ! ..• r•:•: • c •• • :, • • ,, ., ; . .4. '. I .. ' . . % .. • .: •.'; •:.* • Ir•l"••••: •.* I • .. . , .... , • • . .. : .:.. : ; r.I.V:r.I.• Cr" ? . I Y i • . i I f . 7. t : f.ol a.:. a •c.. ! • :••: i : \ • ._. . .-., . • • i. ..; - • • • • • • • • •• , • • 6 1 • ! • . .. .:i.. . . • .. . • . . - • : • . • f. CERT IFICATION — I hereby certilythell ant the registered owner tor nia agonbollhaerallalssarawslabove.IntIlwaecransregaleravalhan FederalA.O1UP% Adm satiation tn ...v. • accordance with Section 501 of the Fetleral•Avialion, Ad of 1958, and imitable Federal Avestan Regialront and that the Nara Ins been Inspected and is airworthy for Ins high) .. described , . - .. OAT C . [NAME AND TITLE (Thint of typo) SIGNATURE • _ . . . , • • ' . . . . . .. [ VIII. AIRWORTHINESS DOCUMENTATION (FAA use only) A. Operliting Lunations and Markings InVriniPtuinirilelin FAR ' . 91.31 as Applicable ' • • • . ... . . . .. i.. O..Slidstalent of Com o i mily. FAA Form 01304 (05(tath when require**. .- H. FOllfieriiiilifOtihtn!“ Cerhi;Calion. the fritpOri Airafal— . • ... --- •-••.:: • 1 }Aback when toZhatedl • . "`. " 1 - ".%''C t . % • • D. Cimeni Operably Limilolions Attached :• - • ••• l.':_• .1 • C. We. Drawings. Pholographs, etc. (iitlachechen toquiredi•'. ' • • 1 • I. Previous Auwonnin ' Cgicallis FAlit73 - . cadres willi::. (Oligtnal Allacht(11 V D. Current Weight and Balance InlosmatiOn Available in Aircraft . E, Major Repair and Alteration. FAA Forni 337 (Alraeh When iiquoitcli J. Current AnwortAiness nificat I's in Accordencesvah . ... . . . 1 1 FAR :2 11 .. 1 . ) • /Copy inched) V F. This Inspecah Racurded f M . etall Records . , . ; , . • ' ' EFTA00277853

• FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 91 a. 4 Ot.kr", it.'421 ••••• • 0 • : . . • • • • • • • 'a . • . ' ••.' • . . • UNITED STATES OF AMERICA , DEPARTMENT OF TRANSPORTATION—FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE, , 1. NATIONALITY AND 2 MANUFACTURER AND MODEL REGISTRATION MARKS N505C BOEING 727-31 3 AIRCRAFT SERIAL A CATEGORY NUMBER 20115 TRANSPORT s•• • • . . • • •• ' - . • . •• .• • t • „ 1 • • • • • • • ' , • . 5. AUTHORITY AND ETAS S FOR ISSUANCE . • TNsainvorthiness certificate is issued pursuant to inFederal Aviation Act of 1958 and cenif es that. as of the date ol issuance. the •• aircraft to which issued has been inspected and found 10 conform to the type certifteme Therefor, 10 oe in 'condemn for sale • 'r "....•• r • ••• • operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as . . provided by Annex 8 to the Convention el. Iniernabonal Civil Aviation. except as noted here" Exceptions' NONE ' • • • . 6. TERMS AND CONDITIONS • .- • . . . • Unless sooner surrenclerea, suspended. 'evoked. Or a lerthination dale rS °MM.'Se established by the ACImintSlialOr. Ibis '.. ...?.... .. airworthiness certifies', rs effective as long as the maintenance. pievenlative maintenance. and anerabons are performed in ... .,,l accordance with PartS21. 43. and91 of theFederal AviationRegulations. as aPPI le. and the aocran is leg:Ste:ea .ntrieUnitecl ....; . .• , States DATE OF ISSUANCE 7/23/90 DESIGNATION NUMBER , • DAR-41-FS-NM - .•-• • •, • Any alteration. reprOduCliOn. Or M. use of this certificate may be purushableoy ot exc ng if 000 0 imposonmena erCeerbng 3 / , . . •.... years. or both THIS CERTIFICATE MUST .8E DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL I: . .:• • • •• • • AVIATION REGULATIONS. ' . ' • • • . . . . . FAA Form 8100-2 (8-821 0 IP • • • GPO si2•e04 • • - • • • • I. ••• • • • : • , a 9 - • • .. • x. • 7 : • -rm. • • ....N..— •—•••'. EFTA00277854

FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 21 EFTA00277855

Gk • • t 11 • • •• • rr• - • r • • ." • • • • . • . t 4 ' .•• •Ah.: 0A j • • • • . . ..• in , A . . r 0 . . MAJOR REPAIR AND ALTERATION . uS dearnmenr For or TIXISDOefOriOn ' • (Airframe, Powerplant, Propeller, or Appliance) R OI Avicnien OCIOC Act.wwwwwton Form Approved OMB No. 2120-0020 FAA Use Only Office Identification INSTRUCTIONS. Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This repot t is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51,000 for each such violation (Section 901 Federal AviatiOn Act of 1958). _-, 1. Aircraft Make BOEING Model • . 727-100 Serial No. 20115 ' Nationality and Registration Mark. N505C • 2. Ovine'' Name (As shown on registration certificate) NORTHWEST HOLDING CORPORATION Address (As shown on registration 1409 Foulk Road, Foulkstone Plaza, 'Wilmington, Delaware certificate) P.O. Box 7138 Suite 102 19803 3. For Use Only - _ 4. Unit Identification S. Type Unit Make Model . Serial No. Repair - Alteration AIRFRAME (As described in Item 1 above) X . POWERPLANT V PROPELLER ___ ___ _ ___. _ _____. _____ t{FPLIANCE Type Manufacturer . -- _ 6. Conformity Statement A. Agency's Nanakend Address l B. Kind of Agency C. Certificate No. North American Aircraft U.S. Certificated Mechamc , Airframe Class 4 Rockwell International Corporation I Foreign Cemficated mecnamc Limited Powerplant 2825 E. Avenue P I X I Certificated Repair Station Class 3 Palmdale, Ca. 93550 I Manufacturer NXAR6B8K D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pal 43,01 the U.S. Federal Aviation Regulations and that-the information furnished herein is true and correct to the best of my knowledge. i :,. / / Date July 20, 1990 I Signature of Authorized Individual I • D. A. Perazzo , /14.- .— T. Approval Col Return To Service . / ,......1,.../ " Pursuant to the authority given -persons specified below, Administrator of the Federal Aviation Administration and f the unit identified in item 4 was inspected in thezmanner prescribed by the is CD APPROVED -L7i REJECTED FAA Fit. Standards 1 Ins P i Manufacturer 1 Inspection Authorization Other (Specify) I • BY FAA Designee 1 x Repair Station Person Approved by Transport Canada Airworthiness Group n Date of APProvai or Rejection July 20, 1990 . 1I Certificate or Designation No. NXAR688K Signature of Authorized Individual • , I • ' U. A. Perazzo' II V t • I— FAA Form 337 • • EFTA00277856

r. _ hr:::1.1 tit .• • -•.; . • . • :, . • t...; ••, , I EFTA00277857

FAA AIRCRAFT REGISTRY CAMERA NO.9 DATE: 9 - 27 - 91 • ti • • 4 • 4." ' • 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 at Work Accomplished (if more space is required, art additional sheets. Identity with aircraft nationality and registration mark and date work completed.) • A. Modified Boeing Model 727-100 , Serial MUmber 20115, in mental type. certificate SA4363NM, amended September 1, T. Valsan-Boeing 727-200 Re-engining Document VA000001, • 15, 1990. . 2. The following drawings and engineering Orders (EWS) aboVe document: NOTE: "VA" denotes Valsan Drawing. a. Chapter 24 ELECTRICAL POWER . VA240000 A • Electrical System Initl. - Strut E.O.: 003A, 101 0240007 E Panel-Load Control Center Modification E.O.: 003A, 004, 005, & 006 b. accordance with supple- 1989 as follows: Revision F, dated January 's • are in addition to the Chapter 28 FUEL SYSTEM INSTALLATION, STRUT VA280001 B Tube Assy - Fuel Strut Feed Thru E.O.: 100 c. Chapter 48 MISC VA481100 A VA481200 C VA481300 C VA481324' NC VA481325 NC, d. Chapter 53 FUSELAGE VA6.30001 8 VA530003 C • VA530004 - NC Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 Frame Assy Sta 1263 E.0.:.101, 103 Fuselage Skin E.O.: 106, 114A, 114, 116 Intercostal Assy - BSTA 1223-to BSTA 1243 W/L244.39 E.0: 106, Intercostal Assy - BSTA 1223 to BSTA 1243 W/L234.06 E.O: 105 STRUCTURE Ballast Weight Installation E.O: 100, 102 Ballast Weight, Support Structure Assy. E.O.: 002,100 Ballast Weight Instl. STA 312 - 360 E.O.: 002, 100 e. Chapter 54 NACELLES & PYLONS VA543000• C Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 -VA543100 D Firewaii Rib, Side Engine E.O: 36A, 003A f.' Chapter 71 POWER PLANT, VA710000 NC Power Plant Instl. - Engine Pod V727RE E.O.: 002, 105B, 109, 108, 001A, 104A, 005A, 004, 110, 003, 111, 006A Chapter 73 ENGINE g. FUEL AND CONTROL VA732301 .K Approach Idle Solenoid Wiring Diagram E.O: 002(Rev L), . 002 (Rev. M), 003(Rev. M) VA732303 0 Relay Instl. - Approach Idle Solenoid E:0.:. 103, 003, 100B VA732304 0 Switch/IND Light Instl - Approach Idle E.O.: 002, VA732310 A Switch Instl. - Nose Gear Position Approach Idle £.0.: 103 VA732315 NC Relay Instl. Pilots Overhead Panel E.O.: 100, 002, 101 - h. Chapter 76 ENGINE CONTROL VA760000 A Engine Controls Instl. - Strut E.O.: 00ZA VA760014. A Drum Instl. - Eng. Controls E.O.: 100, 101 VA760015 A Bracket Assy - Pulley ESTA 100 E.O.: 105 (1§ Additional Sheets Are Attached • U.S. GP0,1989.0-663. 11 EFTA00277858

FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 91 EFTA00277859

FAA AIRCRAFT REGISTRY CAMERA NO2 A' DATE: 9 - 27 - 9/ P. k• . - r DESCRIPTION OF WORK ACCOMPLISHED 1ContinuedY Serial No. 20115 .Chapter.77.ENGINE INDICATING VA771005 NC Indicator:Engine,?ressu're Ratio EPR, E.O.: 001 Chapter 78 ENGINE VA780000 B VA783010 E VA78301I- F, VA783013 D - VA783017 J VA783024 B VA783028 A VA783101 C. 'Chapter 91 CUARTS• VA910002 ' A VA910008 NC EXHAUST , • a . • Engine Strut Controls Instl. Fit Deck -Indicator Ihstl. 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. Placardi E.O.: 007, 008 Relay Instl. - Thrust Reverser Control E.O.: 003 Mixer, Exhaust - Instl. 727E E.0:: 100 No. 2 Engine T/R Wiring Deactiviation E.0.: 002 ° Instl. - Electrical Wire Harness E.O.: 003, 004, 005,006, 007 • Wire List V727RE E.O.: 001, 002, 003 • • , *NEW DRAWINGS ADDED TO MODIFICATION Boeing 727 Service Bulletin 727-53A0171, dated December 14, 1989 SUbject: Fuselage - Station 1182 Pressare Bulkhead web, . Crack Repair and Preventive Modification • • . . , C.. 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. . . . . D. VA000003, Rev. A, Dated 4-4-90 is equivalent to VA000001, Rev. F, dated 1-15-90. END Sri EFTA00277860

r, FAA AIRCRAFT REGISTRY CAMERA NO3 DATE: 9 - 27 - 97 • EFTA00277861

• FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 27 - 91 pa,5649-tioat i. PERSONNEL ACCOMPLISHING THE CHECK LIST WILL INITIAL EACH ITEM IWTHE APPLICABLE BLOCK FOR PARTS A THROUGH D. N/A BLOCKS NOT APPLICABLE TO A/C BEING WEIGHED. 2. ALL BOTTLES (02CO2, H20) SHOULD BE IN NORMAL OPERATIONAL CONDITION. 3. ANY DEVIATION FROM THIS LIST MUST BE COORDINATED WITH CHIEF INSPECTOR OR HIS DESIGNEE: 4. ON CONIPLErION OF PARTS A THROUGH D THE FOREMAN/LEAD MECHANIC OR ASSIGVED INSPECTOR WILL CHECK & SIGN FORM BE• FORE PROCEEDING WITH WEIGHING. ti9 FLUIDS Checked pV . Checke By 1. FILL ENG. OIL SYSTEMS & TANKS FULL . VI.4-1- 7 k." • 6. LAVATORIES CLEANED & VACUUMED ' Q 2 ALL FUEL TANKS DRAINED USING DRAIN PLUGS WI (H AIRCRAFT LEVEL 4. 0,,,. ...r 50•7. , ALL MAGAZINES, NEWSPAPERS & SEAT BACK . 7< LITERATURE REMOVED ke %43%d • 3. DRINKING di 1e)ASH DRAINED EL WATER TANKS FILLED 1... i - .. B. -PROTECTLVE ENTRY, AISLE & STAIR COVERS REMOVED ' - 1:0 1 ‘i‘ 4. HYDRAULIC SYSTEMS FULL ! • •\ \ • 9. WINDSCREEN STOWAGE EMPTY & CLEAN WV , 5. TOILETS SERVICED TO NORMAL QUANTITY e<74-2;" ..in cr -•• ei • • STOWAGE COMPARTMENTS ON FWD. & AFT. LAV. — . BULKHEADS EMPTY .iitV 6. SEAPLANES: DRAIN HULL & WING FLOATS COMPLETELY le/4yred- r;2- . . 0 CONTROL CABIN . • . _ 1 J . ALL INSTRUMENT PANELS COMPLETE ?:)11iA D. CARGO, LANDING GEAR & POWERPLANT - . • .<, 1 a c 2 ALL MANUALS; CHECKLISTS, LOG BOOKS, FORMS & OTHER WRITTEN MATERIAL REMOVED CO/ 2//f • 1. ENGINE FIRE BOTTLES CHARGED kt b r i •- 3 ' ALL CREW SEATS COMPLETE WITH SEAT BELTS & . HARNESSES INSTALLED 4,er .1//f 2 ALL ENGINES COMPLETE I.E., ACCESSORIES, PLUMBING, ETC. e 4 FLIGHT ENGINEERS TABLE EMPTY & . CLEAN EXCEPT FOR STRETCHER KIT i ALL COWLING & PANELS IN PLACE & SECURED 7..riew,' C. PASSENGER CABIN . X 4. 4 BRAKE AIR BOTTLE CHARGED. ..r.A. ..- 7 • REMOVE ALL ITEMS FROM HATRACKS EXCEPT 1. MEGAPHONES, FIRST AID KIT, MOUNTED OXY. BOTTLES, DEMO OXY. MASK & LIFE VEST IN S. ALL AVIONICS EQUIPMENT INSTALLED -P, • 12 • POUCH 6 FWD, & AFT, CARGO COMPARTMENT EMPTY & CLEANED • SI. 2. ALL PASSENGER SERVICE EQUIPMENT REMOVED FROM GALLEY ' Xis A MAIN OXYGEN SYSTEM SERVICED • 7' FULL 71,4"--a` 7 7 •:' ALL SERVICE EQUIPMENT REMOVED 3. FROM FWD. & AFT. LAVATORIES • a MAIN BATTERY & AUX. BATTERY (IF USED) INSTALLED q...N, ,t.). _ -Not ) _ 4. ALL GALLEY AREAS CLEANED & . VACUUMED • CARGO DOORS & FAIRINGS CLOSED & . a LATCHED .-6-.:--: 5. PASSENGER CABIN CLEANED & VACUUMED nb; &,A) LL TIRES A INFLATED TO OPERATING 10• PRESSURE , ' ce7:: 00-- -9)114-v _AIRCRAFT READY FOR WEIGHING as Ariz alo , Aiil ica4 h ?VERSO% ISO AIM • •••• • • . -•,1/4 EFTA00277862

FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 27 . • , • '• !I ,;•".?.• • • '7. ' . tt• -: ' . i .„ • : ;en,. r.••,;1•:-....c. t 4 -e41-4‘ vrk.:-%peroler.44t4;,*. 4•1w,:‘' •1 ; .0 • -a :; . ; •• ". . ' . • ' •17 •i'.. -••:14.1:1::S. • ." . • '. ••••.:- . . . • • . r '• .r. :.• . .• • • 41 .cr EFTA00277863

I FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 91 • AIRCRAFT WEIGHING SCALES: MAKE Eliereeeen ) SERIAL NO. 10(e? -"FIRST WEIGH Nt h MODEL —zwiw awainicmaaTiCOn4041, r.L. • CALIBRATION DATE 5 3 - 9.0 REACTION SCALE READING CORRECTION CALIBRATION CELL DRIFT TARE NET WEIGHT LEFT ML INGge RIGHT "L INGO OS AIL Ya - 4 7 7 3.5 -2o -e0- -62- 1/ 7715-- ligg0 ° - SO ---662- - - iiY75-0 93 `S +1 0 q 3 55- 1 / CIRCLE REACTION USED NET WEIGHT TOTAL 10O1 2T2O SECOND WEIGH REACTION SCALE READING CALIBRATION .CORRECTION CELL DRIFT TARE NET WEIGHT MLG LEFT WING RIGHT MLG WING NOSE/TAIL 11-7 750 -5-O -79- 41 417 9'OO ‘//741.0 +10 -69- -re Ile 120 l 'i3 5- a 6 3 '69' Lt 3 (O 1 / CIRCLE REACTION USED i NET WE GHT TOTAL 1 00/ th CY -5- ST 1. WEIGHING COMPLETED 2. WITNESSED & ACCEPTED Foreman/Lead Mech. Or Inspec 0)1444.4-d ICt4.421,4- Chief Inspector Or Designee NOTE: PART F. AND SUBSEQUENT PARTS TO BE ACCOMPLISHED BY THE QUALITY CONTROL SECTION. NET WEIGHT AVERAGE FIRST WEIGH SECOND WEIGH TOTAL AVERAGE MLG LEFT VVING _ MLG RIGHT WING NOSE/TAIL 117 715- Li F75-0 1-1-355- 91900 q a' Li 20 113425- 956 IS 91 / 7O X72O q 7 Sac ggs-75-- 4t3tho CHECKED BY PAGE 2 OF 3 ' EFTA00277864

FAA AIRCRAFT REGISTRY CAMERA NO.3 4/ DATE: 9 - 27 - 97 . • . . ,,.• . • •, • . . . . .6 4 .6. nl EFTA00277865

FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 97 11 CIRCLE REACTIONS USED. 2. ENTER AVERAGED NET WEIGHTS FROM PART F. BEW ITEMS NOT ON AIRCRAF ATTACH SUPPLEMENT IF ADDITIONAL SPACE IS REQUIRED TOTAL AS WEIGHED SUB TOTAL ITEMS WEIGHED BUT NOT TO BE INCLUDED IN DEW ATTACH SUPPLEMENT IF ADDITIONAL SPACE IS REQUIRED SUB TOTAL BASIC EMPTY WEIGHT REACTION DATE 7 70 41 360 b 200 in.552,5" CHECKED BY 7-3/, 2. 925., 27 MOMENT 45,4124,6e6.-5- ISC1 PAGE 3 OF 3 EFTA00277866

FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 91 • •••• .•• _ • ._t •• .• E. . • • ••••• • ..• .4, . .. .. If • , c. I • 1 0 i • i ‘1 ‘ ‘ ... • ....gm ...Ob. • 1 ...E..... Z: • . • • . . I 1 ; • • . . • 1 • • • . ',. . • • 1 is . • t .. ••••• ••• • .....•• • •• ••• ..... •••••••• A : • ••• dm ..• ... • k . i • 3 EFTA00277867

• z FAA AIRCRAFT REGISTRY CAMERA NO3 A' DATE: 9 - - 97 • Uan TED STATES OF AMERICA . , • - " ' DEPARTMENT OF TRANSPORTATION.- FEDERAL AVIATION ADMIAISTRATION -SPECIAL AIRWORTHINESS CERTIFICATE A Y C A T E G Op Y / 0 E S i G N A T I ON EXPERIMENTAL •-• , • PURPOSE SHOW COMPLIANCE WITH FAR / MARKET SURVEY :• 1.. , 6-. MANU- , FACTURO NAME N/A 3 ADDRESS . N/A . .. _ C FLIGHT/ FROM • N/A TO N/A D N- 505C SERIAL NO. 20115, ., BUILDER BOEING MODEL 727-31 E DATE OF ISSUANCE 05-01-90 EXPIRY 08-01-90 OPERATING LIMITATIONS DATE 05-01-90 ARE A PART OF THIS CERTIFICATE SIGNATURE qr F REPRE r 'MICHAEL J. SON . i DESIGNATION OR OFFICE NC: . • ' • SEA-MIDO, ANM-108S Any ENFrattOn, reproduction imprisonment not exceeding ACCORDANCE WITH or misuse of this certificate may be punishable by a line not exceeding $1.000 or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN 3 years. FEDERAL APPLICABLE FEDERAL AVIATION REGULATIONS. FAA FORM itiO4 (loam ,•• SEE REVERSE SIDE • t • • : • • • t . ▪ , • , • ' • ▪ . . •••• : • N. • " • . . • . • o , EFTA00277868

FAA AIRCRAFT REGISTRY CAMERA N0.9 N DATE: 9 - Z7 - A This airworthiness certilicate is issued under the authority of the Federal Aviation,Act of 1958' v • and the Federal Aviation Regulations (FAR). • • . '. . B --.• C •—•••••••• O . . . This airworthiness certificate authorizes the manufacturer named on the reverse side to conduct production flight tests, and only production flight tests. of aircraft registered in his name. No person may conduct production flight tests under this certificate: (1) 'Carrying' persons'or property for compensation or hire; and/or (2) Carrying persons notessential to the purpoie of the flight. ; '• ' • .. • 1/4., ...... This airworthiness certificate authorizes the flight specified on the reverse side for,z‘rpose shown in Block A. . • • .. - - ' ( .. ' . . - • . • • • cS,i This airworthiness certificatecertifies that, as of the date of issuance, the aircraft to W. ich issued has been inspected and found to meet the requirements of the applicable FAR. The aircraft does not meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention On International Civil Aviation. No person may operate the aircraft described on the reverse sit (1)except in'accordance with the appliCable FAR and in accordance with conditions and limitation: which may be prescribed by the Administrator as part of this certificate; (2) over any foreign country without the. special permission of that . . . . , country. • . ic • • • - - • . . c E ... Unless sooner surrendered. suspended, or revoked. this airworthiness certificate is effective for the duration and under the conditions prescribed in FAR Part 21. Section 21.181 or.21217. . • - - rsf 1 1.4 EFTA00277869

7 2.Yety FAA AIRCRAFT REGISTRY CAMERA 6,:)..3 iV DATE: 9 - 27 - 97 • 4 sktrir, nos r "'Yr ti •VW ar . " • . . gt. •\ • 1. . • . . • • • • .• • • • •••• . • • • • . 4 • U.S. Department of Transportation Federal Aviation Administration Manufacturing Inspection District. Office 7300 Perimeter -Road South Seattle, WA 98108 May 1, 1990 EXPERIMENTAL -SHOW COMPLIANCE WITH FAR's/MARKET SURVEY MAKE: Boeing . MODEL: 727-31 SERIAL NO. 201157: • REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. No person may operate this aircraft for other than the purpose of Show Compliance with the FAR's and Market Survey to accomplish, the tests outlined in the applicant's program letter dated May 1, 1990 describing compliance with FAR 21.193(d). Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi River, on the- North by the U.S.A./Canadian border, on the South by the U.S.A./Mexico border, dnd bounded on the West by no more than 200 miles from the West Coast of the United States of America. ! • A 2. Base of operations is Palmdale/Lancaster Airport, i Palmdale, California and secondary base of operation to be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book endorsement or possess a "Letter of Authorization" issued by an FAA General Aviation or Air Carrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and opera4-ed in accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the aircraft is in a condition appropriate for the purpose intended and has documented that finding in the aircraft log. 6. This aircraft shall contain the placards, markings, etc. required by FAR 91.31. • • EFTA00277870

FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 97 EFTA00277871

FAA AIRCRAFT REGISTRY CAMERA N0.3 N DATE: 9 - 27 - 91 • Federal Aviation Administration Manufacturing Inspection District Office Experimental - Show Compliance with FAR's/Market Survey, Cont'd Page 2 of 2 7. The cognizant FAA office must be notified. and their response • received in .writingprior to flying this aircraft after - incorporating a major change.. as defined by FAR'21.93. . 8.• This aircraft approved for day/night VFR/IFR only. '"No operations shall be conducted over densely populated areas or in Congested airways except for takeoffs and landings, and when under.ATC control. :10. No person may be carried in this aircraft during flight unless that person is essential for the purpose of the flight while in the Show Compliance category. 11. This aircraft is prohibited -prom aerobatic flight; that is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved by the cognizant FAA office. 12. If aircraft engipe.or propeller operating limitations are exceeded, an.appropriate entry will be made in the historical records. 13. After the aircraft has been re-engined, the pilot-in-command must make a log book entry stating the aircraft complies with FAR 91.42(a) and FAR 91.42(b). Mic ael J. son Aviation Sa ty Inspector (Mfg) SEA-MIDO, ANM-108S These limitations will expire on August 1, 1990. J1 EFTA00277872

-ti 4: kith- ••• r cs '0. r. • • .7, • ^ .a.•••••:. •• .• • _ EFTA00277873

, .. • • MAJOR REPAIR AND ALTERATION uSDecianrrient of nomoonction (Airframe, Powerplant, Propeller, or Appliance) Peen MiatiOn Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification 7A/y gs ad INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report le required by law (49 U.S.C. 1421). Failure to report can result in acilejl penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). RECEIVE[} FAA Make BOEING Model 727-100 - 2't L-9.0 1. Aircraft Serial No. • 20115 Nationality and Registration Mark jUi N505C 1/14Y 11;[)() 2. Owner Name (As shown on registration certificate) . NORTHWEST HOLDING CORPORATION Address (As shown on registration certificate) -1409 Foulk Road, P.O. Box 7138 Fpulkstone Plaza, Suite 102 Wilmington, "Delaware 19803 3. For FAA Use. Only - • - _ . 4. Unit Identification 5. Type . Unit Make ' Model - Serial No. Repair , . Alteration — . . AIRFRAME . (As in Item 1 above) - X _described • POWERPLANT, - PROPELLER • • - -- .--- - ---- • _ _ ___ APPLIANCE Type Manufacturer • t - - - - • ' 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. North AHL.-ican Aircraft U.S. Certif cated Mechanic Airframe Class 4 Rockwell International Corporation Foreign Cen baited Mechanic LiMited Powerplant 2825 E. Avenue P X Certificated Repo I Station Class 3 Palmdale Ca. 93550 • Manufacturer NXAR688K • D. I certify that the repair and/or alteration made to the un have been made in accordance with the requirements furnished herein is true and correct to the best of my t(s) identified In item 4 above and described on the reverse or attachments hereto of Part 43.of the U.S. Federal Aviation,RegulatIons and that-the infornation knowledge. i / Date • July 20, 1990 Signature of Authorized Individual . D. A. Perazzo kJ 7. Approval for Return To Service j Pu suant 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 cg. APPROVED :-.7. REJECTED !. FAA Fit. Standards Inspector • I Manufacturer Inspection Authorization Other (Specify) • BY FAA Designee x Repair Station Per I Parson by Transport Approved Canada Airworthiness Group (Th i l Date of Approval or Rejection July 20, 1990 Certificate or Designation No. NXAR688K Signature of Authorized Individual i U. A. Perazzo h . ' . . .. ,..._. i- FAA Form 337 ti y Hsi t, t EFTA00277874

NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. - - B. Description of WorteAccornplIshed (It more space is required, attach additional shoots. identify with aircraft nationality and registration mark and date work completed ) A. Modified Boeing Model 727-100 , Serial Number 20115, in accordance with supple- mental type certificate SA4363NM, amended September 1, 1989 as follows: 1. Valsan-Boeing 727-200 Re-engining Document VA000001, Revision F, dated January 15, 1990. 2. The following drawings and engineering orders (E0's) are in addition to the above document:: NOTE: "VA" denotes Valsan Drwing. a. Chapter 24 ELECTRICAL POWER VA240000 A Electrical System Instl. - Strut E.O.: 003A, 101 VA240007 E Panel-Load Control Center Modification E.D.: 003A, 004, 005, & 006 b. Chapter 28 FUEL SYSTEM INSTALLATION, STRUT VA2-80001 B Tube Assy - Fuel Strut Feed Thru E.O.: 100 c. Chapter 48 MISC VA481100 A VA481200 C VA481300 C VA481324 NC VA481325 NC Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 Frame Assy Sta 1263 E.O.: 101, 103 Fuselage Skin E.0.: 106; 114A, 114, 116 Intercostal Assy — BSTA 1223 to BSTA 1243 W/L244.39 E.0: 106 Intercostal Assy - BSTA 1223 to BSTA 1243 W/L234.0b E.0: 105 d. Chapter 53 FUSELAGE STRUCTURE VA530001 B Ballast Weight Installation E.0: 100, 102 VA530003 C Ballast Weight, Support Structure Assy. E.O.: .002,100 VA530004 NC Ballast Weight Instl. STA 312 - 360 E.U.: 002, 100 e. Chapter 54 NACELLES & PYLONS VA543000. C Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 VA543100 D Firewall Rib, Side Engine E.0: 36A, 003A f. Chapter 71 POWER PLANT VA710000 NC Power Plant Instl. - Engine Pod V727RE E.O.: 002, 105B, 109, 108, 001A, 104A, 005A, 004, 110, 003, l ii, 006A Chapter 73 ENGINE FUEL AND CONTROL VA732301 K Approach Idle Solenoid Wiring Diagram E.0: 002(Rev L), 002 (Rev. M), 003(Rev. M) VA732303 D Relay Instl. - Approach Idle Solenoid E.O.: 103, 003, 100B VA732304 D Switch/IND Light Instl - Approach rdle E.O.: 002, VA732310 A Switch Instl. - Nose Gear Position Approach Idle E.U.: 103 VA732315 NC Relay Instl. Pilots Overhead Panel E.O.: 100, 002, 101 h. Chapter 76 ENGINE CONTROL tA760000 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 g Additional ',.neets Ard Attached .U.SCIP(11989.0.600 71 y'` - • EFTA00277875

-` • AAYft'GtA` t, k • CANER!. 7 D. I.N DATts 2 g • Itt DESCRIPTIQN OF WORK ACCOMPLISHED (tontinued) :;"11 . i.- Chapter 77 ENGINE INDICATING - VA771005 NC Indicator Engine Pressure Ratio EPR, E.O.: co! EXHAUST Engine Strut controls:'Instl..E.O.: 002. . )Flt Deck 'Indicator Instl T/RSys. E.0.L.003, 004 Thrust Reverser System Wiring. Diagram 002'(Rev. G) :Support Bracket AsSy:=:T/R'COntrOl Valve R/S 100 (ReV. E) •Placards*E.O.:pp,0308 'Relay Instl.. -. ThruStReverter Control E.O.: 003' : .:Mixer, Exhaust -‘ Instl..727E.10.: 100 • No. 2 Engine TM Wiring Peactiviation E.O.: 002 - Chapter 78 ENGINE VA780000 B • VA783010. E VA783011 F VA783013 D VA783017 J' VA783024. VA783028 A • VA783101 C. k. Chapter 91 CHARTS VA910002. A * VA910008 NC *New driwings added to modification. Instl. ElectriCal Wire Harness E.O.:. 003, 004, 005, 006, 007 Wire List V727RE E.O.: 001, 002, 003 B. Boeing 727 Service Bulletin 72753A0171, *dated December'14, 1989. Subject: Fuselige - Station 1182 Pressure Bulkhead Web, • Crack Repair'and Preventive Modification . • C. The. aircraft empty weight and center of.gravity was revised in accordance with Boeing Weight and Balance Manual D6-21200. . Weight and Balance Manual Supplement, VA-CR279' •is attached. EFTA00277876

r I I l I k 榦 攥 私 ＞ , } 討 一 ： ： 一 ． 一 · 一 l I I . I F - ' “ 义 〉 : ， 一 一 一 r f - . I ' l !! EFTA00277877

ttk arc -tee_ 29 1991 0.t" q. No.212J-0018 0 . , - -- APPLICATION FOR us orpslinorr AIRWORTHINESS a lionwiu.ion • Fecteral Mahon 5" 010't S CERTIFICATE earrenraranon INSTRUCTIONS-Print or type. Do not write in 'laced antes: these are kr vs.,' use only. Submit Oulnal only to aniauthorized FAA Repreientalow. II additional space is required.-usean attachment. For special fl ght porn. Is complete Sections It and VI or VII as applicable. I. AIRCRAFT ❑ESCRIPT1ON 1 .REG.STRA C. 2.AIRCRAFT BUILDERS NAME (Mew C 50 Eti U 6 . 1 AIRCRACT MODEL DESIRNATIOI4 - .ift 1 72 7 — Avaritspi,4-> MA .• /..i.3 O. I. AIRCRAFT SERrAL NO 0 / /S. 6. ENGINE BUILDER'S NAMEThaikci IL) . I. ENGiNi .MODEL DESIGNATI Br> .1-. .7 A - 21 et - . 7. NUMBER OF ENGINES si ti fte O. PROPEL!, ER Still pr.11- AME AL .-; 9. *ROPE ..1.5 R MODEL 0ESiGNATION 10. AIRCRAFT iS (Crack ii SODiatit, _,..3 • all ik._>I/ I 'IMPORT APPUCATION IS HEREBY MADE FOR: (Cheek atftlicible iremsi. ' . le. A V ' STANDARD AIRWORTHINESS CERTIFICATE Umlaute carvuo., . iit i•••••••O I jUliLITY ACROBATIC] 1 TRANSPORT 1 _1 GLIDER BALLOON B L SPECIAL AIRWORTHINESS CERTIFICATE (Check app. onique din!. \ 2 LIMITED .- 1 - - G. ASS I S PROVISIONAL (indicatekraal 1 2 . • -CLASS II • g 0 se AGRICULTURE AND PEST CONTROL 2 AERIAL SURVEYING $ AERIAL ADVERTISING CC . 1 . RESTRICTED/Indicate Os co/Murat:ft • operehon(0 ID • FOREST (Wareile conservahwq 3 PATROLLING : ' II WEATHER CONTROL O • - • •• • . 7 CARRIAGE OF CARGO 0 OTHER iSpecdp/ ' 1 .. • . 1 RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT .3 EXHIBITION i A EXPERIMENTAL (InditeM to De ccoducted) Operettor(s) . - . .- )itk RACING S CREW TRAINING N MKT. SURVEY d •' bi TO SHOW COMPLIANCE WITH FAR ' • - • • • 1 FERRY FLIGHT FOR REPAIRS, ALTERATIONS. MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT (Indicate 2 EVACUATE FROM AREA OF IMPENDING DANGER • • . operation to be conducted. Section VI then i c. Vil • — ' - i - ' OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WEIGHT . • complete applicable on mites or es. saes: • a DELIVERING OR EXPORT 1.51 I PRODUCTION FLIGHT TESTING $ . CUSTOMER DEMONSTRATION FLIGHTS C 1 MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE -Restricted Opera)ion- and 'Standard' Or linuted.- as applwablej A. REGISTERED OWNER (Ar shown on cashier-aloof aircraft registration) IF DEALER. CHECK HERE I NAM!, , N10 41-44650-61" ge, LA I Ws. . • • .. ,( e,s90 Cenp Ay on. • ADDRESS ... rat PCS-Vole PA4 VA 15 cale era, Ai? rater koAn 61.6. lei 1I3t tor Lws W6-Tew beAsioa ilIo3 A. AIRCRAFT CERTIFICATION BASIS (Check applicable blocks and complete arms as indica ad) g P 3 - AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE and Revision No.) DATA SHEET (Owe No. AIRWORTHINESS DIRECTIVES (Chock it all inviable AD's complied with end wee latest AD NO.1 F I AIRCRAFT USTING (Give page number(s)) • SUPPLEMENTAL TYPE CERTIFICATE (List number °I each STC incorporated) 0 . C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS . . I bi CHECK IF RECORDSIN • COMPLIANCE WITH FAR 91.173 TOTAL AIRFRAME HOURS Pf gg'ie 2 • . . --., iF Tli ikkE EXPERIMENTAL ONLY (Enter hours flown since lest certiliiiale issued or renewed/ /9, g 0. CERTIFICATION — I hereby Willy thal I Administration In accordance with Section 50 aftworthy and eligible (or the aliworthine se certificate m the registered owner (or his earl) Of me airalft desCribed abort that IN aircraft of thefts:Mt Availed Act cal 1958. and applicable Federal AviatiorilleguLshons and . - . .. raquesiat - -" • . is registered with the Federal Aviation thal I he Sucre II hes beer nine salld .1. ATION . DATE OF ORLI,. ATION " Si/ 19 10 NAME AND TITLE (Print or type) rue • I ....t • ... (02441.17- • ?KA. 7 - / SI • A. 710 AIRCRAFT ESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Carnivore retie 'capon onty if FAR 21 183W) epphesl Z 0z 0 5 r; r t 61 . 'Tr:7, itli\ FAR PART 121 OR 127 CERTIFICATE HOLDER (Try Certificate Nal . . . ai Art (O CERTIFICATED MECHANiC (Owe . Culibcito No.) - CERTIFICATED REPAIR S(Al-ION:6,n Ceihhcaiii No.) 0 ° C ! • € I tili • XIPITRAFT MANUFACTURER/0Ni ahem* Of thin) i! i • DATE • TITLE. i .,: . SIGNATURE (Check ALL applicable blocks in items A end% .' 1 THE CERTIFICATE REO 'ESTEE, A. I find Om the aircraft described in Section I or VII male reiediremente lot, ot AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE • 1 g B. Inspection tor • special Mght pernalundir SectiOn VII -, • • • i FAA INSPECTOR FAA DESIGNEE ?.1 3 was conducted bir . ., CERTIFFCATF HGIOER UNDER: FAR 55 I 1FAR 121. 127 0 1351 1 FAR 145 . s g a DATE 45:61 49° DISTRICT.OFFICE - .' S EFIV" Altb0 ' ANAT .1649S .- . , " 40 DESIGNEES ., SIGNATURE AND NO . . • . ' . 1 AA INSPECTOR'S SIGNATURE • • FAA Conn 81304 (1243) SUPERSEDES PREVIOUS EDITION ' . 74,..ite. • • EFTA00277878

VI. PRODUCTION FLIGHT TESTING &MANUFACTURER. NAME - • , . . ADORPCS - ` B. PRODUCTION BASIS (Chock epootabie hemp PRODUCTION CERTIFICATE (Gee prOducUon creficate number) TYPE CERTIFICATE ONLY , APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE QUANTITY OF CERTIFICATES REQUIRED FOR NEEDS OPERATING DATE OF APPLICATION NAME AND TITLE (Print Or type) T SIGNATURE VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER THAN PRODUCTION FLIGHT TEST A. DESCRIPTION OF AIRCRAFT REGISTERED OWNER ADORES.) BLIILOER (Make) .. MODEL . • SERIAL NUMBER • • - N .. • REGISTRATION MARK ,:' • • . .. • • • • ' .... . . . ,, . . . I B. DESCRIPTION OF rucirkr.... • . ' “. ..._.. 4 &STORER DEMONSTRATION WORTS 0 tailor It sPOliceloW FROM ---• ...- VIA DEPARTURE DATE - • DURATION , • .. -_,.. ' . C. CREW I REQUIRED TO OPERATE THE AIRCRAFT AND ITS EQUIPMENT,. • 'PILOT , I I COPILOT : I I NAVIGATOR • I I OTHER (Specify) D. THE AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS REQUIREMENTS AS FOLLOWS: • • . - • • • . • • ..' .... . ... i . — ..." . .. . . . . • ' - • " . .. " " • - • ' • - .. • 1'1 - " • " ' - r _ . . .. • .i .• : . • • • • • • • • .. ..... .. .. . . . . it . .... .. - • .. - ,. _ - .... . . .. , - . .- . . . . _ •• , - - - E. THE FOLLOWING RESTRICTIONS ARE CONSIDERED NECESSARY f OR SAFE OPERATION (use attachment il necessary) ... .. . . • .... . . .. — . . - '•. - - .. . • . . • ' - • • • . . „. • - • r . . . . . . .,. . _ • .- . S ... : • . . • • • F. CERTIFICATION —1 hereb yceiThlty ItIM larrf the Ng 'marathoner (Or Ms agent) of UmaIrcraft deseri bidabovir.trail the aircraft la registered wish Ih•Federal Aviation Administration In accordance with Section 601 of the Federal Aviation Act of 1956. and applicable Federal AviationFlegulations• and the Sircratt has ban inspected and Ii airworthy for the flight described. ‘ • , • ' • ' . • : • •• • . DATE • • , . . NAME AND TITLE (Pant or rypej: N. • . . • .. .... SIGNATURE i I i 4 I i 3 a Ci g a 4 F V Operating Limitatiora.and Markings in "replant, with FAR • 91. 1 as pUcable CL,Stisteinent of Confcetnity, FAA Foi m 11130-9 (Attach when required) . H. Foreign Airworthiness Codification for Import Airc.A f Attach when required) . . . . . . . "'--: t. ve 2.„ B. Carron' Operating Wildfire Attached% i •• N. ' .. . . . --" C. Data. Drawing's, photographs. fit (Almon when foqukocl) I Pnnious Airworthiness Certificate Issued In Accordance with . FAR 2/. 191(b) CAR (Original Attached) / . D. Current Weight end Balance Inlonnation Available In Aircraft ' ' • • 4 ' E. Major Repair find Aberration. FAA Form 337 (hhech'When *end) • • dance with •L Current Airsortinnere Certificate Issued i Accor (Copy elisch Fan 21 .1910)) g n4 Q?) ed) keir F. This Inspection Recorded in Aircraft Records . 4 • -prewar ' 3`.11.,.. • • • . • EFTA00277879