EFTA00277880

.• A ^ . This tirWrihlillieseterli kat° is isSbettlinderikaltitilti.6* ofthe FikieratAyifttiCal AO Of 1958 , antl the Federal Aviation Regulations (FAR). B • This alrwo rth iness cert Ificate autho reesthe fated* narittid On thereireMeSidet0 donduct production flight tests, and only production Ng 11631.1:61 aircraft registered in his name. No ' person may conduct production flight tests linderithIS certificate: (1) Carrying persons br property for compensation or hire; and/or (2) Carrying persons not essential to the purpose of the flight. - ' . . . . C ...... n o This airworthiness certificate authorizes the flight speCifted on the reverse side for the purpose shown in Block A. .ii—i This airworthiness certificate certif les that. es of the date of Issuance, the aircraft towhich 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 Es provided by Annex 8 to the Convention On International Civil Aviation. No person may operate the aircraft described on the reverse side: (1) except in accordance with the applicable FAR and in accordance with conditions and limitations which may be prescribed by the Administrator es part of this. certificate (2) over any foreign country without the special permission of that country. 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. 4•11 1. EFTA00277881

. Form Approved 0 M R. No. 2120-0016 g tri ti set • • a - 0 . - APPLICATION FOR US Deponmere AIRWORTHINESS .- at Ihrepcnohon -i Fedora kakilion CERTIFICATE • Admisercassin - .. J INSTRUCTIONS — Pnnt or type. Do not write in shaded areas: these are for FAA • on cmly. Submit original onty to an authorized FAA Representative If additional - SPaCetarteuired, use an attachment. For special flight permits complete Sect. 0ns • 13 end VI or VII O applicable. I. AIRCRAFT DESCRIPTION I.REGISTRATION MARX iL) SV S e < ZAIRORAFT GuiLoeyrs NAME WON . . CSO Et.)06 }AIRCRAFT mom DESIWiATiON b..W4!' s.:. " — • 727— )00 I. AIRCRAFT SERIAL NO. . i. 0 / 15 Et. ENGINE BUILDERS NAME Wakes Pee be.) - &ENGINE NODEL DESIGNATI , Ji ll 8M ) In' "sk 219 •-.:;":.. .:. ---- . 1. NUMBER OF ENGINES CPROPEU.ER ISUIL7A Ale MOW A PROPELLER MODEL ons GNATION. 10. AIRCRAFT IS rCoock it •orhcicv, ok IMPORT II. CERTIFICATION REQUESTED • ..... APPUCATION IS HEREBY MADE FOR: (Crum solikeeDrit items/ - A :I: STANDARD AIRWORTHINESS CERTIFICATE 'Masco re category(' 'NORMAL' I UT1UTY I 'ACROBATIC' 'TRANSPORT GLIDER i8At.i.00t4 8 `..P Y. SPECIAL AIRWORTHINESS CERTIFICATE (Check stonsonett MIM) LIMITED • L i • it; cuss i • • . PROVISIONAL /inmate clan) . at. III . • z••• AGRICULTURE AND PEST CONTROL '::: AERIAL SURVEYING -;,3. AERIAL ADVERTISING : 3 - RESTRICTED (Immure operations to De committed) ., . „ p66 FOREST (WSW ecoservamml 4: . .. PATROLLING .e WEATHER CONTROL y. tit i 'CARRIAGE OF CARGO . . ilf- OTHER (Speedy; j • 9 RESEARCH AND DEVELOPMENT ...' B. AMATEUR BUILT .•- 3 EXHIBITION • EXPERIMENTAL ihNOVIIO operation/ s i .:• 4o PO cOnductodi • ‘44I RACING 40 . CREW TRAINING X MKT SURVEY ' 1 t .7. " 4 tit IA TO SHOW COMPLIANCE WITH FAR e FERRY PLIGHTFOR REPAIRS. ALTERATIONS. MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT ilndcalo '2 EVACUATE FROM AREA OF IMPENDING DANGER °pew/on to be conducted illy.: Sedan VI VII as ''.:3 OPERATION IN CXCESS OF MAXIMUM CERTIFICATED TAKE-OFF WEIGHT cc-nplele or applicable on reverie idea B DELIVERING OR EXPORT .61 I PRODUCTION FLIGHT TESTING • .74.. CUSTOMER DEMONSTRATION FLIGHTS C PS. I MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE liestnaml Oraranner end -Steislare or -Lveded. 'as applicable.) ' g .t 9 14* 5 0 A. REGISTERED OWNER (As shown on certificate of welsh npistrstion) J..; IF DEALER. CHECK HERE ----w- I "'t NAME 1,g 1. NOttilAuti261 1401-0tOtr t 0-400 0 rp iTi On . ADDRESS Foil tecs-Ries 41 .64Pti MT &.k Pi-4?-4 1$ WM kh1,11419 ;tent letAti IAA 1 M6-7,P1 Wfrigintha irfff03 B. AIRCRAFT CERTIFICATION BASIS (Cheek applicable blacks ana comps. awns as indicated) t AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE Diri A sliEET (Give Na end Revision Na) . : . AIRWORTHINESS DIRECTIVES latest AO No.) (Chest 4 all amicable AOS merged WWI and give AIRCRAFT LISTING (Give aga number(sc SUPPLEMENTAL TYPE CERTIFICATE lbw rhimber OleeCh STC income/area. • C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS . / CHECK IF RECORDS IN COMPLIANCE WITH FAR 01.173 . TOTAL AIRFRAME HOURS • . " PI' .,gs-1, 2.: 3, A ..8j Et d PERIor MEN tenn TALadOINLY (E/ 76::::„8„ ,sil.o.,..ince,„„cesid.coe D. Administration &moiety CERTIFICATION — I hereby cattily that I in accordance with Section 50 and eligible for the einvorthinna madam am Me registered owner far his agent) Of the @naafi daunted above: MN the sworn of the Federal Mutton ANY IEEE. rdappliCableFriferst Aviation Regurabons, and reauested. % . . ' • . . - - • •• . • . tiered with the Federal Aviation mat eve we has been inane and es DATE•OF APPLVATI0N / 5/ / 9c• .:.- NAME AND TITLE/Penaor tysiN . er-1 . tati4•41-7 ._, - eat..O 7— , IV. INSPECTION AGENCY VERIFICATION A THE ESCRII3ED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Complete Ma when only it FAR AIRCRAFT 21. WWI Aghast .{.1, trot FAR PART 121 OR 121 CERTIFICATE HOLDER (Om Certificate No.) • % CERTIFICATED MECHANIC (One. Certificate Nat • . CERTIFICATED REPAIR 5 ANON (Give Certificate Nal rit AIRCRAFT MANUFACTURER (Give nem or Wm) DATE TITLE SIGNATURE s .-"IeN Nie - • aw.. cs (Check ALL epplecebte Mocks In items A endial ' THE CERTIFICATE REOUESTE9 ms A. I lend that me aim reh described In Section I or VII meets (immanent* for. .7.>1 AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CEMIFICATE a. Inspection tor a special MgM permit under Section VII FM INSPECTOR, FAA DESIGNEE i.8. was conducted by: CERTIFICATE HOLDER UNDER: FAR 6S , ' FAR 121. 127 a1351 1 FAR tits 47 2. i g i ri DATE Q5-6/-90 DISTRICT OFFICE SEA-Mtbc, • . 4$ DESIGNEE'S SIGNATURE AND NO. I- 1- Jr -4V. AA INSPECTORS SIGNATURE . • • . • mmeicias .. FAA Form 8130.6 (1243) SUPERSEDES PREVIOUS EDITION • •e z • I% e t-c='..- • 5'11•• /A' • ` - y,Y A•St • r-. - • • •r• ti . i. -a A EFTA00277882

一一：7 老汹一d 一： 一一L3．一一・．一一c EFTA00277883

VALSitikkaktliEtts_:. . 3014 .Westcheiter :Averiue Purchase's, N.Y. :10577 ..• (914)":694-3600 I. May 1, 1990 FAA, `ANM"1085 . 7300 Perimeter Rd. Seattle, WA 98108 • :Dear Sir, '• Attadhed is FAA form 8130-6, Application for Airworitaneths ...Certificate, for adding "Market Survey° to the authorized operations of our Experimental Airworthiness Certificate. The aircraft is a Boeing 727-100 which has been retrofitted with P & W JT8D-219 engines on 'the POD positions and -7B in the center position. We have flown the aircraft approximately 17 hours under the presently issued Experimental Certificate.S We are requesting "Market Survey" so that we may take a TV reporter and cameraman from Paine Field, Everett, Washington to Grant County Airport, Moses Lake, Washington on 1 May 1990 for demonstration of the- Stage IIV Noise Characteristics:.. ' .The duratiOn of the "Market •Survey" portidn of this .Experimental Certificate :will be only. :for `the. one, flight' from Paine Field to Grant County Airport. The: certificate will then revert to "Show Compliance with FAR's" 'until expiration of the certificate on. ,1 August. 1990. • -ze EFTA00277884

V rr-re,ar,PKv-, a•ALL.... • • - EFTA00277885

-FAA. AIRCRAFT REGISTRY CAMERA NO. N DATES 02- gi USDepartment ; • , of Transportation ' Federal Aviation Administration 4,At,r14.,Ac:t 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. 20115 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, and bounded on the West by no more than 200 miles from the Wedt Coast of the United States of America. 2. Base of operations is Palmdale/ Lancaster Airport, 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 "Lgtter of Authorization"\issued by an FAA-General Aviation or Air CaYrier'Operations Inspectbr. , 4. This aircraft shall not be flown unless it is maintained and operated in accordance with .Boeing-Low Ut'Jlization 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. • '7 - -st EFTA00277886

, Federal Aviation` Administration Manufacturing Inspection District Office - - • , • Experimental - Show Compliande with FAR's/Market Survey, Cont'd Page 2 of 2 7. The'Lcognizant FAA office Must'be.notified and their response '.received'in writing prior to flying'this aircraft after' • incorporating a major change as defined 'by:FAR 21.93. 8. This aircraft approved f(* .itair/night VFR/IFR only. • 9. No operations shall be'conduCtid. over densely populated areas :or in congested. airways excejytfOr.takeoffs and landings, and when - under ATC control. ' 10. No person may be carried in this‘aircrait during flight unless that person is .essential for the purpoie of the. flight while in the ' Show Compliance category. '11. Thib aircraft is prohibited from aerobatic flight;sthat 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 O' A Office. 12. If aircraft, engine 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. Aviation Sa -ty Inspector (Mfg) SEA-MIDO, ANM-10SS These limitations will expire on August 1, 1990. EFTA00277887

VALSAN PARTNERS . 3014 WeatcheAtet.Avenue Purchase,'Na.- -10577.. ' • . f914) 6943600' May 1, FAA,\ANM-74.08S.: , 7300 Perimeter:Rs:I.e.: .Seettlei:WAH 98108- AttaCiled is; FAA form 813076,. Application for -Airwerthibeea. Certificate for adding "Market .SurVey" .to the authorized operations of our Expeiimental Airuorthihess: Certifibate. -• - • - • . . . . The aircraft'is a Boeing 727-100...Whibhhas been retrofitted with P & W.JTBD-219 engines on the POD pOsitiOnS•And -78 in the center position. We have flown the aiicraft'AppiOximately 17 hoUrsunder the presently issued Experimental Certificate. We are requesting "Market Surveil." so that we may take a TV reporter and cameraman from Paine Fie10,-EverettOiashingioeto'Grant County Airport, Moses Lake, Washington .Oa 1 May 1990 forsaemenstration of the Stage Noise Characteristics..; s . . c _ The duration .of 'the "Market Survey" of Experimental Certificate will be only for the one, flight'fiom. Paine Field to Grant County Airport. The. certificate will'thenrevert to. "Show Compliance with FAR's" until expiration of the certificate. on: 1 August, 1990. . • Sincerely yours, EFTA00277888

诞 EFTA00277889

FAA. AIRCRAFT REGISTRY CAEERA ICO„ iN DATE: 2 — — et,..aar 51 - a .4 tia*. (FL st, t‘ 4:5'n YAtEstmmakibik 'DERARTmENToFTRANSPORTATION-FEDERALAVIAYIDNADMINISTRATiolt1 SPECIAL AIRWORTHINESS CERTIFICATE Any eh on, reProduction or misuse of this certificate ma /table by a fmc not exceeding S L000 or imprisonment o exceeding 3 years, or tinik THIS CER11FICATE MUST BE DI LA YED IN THE AIRCRAFTIN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS FAA FORM 0130-7 (7-70) USE PREVIOUS EDITION • `Y:epterr'r let ter . •• . - ' EFTA00277890

EFTA00277891

407 US.Departant of Transportation Federal Aviation Administration February 2, 1990 Manufacturing bispection District Office. 16501 SherinanWayi—Suite 200 Van Nuys, CA .91406 . . EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's 3-4 MAKE:'Boeing MODEL: 727-31 SERIAL NO. 20115 REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft mustbe operated in accordance with the following Iimitations: No. person may operate•this .aircraft for--other than-the purpose of Show Compliance With the FAR's to accomplish the tests outlined in the applicant's program letter dated February 2, 1990 detcribing 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, and bounded on the West by no more than 200 miles from the West Coast of the United States of America. 2. Base of operations is. Palmdale/Lancaster Airport, 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 --""166 -bboirentibitVme ss ss1"1:etter of Authorfiationft-issued'by an FAA category/class r tin , aircraft tYPe rating,.. have a flight instructor's General Aviation or Air Carrier Operations Inspector. ' 4. This aircraft shall not be flown unless it is maintained and operated in . accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. This aircraft shall contain the platards, markings, etc: required by FAR 91.31. 6. 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. . 7 This aircraft.approved.for day/fiight:VFR/IFR only. EFTA00277892

FAA, AIRCRAFT REGISTRT CAT:ERA NO. I DATE: 02. g ;,..;••• s , "Fedelll AViAtiott AdidiAittiatia Manufacturing Iiiipectitid Oistrii*Offitt-- Experimefital - Show CompliaNdi'With cdntsd Page 2 of 2 % 8. No operations shall be conducted over densely populated areas or in :congested-airways except for"takeofft and landings, and when under ATC control. 9. No person 'may be carried ,ip:thisaircraft dUring flight unless that person is essential for the purpose of the flight. 10. This aircraft is prohibited from aerobatic flight; that is, in_ 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. 11. If aircraft, engine or propeller operating limitations are exceeded, an apprdpriate entry will be-made in the historical records. 12. 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). bert Stagg R-48-AC-NM 'These limitations will expire on August 1, 1990. ect.,:gm te**"" r ...‘4!‘ '‘';'N"te.00.6frte4i0,44:'""--"- `: • EFTA00277893

FAA AiRCRAFT.REG1STEE CA? ELA WO. i. ,tr DATE: 2-21- 9 fd mow...—...a.,--... dir:ah. 0.••••••••••••.. •-• rt, • •- • • . 0 MAJOR REPAIR ALTERATION L I S I D e v o r t i n e m as scruDortaucc . (Airframe, Powerplant, Propeller, or Appliance) Pearce Aviation Acteriatishotion • • . . .... . . ' . • Form Approved OMB No. 2120-0020 For FAA Use On:y Office Identification ,S0- Fs a 0 --/sr INSTRUCTIONS: Print or type all entries. See FAO 43.9, FAR 43 Appendix 'land 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). I. Alrcraft Make • Boeing Model . B727-31 Serial No. • • • 20115 Nationality and Registration Mark N5 0 OLS - 2. Owner • 1. Name (As shown on registration certificate) .. •• • • VorthweS€ 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 N9. Repair Alteration AIRFRAME .... Os described in Item 1 above) • • •• X POWERPLANT • - ., . PROPELLER \ • • ----7N s • • • APPLIANCE Type • • .: . . .. . - ( -,._ Manufacturer • 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Page Avjet Corporation . 9809 Tradeport .13r4ye '. Orlando/a_ Florida 32827 . U.S. Certificated Mechanic OS4R425M • Foreign Certificated Mechanic A Certificated Repair Station _ Manufacturer D: I cert ifAhat the repair and/or alteration made to the un t(s) identified have been made in accordance with the requirements of Part furnished herein Is true and correct to the bested my know in item 43 of the U.S. 4 above and Federal Aviation deicribed on the Regulations reverse or attachments hereto and that the information . • • . e. Dal.) • . gnature of Aut Individual . .. .. 7. Approval for R urn To Service t, • Pursuant Administrator By • to the authority given persons specified below, the` nit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and Is APPROVED 0 REJECTED • • FAA Flt. Standards Inspector Manufacturer Inspection Authorization • Other (Specify) • • • FAA Designee x Repair Station Person Approved by•Tranapart Canada Ainvonhiness Group Date of Approval lit 6E,Pr. or Rejection 90 Certificate or Designation No. • : 0S4R425If. ' Signar—obailhorized iteAr8 Individual / .. d:41,,?! -.7n/L i.i . FAA corm 337 • etiaftZVotcesere.Lesz• scraslY -co;341-- . EFTA00277894

z 4Q • z -1.5t)c'er:k-t fr,4- t"\.- Jr ' ;G• . . - NOTICE Weight and balance& operating limitation changes stiell.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 • fit more space is required, attach additional Sheets. Identify with aircraft nationality and registration mark and date work completed.) B727-31 S/N 20115 1. -MODIFIED J:POWERPLANT-:-INSTALLATION :4).1-FACILITATE RE-ENGINE PRODUCTION. FOR AIRCRAFT HAVING REMOTE ENGINE OIL REFILL SYSTEM IN ACCORDANCE WITH' VA 71000, REV. .48:,...DRAWINGS PER DER'TH0MAS F. . tCUBRAN NM-a83, APPROVED BY-8110 DATED SEPTEMBER 4, 1990. PERFORMED AIRSTAIR INSTALLATION :IN ACCORDANCE WITH REPORT. 442 (STRUCTURAL SUBSTANTIATION. OF.EXTERNALDOUBLER AND .MISCELLANEOUS COMPONENTS FOR INSTALLATION OF: FORWARD AIRSTAIR) AND REPORT 444 (INSTALLATION INSTRUCTIONS, BOEING'727f00 FORWARD‘AIRSTAIRI AND 6 IN'ACCORDANCE WITH• 750-1-P002. DATED 94101990 BY D.E.R. BOYD SMITH S0-351. • PROVIDED WEIGHT AND.BALANCE UPDATE. 'EQUIPMENT -LIST UPDATED ACCORDINGLY.. ALL SYSTEMS OPS CHECKED AND DO INTERFERE WITH OTHER SYSTEMS. •ALLPERTINENTDETAILS OF. WORK. ACCOMPLISHED ARE ON FILE PAGE, AVITETCORPORAT;Pki UNDER WORK ORDERS'4706.AND 6778, DATEP://ri/sJT:Ani(07,. END ,, ,,„,,agic„„iggetroiralt.‘aantatrra` • EFTA00277895

EFTA00277896

Twvemqs7PapIlilvt%"=c- iTlA alECKAFT REGISTRY CA'r,ERA p0.7 N DATE: 12-21-90 • r r • • .;it••• • rat -1;1:jilt/Ilea 31;sammi,spdpeammisMINIa _-zdaRatagec.-- EFTA00277897

gicgorglict—Soscref&r.t.kirrs FAA AlRCF.AFT REGISTRY C.UtIF.A N DATE: 12-41-90 • •• ••=. - t:•4; ..40;rs.g. .AL • •:'44 '• ••• UNITED STATES Of AMERICA DEPARTMENT OF TRANSPORTATION—FEDERAL AVIATION ADMINISTRATION ' STANDARD AIRWORTHINESS CERTIFICATE NATIONALITY AND REGISTRATION MARKS N505C 2 MANUFACTURER AND MODEL BOEING 727-31 3 AiriCRAL7 SERIAL NUm0E0 20115 4 CATEGORY TRANSPORT 5 AUTHORITY AND BASIS FOR ISSUANCE • Trtsalmorthinefulcertilicela is issuedpursuanl toilleFederal Aviation Aci of 1958andcerfilles ai oftheMte of iisuance aircraft to which issued has been inspected and found to conlorm 10 the Ilse cenificale therefor lo be m cvochhon for salt operation, and has bean shown lo hysel the requer errant& of the applicable comnrenensive an detailed aimontimuss coot as provided by Annex a to the Convention ohIntematoonal Cml Aviation.excem as noted herein EaraptiOnt • NONE ' • ' B. TERMS ANO CONDITIONS LIMN* 5004r surrendered. suspended. revoked. or a termination date us otherwise etlabhiliel tw.the AdmatflatOr ibis alnvorthincee certificale is ellimint N long as Me maintenance preventative maintenance and nitenitiort air perlotn*d In IccordencewithPerts21.43.andfll ol Huffed**, Aviation Regulations. estop, ate find the aircraft •i registered itIll•ets• d Stets& DATE OF ISSUANCE 7/23/90 Any attenition.feprohuclion.tx CellibefratemaybeliontinITM nol exert 000.o implisd'imtolmilexerealmj 3 years. or boib. THIS CERTIFICATE MUST BE DISPLAYED IN THE_AIRCRAFT IN ACCORDANCE WITH APPLICABLE I-El:WAAL AVIATION REGULATIONS. FAA Form 8100-2' ore2) CPO ena•nt•4 usa of \hosso FAA REPRESENTATIVE % WING C. CHIA. ea% DESIGNATION NUMBER DAR-41-FS-NM • i.cm..4 O.:my boa - 8. ;frial: • -Nisi, lab • ••••• •••• Cfr• EFTA00277898

a•74.1 ..J1V-r•-_ -"Wiii'illr.7. , .cam, , :,r; FAA AIRCRAFT REGISTRY .CA4TRA R0. 7 N DATU ...c; s4op • • doittacaYom. P•46 .--•)4 • ear-t;s6--"aAl.:- WASEA.I.TAMILle••=iliaWEi.rfcq ',..!gt• • R. . tr•U•••_. vs' EFTA00277899

AA AIRCRAFT REGISTRY C RA NO. 7 N DATE: 8- 15- 90 r N a . ireg., • - 1.0” . . . 1 .it-- ....., • , * 1)10 ty • $,• t • • • .a.t."' vow Form Approved • . 0.M .8. No. 2120-0018 I , APPLICATION FOR I Ultieoccirned . AIRWORTHINESS • Federal ‘4311on CERTIFICATE mhastranon INSTAUC710NS -- PrInter typo. Do not wrlte in shaded areas; those are for FAA use only. Submti original only to an authorized FAA Representative. If additional Space's required, usean attachment. Forspeoial flight permits compleloSections II and VI 01.VII LIS 440floa,b11).; , I I. AIRCRAFT l DESCRIPTION ltREGUSTRADON MARK I1S05C 2.A1RCRAFT BUILDER'S NroCE (AEON Boeing AIRCRAFT MODEL SI NATtON \ ,J - D ‘ t\ - • •• to-;ti 727 -31 • - YR. WA 4, COOING 69 FAA / 3 ,gc70/0 • . 5. AIRCRAFT SERIAL NO. i 20115 5 & ENGINE f3UI L DER'S NAME mak; Pratt S Whitney - 7. ENGINE MODEL DESIGNATION - JT8D-,76 ,k5 3 ts'm 8. BER OF ENGINES 3 • . 9. PROPELLER BUILDER'S NAME (Make) 10. PROPELLER MODEL DESIGNATION 11. AIRCRAFT IS (Check it appttc•bio) 1 IMPORT 0 a F iB = -e, APPUCAT1ON IS HEREBY MADE FOR: (Choc applicatninimu A I STANDARD AIRWORTHINESS CERTIFICATE (/rtcocatit cerog,try) I 'NORMAL I 'UTILITY 1 'ACROBATIC' 'TRANSPORT 1 'GLIDER I I BALLOON El SPECIAL AIRWORTHINESS CERTIFICATE (Check appropriate ilinu) e `3 .. LIMITED 1 CLASS I .. cl PROVISIONAL (Indicate attl) 2 CLASS II 1 ' AGRICULTURE AND PEST CONTROL 2 AERIAL SURVEYING 3 AERIAL ADVERTISING 1 RESTRICTED ffnetteste opershonEt)I0 be conducted) 8 FOREST (WrAlloto consarvenan) I ,, pATROLLING a WEATHER CONTROL --, I CARRIAGE OF CARGO 0 OTHER (Specify) 4/ . RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT '8 EXHIBITION 4 nd EXPERIMENTAL (Indicate operetiOn(a) to a conducted) 4 RACING I CREW TRAINING MKT. SURVEY l X ei X TO SHOW COMPLIANCE WITH FAR • 7 FERRY FLIGHT FOR REPAIRS, ALTERATIONS, MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT Warta 2 EVACUATE FROM AREA OF IMPENDING DANGER 3 operation to be Conducted. then complete Section VI or VII as I OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKE-OFF WEIGHT a applicable on remise style) . 4 DELIVERING OR EXPORT I I1 I PRODUCTION FLIGHT TESTING - • • a CUSTOMER DEMONSTRATION FLIGHTS c I a♦ MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE 'Restricted °potation" and "Standard' or -Limtled.- as applicable) z 0 p 5 a €€ ii : • i, Iii S it A. REGISTERED OWNER (As shown on ceittficale of aircraft registration) IF DEALER, CHECK HERE 1 NAME • Northwest Holding Corporation ADDRESS Foulkstone Plaza, Suite 102 1409 Foulk Road, P.O. Box 7138, Wilmington,DE B. AIRCRAFT CERTIFICATION BASIS (Check applicable blocks and complete darns as indicated) 1.9B03 r AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE DATA SHEET (One Na end Revision No.) A3WE X AIRWORTHINESS DIRECTIVES (Check it all Appic ego AD's con) plied watt and pare West AD No.) 90-02-19 AIRCRAFT LISTING (Ciro page numbs:fit) Rev, 18 - Dated February 20, 1987 SUPPLEMENTAL TYPE CERTIFICATE (Cut number of each SIC Incorporated) C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS X CHECK IF RECORDS IN COMPLIANCE WITH . FAR 97175 TOTAL AIRFRAME HOURS . 29820 Hours • - a EXPERIMENTAL ONLY (Enter hours flown salts leaf cart tficels issued Oe renewed) -0- D. = CERTIFICATION — I hereby certIty tttat I Administration In eccord•nce with Section 50 orrery:011y and eIrgitale for the mrworthineas certificate em the /agitated owner (or his agent) of the aircraft of tr. Federal Aviation AcI of 1958. end applicable reatenfed• deacnbed above; that the aircraft Firtkra/ Avila:an RegutsIon : and is registered with the Federal Artaticm that the aircraft has been inspected and rs DATE OF APPlICAT ION - February 2. 1990 n oTIT I or I f Valsan .Program R.A. Braulik naineerina & Manager SIGNATURE Z g t t AP 1 g et c V A. THE AIRCRAFT DESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Compite• tan seefron only-if FAR 21. BT(d) applies) e I FAR PART 121 OR 127 CERTIFICATE Carolicat• No.) HOLDER (One ' S I CERTIFICATED Certificate Na) MECHANIC (Cl.. . _ - CERTIFICATED REPAIR STATION (Give COf I, lc a la No.) -.2 ..06 .4 _ AIRCRAFT MANUFACTURER (Dire nem* of firm) J DATE e TITLE SIGNATURE t . F p 0Z CR 3 3 >.1:4 SC N . (Check ALL applicable blocks in items A and Ell THE CERTIFICATE REQUESTED J A. I hnd that the anctalt des/tithed in Section I or VII Ibsen requirements for. 4 AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE B. Inspection tor a apecsal WI privet under SWIM WI ' • FAA INSPECTOR FAA DESIGNEE was conducted by: .. . • -..1. -- CERTIFICATE HOLDER UNDER. _ FAR 65 i _ FAR 121. 127 or 1-...y r frAR 145 DATE 9A-- %pa DISTRICT OFFICE • ‘,(01-0‘ , Nays not goo. . • • 7> 2.• - , ATUR N NO. D --Ape -sr --.9 . ..:::- .....- A., ni , 1 AA INSPECTORS SIGNATURE FAA Form 8130-6 (6.06) SUPERSEDES PREVIOUS EDITION • :V• ...... • "f - " • . • EFTA00277900

E. THE FOLLOWING RESTRICTIONS ARE CONSIDERED NECESSARY FOR saFE OPEFIATIONJUI.datteChInent UneawFwri • . • P. agamealsOpa- eats demay mu i am In reCettered Ores iahsa9.nU Oi Me *wall described ton. Mai the airalin is registered with the Federal Aviation Adminsbetion in itCardenitlitvilh Elect100 al 00 the Feeterel Aviation Act of lelle, end oppaceete Federal Aviation Regulations. end Mat the Wenn has been inspected and is airworthy for the Mod tesic W.= EFTA00277901

,. UNITED STATES OF AMERICA •• .. DEPARTMENT OF TRANSPORTATION - FEDERAL AVIATION ADMINISTR . ATiOt,.}- i, SPECIAL AIRWORTHINESS CERTIFICATE A BATEGORY/DESIGNATIONri ,A-Zrel - If6t denr PURPOSE ijalAret, . B. • MANU- FACTUFIER NAME ADDRESS ifh• 'C I" FLIGHT . ... FPON1 Atg _7 $: • To 4,4 arta D NmAcc isof SERIAL NO. Z e.tr . MODEL "77:-.0„,/,' BUILDER E . DATE OF ISSUANCESOffrar t /4'99 EXPIRY zehery/f/InetV• A PART OF THIS CERTIFICATE OPERATI LIMITATIONS DATEDS04,09/475WRE WO OF r e ard ed i FAA ATM — DESIGNATION OR OFFICE NO. A r 7 -4 Cbg0 • - — ' . _ .. Any alteration. repmduction or me 1 this carlificaer may be punishable by a line not exceeding 51.000 or Imprisonment not exceeding 3 yearn, or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA FORIIM30.7 me . CPC arl/FligF Ainr EFTA00277902

AA AIRCRAFT REGISTRY RA NO. 1 N DATE: 8- 15- 90 A ^ This airworthiness cenificale is issued under (he authority Wipe Federal Aviation Act of 195‘. and the Federal Aviation Regulations (FAR). • • .. B . . This airworthiness certifiCate authorizes the manufacttiret named on the reverse side to conduct production flight tests. and only production flight tests, of aircraft registered in his narne.,Wo person may conduct production flight tests under this, cestfficpte: (1) Carrying' persOns or prqperty for compensation or hire: and/or (2) Carrying persons not essential to the pitrpose of theilight. . .•• , .• C c' This'aInvorthiness certificate authorizes the flight Specified on the reverssside for the purpose shown in Block A. .. • o . . . . , . . . . ,.. .. , . This airworthiness certificate certifies that, as of the date of issuanCe, the aircraft to which 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 op provided by Annex 8 to the Convention On International Civil Aviation. NO Person may operate .thaaircraft described on the reverse side: (1) except in accordance with the applicable FAR and in accordance with conditions and limitations which may be preacribed by the Administrator as part of this certificate:.(2) over any foreign country without the special permission of that country. . - r . . . . . . . . .. • - . c F • . . . • • . Unless sooner surrendered. suspended. or revoked. this ainvorthiness certificate is effective for the duration and tinder the conditions prescribed in FAR Part 21. Section 21:181 or 21217. ... . • • - EFTA00277903

1/ UNITED STATES OF AMERICA DEPARTMENT. OF TRANSPORTATION -FEDERAL AVIATION ADMINISTRATION • • STANDARD AIRWORT I ESS CERTIFICATE • • NATKMALITT AND REGISTRATION MARKS 2. MANUFACTURER AN . NSOSC , Boeing . • ; S. AUTNORITX AND BASIS FOR ISSUA I This airworthiness certificate i s urwont • dote of issuance, the aircraft h issued 1 'therefor, to be in condition 1dfe, opera 4 • cornprawnsive and detailed. f iwo /miss i Aviation, except os noted n Exceptions: F. TERMS AND CIADITIONS Unless soon*, sumndirredersu this airworthiness artifice performed in accordance w aircraft is registered In I nil ri 1 DATE OF ISSUANCE FAA REPR IV Exchange 06 oltied,\61‘ long os and 91 of AIRCRAFT SERIAL MOOT 5 Transport 1 and certifies that, as of the t • nform to the type certificate he s ;cements of the applicable • ntion on Internalionol Civil • is net toblished by the Administrator, t. f pints:mance, and alterations or. I *lions, as appropriate, and the DESIGNATION NUMBER Any alatatio reproduction, or misuse of certif.( o ;skiable by a fine no exceeding $1,000, or :tn. prisonme of exceeding 3 years. or both. IS CE TE MUST SE DISPLAYED IN THE AIRCRAFT IN ACCORD. ANCE N APPLICABLE FEDERAL AVIATIO REGULA S. FAA Form 8100-2 (7-6n . • v FORMERLY FAA FORM 5352 „ , • . . —tr. et EFTA00277904

" > > > ＂ 脚 ＾ 州 ＞ 哟 阃 蝉 蝉 。 审 川 帅 阀 6 ' ' ” 是 。 ’ 鸿 ＞ ～ ° ＞ 闩 忡 ＂ 啪 l 料 动 t 漶 EFTA00277905

UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION - FEDERAL AVIATIOArADMINISTR.,TION SPECIAL AIRWORTHINESS CERTIFICATE A CATEGORY/DESIGNATION V rguiTAL PURPOSE TO SHOW CON CE watt, . Roes B MANU- FACTUR ER NAME N •'4:4' 65", ADDRESS _, /-' C FLIGHT 13Y n FROM "-...y \ TO 1 ..6- ttli N- 5456 I Y. l'S ER* 0. 20115 IRJ I L O E R Boeing c t i MODE 727- 1 DATE OF ISSUANCE Fe -t, 1 E 8/01/90" E OP IN M •TION cy 2 PART OF THIS CERT! F ICATE St ae r0 AA %- ORATION OR OFFICE NO. - it • • ' .- • . B RT OAR-48-AC-M . Any ohm on, rtproclliCtIOD or misuse of this artificats way bo punishable by a fine not tzenedina S1,000 or imprisnntnent not ezecerfing 3 yens, or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE writ APPLICABLE FEDERAL AVIATION REGULATIONS. • .. . FAA PORM 6130-7 l7-7P) USE PREVIOUS EDITION SEE REVERSE UDE . 'zierta." EFTA00277906

A - — This airworthiness certificate is issued under the authority of the Federal Aviation'Am of 1958 and the Federal Aviation Regulations (FAR). B , - . This airworthiness certificate authorizes the manufacturer named on the reverse side to con- ' duct production flight tests, and only production flight tests, of aircraft registered in his name. No person may conduct production flight tests under this certificate: (I) Carrying per- sons or property for compensation or hire; and/or (2) Carrying persons not essential to the purpose of the flight. C "' This airworthiness certificate authorizes the flight specified on the reverse aide for the pm- pose shown in Block A. , air- ' • ,. ' This airworthiness certificate certif161 that, as of the date of issuance, the aircraft to which' 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 worthiness code as provided by Annex B to the Convention On International Civil Aviation. No person may operate the aircraft described on the reverse side: (1) except in accordance with the applicable FAR and in accordance with conditions and limitations which may be prescribed -by the Administrator as part of this certificate; (2) over any foreign country with- out the special permission of that country. 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 . 21.217. +t fo EFTA00277907

1.• A -s - ••••••• • • T• • p. USDepairreor of Transportation Federal Aviation Aderdnismation February,2, 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's MAKE: Boeing MODEL: 727-31 SERIAL NO. 20115 REG. NO. N505C - THESE-`OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT rw Manufacturing Inspection District Office. 16501 Sherman Way, Suite 200 Van Nuys, CA. 91406 This aircraft must be operated in accordance with the following limitations: • 1. too person may operate this-aircraft for other.than-the purpose of Show Compliance with the FAR's to accomplish the tests outlined in the ' applicant's program—letter dated%February.2, 1990 describing compliance with FAR 21.193(d). Aldditionally, thit aircraft-shall be operated in accordance with applidable air-traffic and general operating rules of fAR 91, and all .additional liMitations herein prescribed under the provisions of FAR 91.42(4). . 2. -All flights. shall.be conducted within the geographical areas \ • described as follows:. 1. Western Mnited States of America bounded on the East by the Mississippi Riier, on the North by the U.S.A./Canadianborder, on the South. by the U.S.A./Mexi,co border, and bounded on the West . by no more than 200 mileS. froM the West Coast of the United States of America. • 2. . Base Of operations is Palmdalettancaster Airport, Palmdale, 'California and secondary base of operation to be.Moses Lake Airport, Moses Lake,.Washington. f ' 3. The pilOt-in7command of"afrdraft must, as applicable, hold an appropriate category/class rating: have an aircraft type rating, have a flight instructor's. — log book-endorse:lent. of"possesi a "Letter of Authorizatton"-lssued by an -FAA • . General Aviation'or Air Carrier Operations Itspector. 'A. This aircraft shall not be flown Unless it is maintained and operated in accordance with"BOeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. -This aircraft shall contain the platards., markings, etc: required by .FAR 91.31. • 6. The cognizant FAA office must be notified and their responge received in writing prior.to flying this aircraft after incorporating a major change as defined by FAR 21.93:. 7. , This aircraft approved for day/light .VFR/IFR -":1" rv$1777= "T-IlenialrgitykraMr-rce-- • ?-4 rf EFTA00277908

Federal Aviation Aftinistration Manufacturing Inspection District OffiCa , • ! - .:. • - Experimental -Shell Compliance.With FAN'S, Page 2 of 2 8. • No operations shall be conducted over densely:OnOulated-ardo or in, 'congested airways except for takeoffs and1andings, and When,Under.ATC.O0tre!. . ••• . ',No persOri.may be carried in this aircraft during flight unlets that -person is essential for-the purpose of the flight. 10. This aircraft is prohibited from aerobetic flight; that is, an. intentional maneuver` involving an.abrupt -change in the'ait.craft's attitude, an' abnormal attitude or abnormal acceleration not necessary for:normal flight unless approved.by the cognizant FAA office. - . . . 11. .If-aircraft, engine or propeller operating limititions are-exceeded, • an appropriate entry. will be made, in the historical records: 12. After the'aircraft hasImen 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). T6eieilimitati0nS:*11.1 expire on August 1, 1990. EFTA00277909

AnclAPT NEOISTAV CAMBIA NO. 1 N DATE: 8- 15- 90 VALSAN• PARTNERS 3010 Westchester Avenue. Purchase. New %TX 10577 .* • (914) 694.3600 Telex: 825379 VALSAN OF Fax: (914) 694.6062 ADelawareLtavtedRinnemhip Febfbify 1990 Marketing Office: 99 Washington Street. Norwalk, CT 06854 (M3)866-6051 • • Telex: 6714726 DALAV UW Fax: (203) 855-0362 Product Support Office: 3605 Long Beach Blvd, #205 Long Beach, CA 90807 Tel: (213) 424-2145 Fax: (213) 595-0920 Mrt Bud Martell, Manager • . . Federal Aviation Administration Manufacturing Inspection District Office.• In reply . .16501 Sherman Way, Suite 200 • refer to Van NuyS, CA 91406 * . 001020290 .Subject: Application fortxperiMental Airworthiness Certificate • (To'Show Compliance. withFA,Ri) .- • • Gentlemin: This letter is toinfotii\You.thai- Valsan intends to operate Boeing • . . 727-31 ,. Registration N505C, Serial #20115 owned by Northwest_ Holding COrporation,Foulkstohe Plaza, Suite 102, 1409 Foulk Road, P.O. Box 7138, Wiliiiington,Delaware 19803 in an experimental. flight test prograM. The flight test program is in support of the Valsan JT8D-219 Re-Engining:PrOgram TIA NM-100S-1320. / Terms and conditions of the. Experimental Airworthiness Certificate are as follows: •• • • Valid for six (6) months fromLeffeCtive date of the . certificate. 2. Geographic area :is the, Western United States of AMerica. 3. Operation of. aircraft'will be in. accordance with alt. , applicable F:AjWs and:F.A:A. 8130-6 (attached).. Aircraft to'be maintained in accordance with Federal Aviation RegUlatiOns Part 91.169(f)(4), a current inspectiOn program recommended by the. manufacturer (Boeing Low Utilization Maintenance Program). R.A. Broulik Valsan Program/Engineering Manager C/O - Rockwell International 2825'East Avenue P Palmdale, CA 93550 Attachment RAB:lg t•-•••**0.,.. . • . EFTA00277910

烤 暮 · 儿 黧 h 亡 m EFTA00277911

US .DEPAPTAIDIT a TIVIONVOITIAT1ON - .. ..---,• ..sai ' FEDERALAVIATION ROINOSTRATION Sadsaltriiii No. 04-11060.1 . J . 4 ' atiumt WHIR AND ALTERATION tPOD FAA WE ONLY i ., OFFICE ,IDENTIFICAT1ON (Airframe, Pewerplent, Propeller, or Apptione0) '101F-PHX-FSDO s INSTRUCTIONS: Print or type Ill entries. . See FAR 43.9. F4/1 43 Appendix 8, sod AC 43.9-1 (or subsequent revision thels..1) for instructions and disposition of this form. - ... ..•- • AWE I MOOR - • • BOEING • I Z.21.7.31 I. AnKilAn Sing NO. - • 'NATIONALITY AND REGISTRATION MARK . • . .4 i 0115 i N505C • \ NAN& (As shown on nigistnation mi i rtificars) I ADDRESS (As shown.on mpildration ionOcoto( • 7. OWNEI • . FB TRANSPORT INC. 1 100 PINE ST 2.1 FLOOR I P RUNT . c i2 SAN FRANCISCO. CA 94121. 1 MR FAA USE Min • • , . , . ... • • . - . ... - - . . .. . , • . ... I. UNIT IDENTIFICATION S. net , • 1 -. . . onto L ...----- . -. Ulna NO. " SPAS *me- Anon • AIIIPRAME . IIMNIOMONOANISOMMIN (As thootni a slim I oboe)me teen . . POirrEltPtAte - . . MOMS • • • : t • - . APPLIANCE roe . o •. mAsanakras ; • A. CINFOIMITY STATEMENT A. AGENCY'S NAME AND ADDRESS . R. KIND Of AGENCY ' , C. CERTIFICATE NO. • • vs. Ceetiticatur Pi1Cooksic • . . DYNAIR TECH OF ARIZONA. INC: .3737 E. BONANZA WAY ' -. p is rer.t.rO4cominweci micmanic oCeenrICATID RIM! Inaptis • CRS A07-36 -AIRFRAME.IV ' PHOENIX. ARIZONA -. 85034't .. • satiuMCWItt D. I certify that the repair and/or alteration made to ' • inachtnents•heritobave been made in accardanie. with and that the information furniihed Stein is true and the uriiiIst identified in item .4 above and described on the reverie or the requirements of Pan 43 of the U.S. Federal Aviation Regulation! correct to the best of my knowledge. DATE " - • , ' AUGUST 10 1989 SIGNATURE OF AUTHORIZED INDIVIDUAL' . ' : . • • I . KENNETH ROWBOTHAM—Wernenta.a 4AP44 ,."-- 7. APPROVAL FOR INTIM TO SERVICE - -A' Pursuant to‘rba authority peen persons specified below, the unit identified in item 4 ',rasa:edin the manner prescribed, by she Administrator of the Pt Aviation Administration and is @APPROVED O RE) • It • 'AA Pit. suitopuits aaaWACNINI . . OTHER aativ) IMPICTI0NSONOIWATION . IAA Otteill XXX illia. SUMO.. CAHN:KAN OrMITOUNT - Or NAMPO., worecrot v.Xr DOI OP AMOVAt a RIIICTION . AUGUST 10. 1989 OR =ON NO . CRS 407-36 SIGNATURE Of WM D I DANIEL WEAR , . . . (1320) EFTA00277912

'F i.At8cRATT ItniS/RY CAMtKA NO. / 41 DATE: 8 • NOTICE iliWeight and balance_or operating limitation changes shall be entered-in the appropriate aircraft record. An reiteration. mitst: 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 witIleircraft nationality and registration mark and date work completed.) 1. FABRICATED S INSTALLED REPAIR ANGLE ON LOWER EDGE OF FUSELAGE SKIN FOR NO. 2 ENGINE SIDE COWL AT FIREWALL BULKHEAD 'APPROXIMATELY FS 1455 PER SRM 5.1-40-4.. 2. REWIRED 'CRACK AT RH HORIZONTAL STABILIZER LEADING EDGE APPROXIMATELY STA 78.3- 88.3q PER SRM*55-10-3. 3. . REMOVED CORROSION. CUT OUT BULGED AREA IN EXTERIOR FUSELAGE SKIN, INSTALLED DOUBLER APPROXIMATELY FS 1157 AT STRINGER 27R PER SRO 53=30-3. : 4. REPAIRED FUSELAGE' SKIN CORROSION. DAMAGE BS -1166 - 1174 AT STRINGER 27L IN. ACCORDANCE WITH BOEING REPAIR MESSAGE NO. BPI423200D. it U.S. GOVSINSINIVIT PRINTING OCCICE: ISS6-689-121/43146 osspAltia-wft" EFTA00277913

,____ ,,,,_ ill U.S DEPARDAINT Of TRANSPORTATION • . ,. •. FEDERAL AVIATION ADMINISTRATION RA Fine App. ed ,Bage t Pinta. N.. 04-Ito60.: MAJOR REPAIR AND ALTERATION -- -• 4 - . . (Airframe, Peworplant, Propellor, or Appliance+ VNYF. SD; OFFIcrF07R Et; fictictalltEop4ONLY 00/7 INSTRUCTIONS: Print or typsell entries. S.. FAR 43.,. F4R 43 Appendia D. end AC 43.9-I lot subsequent revision thereon for instructions sad disposition of this form. 1. AllCitArf•••• MAKE • . .REOEIVED.FAA !mote , - EING ' • "1 ' • •• 727-100 SERIAL Fib! rAy 0. • 1. 1990 'NATIONALITY AND REGISTRATIDN MARK I , . N505C , . 20115. 2.CIVINEI, . NAME Os shown on registrstion tortifi.cetiamv Fq..)0 ADDRESS (As shown qn reoistrotion cerriScorto) LIMITED INCORPORATED - • • -- ""- '7 -- - 4387 International G'ateway - 'Col umbus > Ohio : 43219 • • . . • 1. fOR fAA USE ONLY . , • • • '•• . • • • . -.• , . ...... ...._ .... .. . .. ... ..-. .. ._ .- • .,. . • . . . . ; ... , : • ., . . • - , .... . 4. IT IDENTIFICATION S. TYPE- Watt Mont • f • • ' . Melia NO. ' • IIIIPMII Anti- *Now AIRFRAME . .. . _ . • • _ . esetweteneeniennotoe (As thoscreed m Ihom ) obovoineeenbaseenreevraseem X • tantrum • . . , . - . . .. . . . . . . . . ' • . . X PROPELLER . . .. . . . , ' • . APPLIANCE ern i • • • •• • • r • . sensusecuu a . . . . • • . • • • . • • 4. CSINFORIIITY STATEMENT • ekr, A. AGENCY'S NAME AND ADDRESS S. KIND Of AGENCY • C. CERTIFICATE NO. North American Aircrat' - . -- - -- . •••--- Y.N. tannest** setetiaisse flOt8WepSlAniant Rockwell International Corporation . foam*. cestmcarto macmAwic Class 3 2825 E. Avenue P . . X "CIPIPICAIT0 NMI' STATION. . • Y " • . NXAR688K Palmdale, Ca.. . 93550 . auireRIACTRATO . . .: . O. I certify that threepall sad/or -alteratitia-made to the unit(*) identified in item attachments hereto Inve'been made in accordance with the requirements of Part and that the information furnished berein is true and cornet to the best of my 4 above on described on the reverse or 43 of the U eral Aviation Regulation,', knowledge. DATE . • • SIGNATURE. OF AUTHORIZE nigli ti ot7 tj . /0 9e) I .D.A. Perazzo INDIVID • . d ; 1. APPROVAL FOR RETURN TO.SERVIC - S r. . Peasant to the authority jinn venom speciied below. the tink4enti6ed In Ste 4 was Impened In the manner prescribed by • KW Administrator N St h& ide Aviation Administration and is • APPROVED REJEC , i • . I IIIA Ot b/IMG t. SY suanatites . ~toss saniatiwno•• Orrin ISesehi • • IAA WOWS i X Ilia PATCH • .cataagui Ro n . 'Of TRANSPORTmunatto . : AISM. • .• • • DATE OF APPROVAL OR RAJ! i f t 97 4.4 .199a CERTIPECATI 'OR SIONATUkt ? MTH ED INDIVIDUAL • ' DESIGNATION NO. • L. . a" • NXAR688K ' 4 .....4.-frics) EFTA00277914

鞲 － 口 EFTA00277915

.,„ NOTICE " Weight and ba lance or operating limitation changes shall be entered In the appropriate aircraft record. An . " altmition must be compatible with all previous alterations to assure continued conformity with the : • applicable al/worthiness requirements, 8... DESCRIPTION OF WORK ACCOMPLISHED Ott amore. space is required, attach additional sheets. Identity with aircraft nation4lity and registration mark and date wort con pletad,) A. Modiinalloqing Model 727-100 , Seiial Number 20115, in accordance with supple- ' mental' type certificate SA4363NM, amended•September 1, 1989 "as follows: 1. Valsan-Boeing127-200.Re-engining Document VA000001, Revision F, dated January 2i. The following dftwings and engineering orders (al's) are in addition to the above document: - • NOTE: - °VA" denotes Valsan Deaiting. a: `'Chapter 24 ELECTRICAL POWER • A240000 A Electrical .System Instl. - Strut E.O.: 003A,'101 VA240007 E -, Panel-Load Control Center Modification. E.O.: 003A, 004, 005, 006 b.. Chaster 28 FUEL SYSTEM INSTALLATION. T- , STRU • . . VA280001 B Tube, Assy - Fuel Strut Feed Thru E.O.: '100 Chapter 48, MISC A481100 .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.O.: 106, 114A, 114, 116 Intercostal Assy, - BSTA 1223 to BSTA 1243 W/L244.39 E.O: 106 Intercostal Assy, - BSTA 1223 to BSTA 1243 W/L234.06 E.0: 105 Chapter.53 FUSELAGESTRUCTURE A530001 B Ballast Weight Instillaticin E.0: 100, 102 VA530003 C Ballast geight, Support Structure Assy. E.O.: 002,100 — VA530004 NC Ballast Weight Instl. STA 312 - 360,E.O.: 002, 100 Chapter 54 NACELLES & PYLONS - ,VA543000 C Main Strut Assy 2, & 5) E.O.:-003 VA543100 D Firewall Rib,.Side Engine LO:.36A,003A Chapter 71 POWER PLANT _ A710000 NC Power Plant Instl. - Engine Pod V727RE 002, 1058, • 109, 108, 001k 104A, 005A,.004, 110, 003, 111,1106A Chapter 73 ENGINE FUEL AND CONTROL- . . A732301. K .Approach Idle Solenoid Wiring Diagram E.0: 002(Rev . 002 (Rei. M), 003(Rev::M) VA732303 D Relay Inttl. Approach Idle Solenoid E.O.: 103, 003, 1008. • , VA732304 . D • Switch/IND Light Instl --Approach Idle E.O.: 002, . VA732310_ 'A Switch' Instl. --Nose Gear Position Approach Idles-E.O.: 103 VA732315 NC Relay-Inttlf Pilots Overhead Panel E.O.: 002; 101, Chapter 76 ENGINEIOTROl. ' • A760000 A .Eng)ne COntrols,Instl. - Strut-E.O.: 002A VA760014 A . Drum Instl. Eng. Controls E.O.:- 100, 101 VA760015 A . Bradkit Assy.:.- Pulley ESTA 100 E.O.: 105 EFTA00277916

EFTA00277917

DESCRIPTION OF WORK ACCOMPLISHED (Cf:iiitiPliel) • . Serial No. 201lt . Cha ter 77 ENGINE INDICATING * ! A771005 Indicator• Engine Pressure Ratio EPR, E.O.: 001 Chapter 78 ENGINE A780000 VA783010 E. 'VA783011 F VA783013 D • VA783017 J VA783(et VA784028:. • ' • A, VA781101:- EXHAUST Engine Strut controls Instr. E.O.: 002_ Flt Deck Indicator Instl. T/R-Sys. E.O.: 003,:004 Thrust Reverser System Wiring Diagram'E.0:: -002 (Rev. G) Support-Bracket Assy - .T/R Control Valve -R/S E.O.: 100 (Rev Placards 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 Deaetiiiation E:0 002 , - Chapter 91 CHARTS:. VA910002 A • Instl. 7.EleCtriCal Wite Harness 603,*4,-605, VA910008 : NC : Wire List V727RE E.O.:-00.1,.002, 003 • • ••: *New drawings added to: modification 127:SerVice:Bulletin 727-'53A0171, dated December 14, 1989... FUselage's., Station. 1182 Presture'Bulkhead,Weh: • Crackllepair.inCPreventiVe • Modification'. . • , . The aircraff.eiptY ueigtit.and center of gravity was .revised in accordance with Bbeing Weightand Balance Manual D6-21200.- . Weight and BalanCe Manual Supplement,'VA7CR279 ' is attitched • EFTA00277918

EFTA00277919

SCALE READING Left Outboard-Main 24402 Left Inboard Main 21865 Right Outboard Main 1 X23687 Right Inboard Main t -•4777%..14,4).% Left Nose Right Nose „4 :04T414,V.C .i4t ,4**-Kns. Subtotal (Nose) Items 4WW0AnAPDTVREA5K- part of Basic Weight but not Weighed AIRCRAFT. BASIC WEIGHT gsctvxivw?;antfpk Au' ti,j1m4 44. 111.221 = (MI) Distance tram the jig point to the main axis Centerline 520.1 1 • (M2) Distance -betweinthe• lettilose axle centerline and the jig point. eie.nl e (N3) Distance bitween•the right nose axle centerline and the jig point. 330.101 • (RI) Distance fres the referent. dates to the jig point of the aircraft. 950.121 a (A) Nein LOS Reaction' 311.371 = (I) Nose 'Axle liaction. :Ti litttaeVeRgirtiitid6;:%irtrisi • REMARKS 883253 176804 The aircraft was weighed in a level attitude and in an enclosed hanger. . .• 4k - 2. The wing panel jack' point was used for the aircraft jig point. 3. This is the summation of'the 3 weighings. - _- 4. Baseline Weight Results for Post Mod Flight Test, dated 4/10/RO. J EFTA00277920

•1 Y. rr_f', EFTA00277921

727 — 100:/ 200 Weighing Form Left Outboard Main Left Inboard Main Right Outboard Main Right Inboard'Main riffix• Left Nose Rightlifose Subtotal 89563757 part of Basic Weight Basic Weight but not Weighed 1 AIRCRAFT BASIC WEIGHT 4.4?.. • :ijki?-77-r= .,504 •`x i 1 . 96173 931.278139.33% tsrilfzt , CORRECTIONS „"tittiga, Items NOT weighed but night Basic Weight mEAsuREmEtrie 118.22) ..(.1) Distant, from thelig point to Vie gain axle eantenlin, 320.11 s (112) Distant* between the left-toss axle centerlinaand tha jig point. c (M3) Distinta.batenn the right noel axle centerline and tha jig point. s (R1) Distant, froa Lb, referants data to the jig point of the aircraft. 950. 121 s (A) Main 'Rile Reaction A s .R1041 311.371 (s) 'sits•'ail Reaction II a R1-(1124443)/2 The aircraft was weighed in a level attitude and in an enclosed hanger. • • 2. The wing panel jack point was used for the aircraft jig point. 3. This is weighing 1 of 3 .4=447Awan,1147' EFTA00277922

潜嗨置鲢薄鬈鑫坚： EFTA00277923

JAL AIRCRAFT REGISTRY CAMERA NO. 1 N DATE: 8 75- 90 .. .. • ....::•7; i 727 - 100 1_ 200 • : C. • .• .. ..r. . • -'"t;..II ' WeigIving.FOrm • -,: ' L *Alt.il ...fl. “;:ic._ .: . • •• Date 'Model .18eriail c Number Place Weighed' Technician Phone 4/18/90 727-100 10115 - N505C . •ALMDALE FOLEY (805)265-2151 REACTIONS ' ' . • SCALE READING . •'41.1 • " ‘.TARE . NET • - ARM it $ WEIGHT ... .. , ... ''• MOMENT . - • • *. :tot& 4 • xi 1.qt • • ••••• \ 1.••". • % ;;;;;.;.A.4.,*:::*;14., Left Outboard. Main- 24402 • t• !.. I.7;!et. . ..2..::gi.19Firei. Vt.; *.:' r 6 24408 >. - . .41 " . Left Inboard. Main. 21865 t. 2 21867 •:.:;;;2;.:444.4.!."211.11#•dia.,4;;I:f .t'it l4 1(tl':cliii: L. •:.'ner&E,4:40.4,Fer, .....ip.bv..1-....e,:•:•.•.:../Y41:11,A .47:3;4 ". is . .3•1 %'•.I 1"i . • ' • 4 ••••• -,..•: 8( 7 ...4.- ! !. 1Wi " rt:" .... :Sri .: • ' -‘ ' " I !!! 31 174. -- gyel;..‘ 17... Ca •:. , ..„;..f.t ,:......g:Ca Right Outboard Main 23689 4 23680 ::::-..44:k..t412: ...Q..: .:.....,•• .. Tr .•! 0. • ..bP .1) ... .h:il 'Cer ... %'.. .81 ••• .!'t 4.• u •/, 9 far 4.10, if f, .. 3 23384 ..4. • "ran.... ktype ,... .....;:;:oA.;:•.i:-. •...t..i,.5 Right Inboard:Main' 23381 r i 5-ef-,4s .4. 8 Tiv....,. - ...:....04! ;.:..:1.:44.%;.:. . n..f .......:.=:. ... 4 s.01.5 4 ..2 ' . . 4. so ...:0 12 C I.:nil" • ' .... ' 'C .175 ‘g`:r•••••••.:•:• '" 7 93344 A - 950.12 ' Subtotal (Mains) 93337 . . •• • r I 88688001 ee i o. • 2-: 7. ti 5 ik 'Men 4tPitir .:11 OA , . • Left Nose •'. . 1338 i;V:Z - na 1338 - -, t• . • . Right Nose - .- 1501 0 1501 --- ,, fairgiN9! .".1.1,z44/P .‘ I. - 4,1' •:. it •,,,, zi k2,F2 • v,..•-mts t... ..44.,KAcre. 1.-- . 4.:. . r: l'• Subtotal (Nose) 2839 1 e 0 .2839 us 311.37 A htili.5.04.ekl ie0 161 17 1 r rs.sranons•• .......•: .• r ti. ,t:if- 883979 “.... ' AL • ri Ze•;•• ... .iia"VV %at fier;":::! el :, TOTAL 96176 id,41. 7 96183 931.27 e.- - 89571981 4;i . . ite rae liti at.t' ",..., e YL i•str ,.... , • -$7 AwAt "k" lt t 4,1.,41, sIr..t.;!" •;514 • • aka ! , 7 t 1: -AAc“..2 f.h. .." ..!5".f,33C.4 a " . E., t t a:1 7;;;:t.:•Ir Items NOT part of'Basic Weight o :)...e • r, • o PLUS t"4"717 R41411V-gitilVP.Vialt;01,3 Airefti:- 4 „.. • . • A ' .. sto ", ..m il'llilkin,?/•:gial-iR.; Items part of Basic Weight,but not Weighed ofay AN. • -.J . 0 pp •• •:.: • . ....tVrait % 4.; ••;•.: V % ••!..•:"•••• :: V& .• 34,41,1 Ltlit.142:::4:' ..:94..A., 0. A.M.S.< Arty r .1 gi' •ri: it .4.!”71. .11LX:Z4 itSC•A••• : diefk :.. .., u. ii . V2 — .4. :: f: •••• AIRCRAFT BASIC WEIGHT • 96183[ 931.27 39.33X 89571981 tlirlektspiflt r 1.9wA *"' 11 - 11'1. 22 14 •161"*".•a!"4(1•24#‘ •• • 'clus‘'" 4t•Pc.C*11#7ite 0 K. s , - ir. h -. „ • C lr,, laii ,, rd . frtrat trit: '4-.02."{ 4n;.2:- l. ••• 4 CORRECTIONS a :,..:tit ts2..... y:. :,. m: . s. Sq.. 4 •cit. •.1 .• ;A:t. • NOT Part of Basic Weight r Items NOT weighed but Part of - Basic Weight Description Weight Arm Moment Description Weight Arm Moment 1 • . TOTAL ; 0 0 1TOTAL 0 ,..i.fi,-orritez.f , k-r.• .. .,:,16.4. .,..-Z2.4-,A.:.. -7. _W. l*:.,..*.e..:t . . . err 4,- , . ....., t4.4itatift! .i..J.•r „ t 1)ilgzliii . mustummurrs ‘ ,,,SS ;A— • , : ,... i .. ' '119.22 a Oil) Dieter*, fro, the. 310 point to the sain.axle .centerline I 920.11 a (142) Distrito between the loft nose axle centerline and the jig point. 910.991 a (11.1) Distance between the right ;Se axle centerline-end the jig point. ilS0.901. a (R1) Distance fecal the .referenle data to the 319 Point -of •The aircraft. 950 . 121 a (A) Rain Axle Reaction' Ori‘111011 . . 4 . 311 371 a Cal Sim Axle ...action a s R1-(112019)/2 . • .. • Elifiliiiit,:i*:2;.!t1;- ..ci,n ..lin.. 100,1i.:\Vitil REMARKS" 11:0F0Fitt l.‘' '•-•.:.T.I.ty.i'vill: '•.141.9)! 4-'1474.4fi.L.i n • . . . 1. - The aircraft was' Weighed in alevel ..attitude and in an- . enclosed hanger.' • . . • . . . • - 2_. The wing' panel jack point was used for the- aircraft jig ,point. • . 3. This is 'weighing' 2 of 3.: • • . .- • EFTA00277924

tIAA AaRCRART REGISTRY Mini WO. .1 N DATE: 8- 75- 90 • • •";-•'"7 • • • a 4. u"ktin'ti EFTA00277925

6 24407 2 21864 Items NOT part of Basic Weight PLUS 1 771',iS :14:;!:r AigligteieiT:tra$5ZitiMil0.,4.6 Items part of .Basic Weight .but not Weighed ......7...;,„•:,Fc, i..,,,,,:i.:::a..491:4:;514.t. AIRCRAFT? BASIC -WEIGNZ 96180. 931.30139.35X 8957232 •i TrA43114114-2i;, ..1;!.P..1.51,c, ea'. fill• s,,,w-Pirsi34•tksz.srsta‘wt:ttiormike*A" alliq2:2:filf,f•O:z•• -':i.3rit;.-• Vci.14•::, 044Kiat• aictilfii • 4.:•• ••tilref•air ••••- • %'d :- • fisttel•• N.*, • 4 I'i3„.. .ese4:71,*...:-6w:etonttit4,4ti -C"RECTIONS 6.,:04410T.”44:1:%'?...1 59.5:Tt2 fritii11444( .. . tifizeFitsic. NOT Part of • Items NOT weighed but Part of • Basic Weight Basic Weight Description a (MI) biltince tree the jig•point to the ;Pain axle centerline .•. el.( 12). 01ittence-betweeri .the.loft -nose•axle•centerline and the jig point: c••(Iii).Diatance•between the right mese axle' centerline and the fig point. (Ii1) Distance from the reference-ditue to. the 'fig paint of the etrcraft. (A) Hain Axle Reaction imam . " (II) joie Axle React/en aR1-(1424443)/2 • 4 , REMARKS 1.. The aircraft waa vieighid in a 1pvel attitude apd iri an enclosed hanger. The wing' pane1. jaaki point:weis used for the aircraft jig point. 3. 1 This. fr ...weighing Of 3 • • . . • . • 1 • EFTA00277926

r'lvAr3414" 4241:44- -.4s-Aats <ler L 2 64'n, -4prer,liar# - - • — EFTA00277927

'• - e • war. Etir WnANDroaTATI0N pie tired dger wean No. 04-R060.1 FEDERAL AVIATION ADMINISTRATION MAJOR REPAIR AND ALTERATION' - FOR FAA USE ONLY • (Airframe, Powerplant, Propeller, or Appliance) IDE TOO - Cy • INSTRUCTIONS: Print or type ail 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. 1. AIRCRAFT MAKE Boeing • MODEL. '-727-31 SERIAL NO. 20115 NATIONALITY AND REGISTRATION MARK N5051 • 2. OWNER NAME (As shown on registrallavontificate) Tenneco Inc. ADDRESS (As shown on registration certificate) 16951 J.F. K. Blvd. Houston, TX 77032 • • 3. FOR FAA USE ONLY • • - • • . Ninti: ; ,..: -.4..1:.-•. • ...:•• -.J., :• •- -; , • • 4. UNIT IDENTIFICATION S. TYPE UNIT ;MAKE MODEL SERIAL NO. REPAIR . ALTER- ATION AIRFRAME ateweeentweenneetee (As described in ;tern T. above) XX POWERPLANT PROPELLER • APPLIANCE TYPE MANUFACTURER 6CONFORMITY SlATFJAENT A. AGENCY'S NAME AND ADDRESS B. KIND OF AGENCY C. CERTIFICATE NO. U.S. CERTIFICATED MECHANIC . • Tenneco Inc. FOREIGN CERTIFICATED MECHANIC 16951 J.F.K. Blvd. X CERTIFICATED REPAIR STATION 205-10 Houston, TX 77032 • MANUFACTURER D. I certify that the repair and/or alteration made to attachments hereto have been made in accordance with and that the information furnished herein is true and the unit(s) identified in item 4 above and described on the reverse or the requirements of Pan 43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. DATE . . . 04-04-85 • SIGNATURE OF AUTHORIZED INDIVIDUAL • 7. APPROVAL FOR RETURN TO SERVICE Pnrsuan 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 Ir4 APPROVED O REJEL. CU) EY FAA R.T. STANDARDS INSPECTOR MANUFACTURER ' INSPECTION AUTHORIZATION OTHER (Specify) , FAA DESIGNEE X REPAIR STATION ' CANADIAN DEPAREMENT OF TRANSPORT INSPECTOR of AIRCRAFT DATE OF APPROVAL OR RU1°1°01-04-85- CERTIFICATE OR DESIGNATION NO. 205-10 - - •• SIGNATURE OF AUTHORIZED INDIVIDUAL ....4/O • iAT....- t- a tre :•.;?:Ps_ • • ••`:—.. •' " "I ••:• '14.‘11•.'.44 • • • d • . • ? ‘ "e' . j..: •••e I••••• ms•S • EFTA00277928

FAA AIRCRAF REGISTRY„ CAMERA DO. DATE: '71- "." -....r.T•T • NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An atterotion' 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 air- Craft nationality and registration mark and date work completed.) CREW AREA CHAIR INSTALLATION I. Re4ovecifolding,couch:from L/H crew compartment station 400. II. Installed (1 each) Tosington T1150M24 F/A AFT facing single chair on sliding rails from station 420-tOTstaticih :380. • III. This alteration. was completed in accordance with Threshold Engineering Company of.San Antonio, TX, drawing #270 and instructions identified in report #259. IV. All engineering drawing and reports were drafted and approved on FAA Form 8110-3 by J. A. Dugelby D.E.R. .(designation number.SW.7256) and are available. to the administrator on request. . • V. .All work performed utilizing acceptable methods, techniques, and practices per AC. 41i13-1A. .VI. )Aircraft weight and balance amended. ---END--- • ADDITIONAL SHEETS ARE ATTACHED , •• ••. • . _ , . _ _ . *US. GOVERNMENT PRINTING OFFICE: 1977-771.021/344 EFTA00277929

. . • ." ::,e4; ). • • • I - contmea Of Tatuvonnou:: • FEDERAL AVIATION SINISTRATI0N . • . - NIAJQR REPAIR AND ALTERATION - -(Aidrame,Weirerilent,'Propeller,.or Appliance) • in &tinned fistoWer Biroce No .04-R060.I • FOR FAA USE ONLY OFFICE IDENWICATION Sai-feloo , . . . . . INSTRUCT ONS: Print or type all entries. See FAR. 43.9,•FAR 43 Appendix S. and AC 43.9—I Lot.inbsequent revision di • for instructions and disposition of thie,forta. . - • MAKE•• MODEL Boeing. ' : . 72-7-31 • - 1. AIRCRAFT SERIAL NO.20115 r ' NATIONALRY' AND REGISTRATION MARK -71. N505T - 2. OWNER • . NAME (Asshcam on registration certificate) ---. CADDRESS Tenneco: Inc • : ... : • • _ (As short on registration ceitificcrte) • 16951 JFK Blvd. . • , . .Hotis t on , Texas 77032 - • - 3. FOR FAKIISE. MI • • • • to dalatMeSian Identified herein complied with applicable airworthiness requirements and Is approved for the above described aircraft subject to conformity' inspection by a person authorized in FAR 43, Section 43.7. • • • .... . / 2:raCC • babe Signatur of F seeder ' - 4. UNIT IDENTIFICATION .5. TYPE I • UNIT . . MAKE • - . • MODEL . SERIAL NO. . REPAIR ALTER- • ATI0N • • . AIRFRAME • - ' • . . • • . " . - . . ' • • ' .7PIII•••••••••••••••In4 (As descited in item 1 above) .- XX . POVIERPbOlT . - • • • • , PROPELLER ..- : . - . • . TYPE . APPLIANCE MANUFACTURER . .. , t • 6. CONFORMITY STATEMENT . A. AGENCY'S NAME .AND ADDRESS B. KIND OF AGENCY C. CERTIFICATE NO. Tenneco Inc U.S. CERTIFICATED MECHANIC • 16951. JFK Blvd. FOREIGN CERTIFICATED MECHANIC .• Houston, Tx. 77032 x aunkuoui REPAIR STATION 205-1.6 • • • MANUFACTURER - . ca. • D. i Certify that the repair and/or alteration made to attachments hereto have been made in accordance with and that the information furnished herein is true and the unit(s)• identified in item 4 above and described on the reverse or the requirements of Part 43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. DATE • • - . . - SIGNATURE OFI C7 IN IVIDUAl. 7. APPROVAL FOR RETURN TO SERVICE Put uant to the •authority given persons specified below the unit fintified injtern 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is' APPROVED O REJECTED - FAA RT. STANDARDS INSPECTOR • fg MANUFACTURER INSPECTION AUTHORIZATION OTHER (Specify) BY FAA DESIGNEE , /lc WAN STATION CANADIAN DEPARTMENT Of TRANSPORT INSPECTOR Of ARCIAFT • DATE Of APPROVAL OR VA CTION I,2.- 30-14 CERTIFICATE OR . DESIGNATION NO. ,do s^ rb • SIGNATURE OF AUDI IZED I DWI UAL .. . • _ .. .-.._ EFTA00277930

. NOTICE . . • . Weight•and balance o- operating limitation changes shall be entered in the appropriate aircraft record. An altiratiOn must be compatible. with alt previgus attetations to assure continued conformity•with the - .. applicable airworthiness requirements. • • • • • • 8; DESCRIPTION OF WORK. ACCOMPLISHED (if more space is required, oltach additional sheets. craft nationality and registration mark and date work completed.) • Mounted T.T.G. (Time to go) .Preset•Unit forward of center console, below existing Radar Indicator: (.5# @ Sta 210) • IV. Meunted .D.I.U. (Digital Interface Unit) with suppliers rack on shelf adjacent to ATC-1 Transponder in A & E Bay, R/H Side. (8# @ Sta 463) Installed 2 amp klixon CB on:fetwara-end pf.#2'Essential Radio Bus CB.Paneli. • '.Left side. of cockpit. (Ste 261) • • • • Installed wiiing and associated hardware VII. Complete system installed, tested, and operationally checked, in accordance with the manufacturers manual #910600, Tenneco Inc. Interface Wiring Diagram . 011586, and acceptable methods, techniques; and ptactices per AC 43.13-1A Chapter 5, Chapter 11 Sections 2 thru 7, Chapter 15, AC 43.13-2A Chapters 1 and 2, • EFTA00277931

FAA MCRAE REGISTRY CAMERA NO. DATE: v i - g9 adell••• . • 1 :s>.•••:: • 2 B 0' e. 1 PI WOO awri--;-•?-5 1 3 ••• v pc Mus—ia;--Wr DC Revues — r/Pt WAIT+ • your- ' -ist RIN+ I A is , _ /7 1- 6 7 (9 22 • t3 ‘ 24 I 17 • • 33 45 Ts 44 35 3 : se 443 49 30 • 34 Ls RIN- am Ott ans. C CO • 3 • ø X Guntur POSAM PTIONAL CABIN OWN« CONMOI. UNIT (DCI4 3 . } • AIII.fR0W 1OO (0101 Jfr 39,t eaWark, Okilla .1.1.64k6 J~/46‘7i2 Cs. jeCITE BEN/a18 noso frotwrort. -7"••• - • • • a AM Mt acts ets.sAse A S aW 4440%90 Aso Ott/ VIC44'0 14440 Attn. ELIMINATE ALTER ran OCU ,GOWN. MANSE. PEZ OCh LOG It 2S1 /043-83 diseer »snit a - CASE PER OW LOt S 29. ~isn't* OM LOS s 36e CAMEL la OtS. 'Earl 4-44 moms bre 4921/14 L4A 30Erts It MY c tea As loff..1205iro4; 1:buisr-te esepstky., RILay. WALL ortJ.E.k P05 Iran: ea! To 1(42 Se vipka - fl A nurse: conraot nkr Ottio4W. 6170140 EZhAftV IS ON tilem. P142 49 GNO AND PM 30 Onal MELDS MAT DISPLAY.. Pnal OPEN AND AfA130 GAN) . YIELDS 11413 OISILAY. P44.29 OPEN AND PIN 30 OPEN ALTS(NAYES OLSAI..11e. ~21 GINO AND fl y 30 0A/0 TIELOC. t.060 DISPLAY. a. 371 CAns Atft£StmtE ~VECTOR Meats/ UNINSELT10A/ 115 /UM 4:*e. ami. tAM£ was 3P1 ØØ as TAW OF Dui . tria le %stir) . ;pc irTERFATC Or Wu To es Z3 t• PORF OF --.Sicsonst_ C.44tutEt tan 1.1 MX ~WED AV AstAte: au in rJA te_setwout [ant Pea n(4 NEnalFFs/ 7t ooTA (Kr . NrA TS oisiN tµYA our. 54 Can 7 - 6-(1404b ~NS .04/0111r) RN Awe ors wag on s r-sr ant atones* twat AM MUSIC sr? insur VHS Z 241 BUS. gasp DI AND 84 IDARIDD 4/4/11- OVA/ AND le2 2.4V SVC WOIE: AU-17110E ENCINO IIPLIT nor use stnei ARA•tC 414 miIPUT1 ARE REG4ft£Q annee P/J-PLAY annsneryz oersinEa P7104 ACOSTA W AR//AC 419 1411/1: fox REPEOXE roc osr" ohm AV Conifer SPERRY AZ-243. CCIPINECYOR 7S /4- 47 10 PIN 5, 47I4- 47 ro sin 4 IND 9J/4-44 ro rain. 4,2 AR/NC 2 fVK£ 010~ BE USED FOR DIGITAL ADS IF rsys ot one CONNECTED. art AC/NC CAM ea- ast-is BV #2 INS Ode ONE a - DIGITAL ADS nor asap- nS. TOC IALT a Ow, 83331 2 WIRE AND t YOKE 4.11/K OUT/WY "OUP ar wswecreo IF AVADABLE.. 4. AVOID swore& cost WITH orace IttaRAPT WO/N& MOWING. morn ~TM* DIRJLEAITZ • 3. ALL .11/1aDED Inter 117 NAVE AVSZDATED "setter. sinew: ro at atenfoco TO can-warn rani At MADAVID 100 D/D RACA' END. At AND At OZUI COVACC71X team/re-4:os° ossnerse «nu. goat MAW» SE ta/C433 IN rot tan' sun r>/OFTN. 24MI, OPTS:WILL CSCEPT Ate aura /moor. NOTEst: ream. ormatwin sPECUYED, CONNECTOR. TABLE RET soarcedmom 1 acre-aszsre MAC P.,W LPL earn enzscuucu-oon rum 6/sole ' 2P/ Pr PrOGI -43-15 PTOcc-S-÷s 625'00 8 _3 PI In 3 /24 F -I41-12.9 442.5- O/P in' i4S31.22E-444-/PS HS3Il2E - /F-.7S 4250/7 3.12 1/3/1i .94 ati EISC tlut..c NO 625O/9 I ()MI COO( NC(I0 Offif 10F.PariNG IVA .i MIA? • 140110CLATUINC ON OESCSNITON ' . PARTS UST I 'fl. ~En OMONFSL SeNaNCO ' man NO ~MU OISCatias . ~9~a Me. Int ~era otessios skails = = ASPIC, MICORIOCA TED HitfC MY FORD W. 7211714 CA 421 SO • APINON•45 OlfC ''t"..1 amoretten aiLDED larl13 1NTElittNAIECT WIRING AIRSHOW 100 WITH DCu Nal Ufa ON APPIXATiON 00 NOT SOU Oliastosa 910600 gvp SEEET 31 SM D tom socsa so; OLNYINC. FO. Ina 4.-- T . 9 20410 F IT.ccT / Of _~.wi.-s. 3 ..b. •-).:;•;if:. •• . • 4 •1' • •r •t .•1: C.:;;; .. • • 7 :•_7 — nee, plit;es •' • • ••• ' -• 49•;:“" •154„; • ea. 2 o. . Svc, EFTA00277932

-115%021.771 •*.seiffirs . , • • et I PYDED our 75 al• } oars •••• az Argitoc 4141,14Z 9 O.47-A — 2•M/l% It REF AMEN TA 170,0C eft SIG .1. • r/HE't kr av Dosnm Com-Ro S16 - • . ISMINItrrai sfaitW.-e-A-6ta . - . ' • _.• - ;.- EFTA00277933

- FAA A IRCRAF CAMERA EO. rtami REGISTRY • DATE: MYOPIA: OMNI O/LTLAT OM ma UNIT WO* NAP VCR • -erf INFO Mira. Iko A enalar-S PROW Vat PE Ae«.0)14 e.g. APPUCATION jct. ATE &W/NO VIDEO A a Dc Atin tsetil VOCag0 An0 arr.& GUIMINATE ALTERsaTE DLL COMV.,_ is 0git -AGE DIAPMG PER 2•I • trzonm toe /04J-03 Akre r0-20431tate 12 ft-fil a," ora22004 gott0 D Gaol PER OW tot • 2.96 c LALIMEW7704 LOG a 164 30CTES 00,4 CaMat SZE tieM i4/ doFf- Powhtg 15 er.weEr.: in pa, "'UK /i/ALL 0774£7,. .231, 15 Suoy1/Eli ra Rd it le If. »tor A agrater LL' ogrou TAE ouPtiV. &ROUND RETURN it ON WIELD. ,c9k Gam AND ems° OPEN naps MAP DISPLAY. Arm Et OPEN AND Ft.W.30 6.40 YIELDS INTO DIM«. Ram?, OPEN AND ~30 OPEN ALTEcivareS Dtsietny. RaVn 6040 ANO Paa 30 4,110 YIELDS L060 DISPLAY_ 3S1 (ACM AttatiME Waeablt eCCOW CaUMEtTIMU 76 "(MO bal. SW CAME won 3F1 Ottitidels *3 tier OF /KU cma FOC pericoic. OtTIERFAtt Or tol -nb 23 t • roar etc fetsons L ZáMfUlElt. mate« 43 marstrauct 7Y Assn.: MU AI OW JEte-itérimmi ItS,t3z font nm bescoutTOM r.t 90617. OUT 3 ‘. 11,0.TA rT DATA. • Z ton air STS 610MMS 7 Tra.m.NA , 4031440 pi swag FOt asmaCers wing ate I t.v/ taut titaliaOO.4 town ~Aisle arli ermor ova z 241, BUJ. ammo Or ~Oa MillatCarf INAPT aver itmo az 2W 60.0 gore: ~Iron ~DNS avato-Nor IWO WHEN ~at 429 INPOT.f ARE irealarea arrrurr£ or.rpur pairrrerray . OBTAINED FROM AIZILITA OW AR/AC 424 AWIL17: Pot REFERENCE: POE oar . DMPLAY CONNECT SPERRY AZ-Zett CONINECMC 77 IA- 47 TO PM/ 5, 7.TIA- 47 TO P/N G ISO 1-T14-44 TO rum. &In AR/NC 2 Witt tHOLICO BE VIED FOR DIGITAL ADS IF INS OR ONt CONNECTED. Art AtiNC CAN BE ant BV si2 INS 04 OAV er DIGITAL. ADS flOT USED- . LI\ roe • hut OR ow, to». 2 WIRE AnD G WIRE AXING •OUTPLIT .11ARILD BC convocreo AVAILABLE- a. AVM', /(01/7"Ne COAX win< orate ~CRAFT ewers.* AIOATE PROOLICYN6, CYLALiNTt. 3. AL( .nwricoco mar TO wave ~Area JACKET . SMIELAT TV BE IMWACCO TO CONVECTOR SHELL AT ARTNOW i00 DILI RACK EARS. a at Ant Ar mix apmeerac .caumee case 04400ETER COAX. 1654 name) IPLICED Av TOR WNW RUN 0/0,7'1. 1124 AIVO OPTIONAL EXCEPT fait POWER ~POT. "NW runtrr omen's:Er EPECIIII£0) CON.VEC773A TABLE REF OUTZIPTION ALTERNATE *PAC P/N In OIS7.1111PC7t3ZELY-000ITZto) 61s-o/e 20/ RPTOL£--8-lS Procr-8-+S 625008 5.91 1153,26F-10-ap 625Die . 3.01 nS3I22E-/f-IPS 33:12E-M-425 6250/7 -3JZ uslv 4g 20 aNC etxx HD 6250/8 l iatioTcoor rain OR Mine I•1 co NOT OAMMNS flll COCRIPTOI AIMS (Zr '910600 gEVP : ,SHEETr 31 2 410eC. ~tattoo rev «WC 147F0A0 CD. 77.137/N CA ILI 20 INTERCONNECT WIRING AIRSHOW 100 WITH DCU r- et. C LL 0 C • 920410 'parts • of: • EFTA00277934

• ORAIRMIDif Of VIANIPORTAVON ' • . .. • . 'SPA AVIMIOt4 ADMINISTRATION t• . .- -. • Fern t r...vgat Bw4ei wren No. 04-R06-0.1 ... MAJOR' REPAIR FOR FAA USE ONLY . ANO .ALTERATION, orna IDENTOF • (Airframe, Powerplant, Propellers, ei Agi011arim) .‘ ak , # - INSTRUCTIONS: Print or type all entries :Sri PAR 45.9* PAR 43 'Appridlx Di red AC 43.9-1 (or subsequeist revision tbeteci .: for lasaructions sad disposition of this form; -. ',‘ 1 . ; •••••.' • - ' -- - . _ -46-MODS; 1. MAGNI MAKE • - • _ ' HOF I NG - . ' • • '. ' 727-31., , SERIAL NO. . • ...... , ann5 NATIONALITY AND PROSTRATION MARK • - USA N51.15T . . .__ HAW (Ais them, TENNECO on. registration eartIllare) INC. ADDRESS (As.showr on registration certitioste) • . .16951H3.F.K. Blvd. • _ .1lottiton: TX 77032 fr A. (Olt FAA OFF ONLY >. , • . .. imposorwasse ss. is scIt.to.itiiiip....rf:47:3364:r... irma ilsoraionvogru bs rife.; id . t • 4,11: IDOMFIGTIOIL , 5. ME UNIT MAO .1 ,,..„. - • MOM • • • . 7 SUMS PIO. .: - tiPAIR ALTelt- ATION AIRFRAME e • . werwanneoes•444.• iit dirtErill; Orr' V aboar) J. mirOimistraus . ,. • . . • . X POWERFLANT - • - . . • • .. _ . , . - • . .. PROPELLER C ;-- • • ' • ' APFLIANCE VIM '` _ ' IMNIPACIIMIN ..- ' i. (OISMNITT _STAMM A. AGENCY'S NAME AND ADDRESS S. KiND OF AGENCY C. CERTIFICATE NO. G. C. Kolb el.t. CIETIPICAT19 MIOLANIC Tenneco Inc. POUCH OITOICATITS MICNANC • 16951 J.F.K. Blvd. X •FINTIOCATID SPAR STATION 205-10 Si. TX . 771112 leNUIACTVIllt D. I certify that the repair and/or altrrittion made to attachments hensto have been made in accordance with obit the information fratthiSiti herein is the unit(s) identified in item 4 above and described on the mete.* or the requirements of Pan 43 of the U.S. Federal Aviation Regulation, best knowledge. sad tree sad correct to the of my DATE • December 21, 1984 SIGNATURE OF AUTHORIZED INDIVIDUAL - LS _....e.... " 7. ifilliflU. _ 44 1 FOP II TO SEMICE %neat to tin autheriey awnpasoes below identified in items 4 inspected in by specified the unit was the manner prescribed dr Administrator of the Mad &Woe Adarakaratier and is Etatinovw allijEc hp BY M4 PLY,• MISS IyallOS a OWILIFAltiat 1141PICOON AUTNOSILATION OTIS fliptin, -='-, - MA MOM X WAS STATION CANALMAN CaUITMINT Ot TIA14,041 !WC" fX ASSAM a DATE OP APPROVAL OR REJECTION • Dec. gat /940k - CERTIFICATE OR DESIGNATION NO. Baer-L>a . — SIGNATURE OF AUTHORIZED INDIVIDUAL • ...dies. - d..-- rce.er • • O. EFTA00277935

. . Weight and batons or Operating limitation changes shall Wintered in Otis appropriate aircraft record. .An altoratiOn:Must be'compaHble with all previous alterations. to assure continued conformity with the . applicalskainiartldnsise requiremeati.. O. DESCIPMOM•OFROMI A(f.OIRLIMED (0 more epos* is required, attach - identify with oil craft nationality and rogidrationinadt and data- work. 000tplohod.) • •-•;V:" . • • . . ,•• ' ' . 7 ,77 .7 t.;1'7". I. t.itenioved Thermador Trash Compactor P/N TI4C-28B S/N 3060438, Having 6 AMP,,,;•,:,0 • 4 a • load, approved on 337 dated 9/19/83. • AL:- Installed:Montgomery Ward Trash Compactor P/N SBW-5235-c S/NT481100442,- 1. Having.10 AMP Load. _ • III. Unit ftinctiOn tested. iatisfactorily; unit operation does not adVersely - affect the safe operation of the aircraft. • IY Installation was same as previouslylpprOyeCoo:N505T 4/01/81'for - -- • -1 Aireseardh Aviation Co. , Los Angelei-,-CC-- 1See previous-weight and BilanCe 's Data Report 11C-3688;) V. Installation using acceptable meaies, techhiques, •andfirectices in dente With AC4313-1A Chapter 11, and Chapter 13. • •VI. Weight and Balance and Equipment List Revised I •_. , - . • C t) iv e>•.- r.,•• • . • ;VI • I . Viq',~.• 71 , a • A ,.:144.0 • & •-••-• e • . tc: :Ism • -7,1•7ostip •., •:* • • rti-.• • • L. • - •••••:. : • • . • !- • .• - : . . . 1!.7 . t •• • EFTA00277936

a ll..... .. ....1.1. 4AIENT Of MANSPOIHATION CEDE AVIATION ADWNISTRADON - , • Form Approved • . Bud;et Buren No. 04-R060.1 ' • t MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY . (Alrfromi,.Powtriitant,.Propollir, or Appliance)' . i zjoarrgri INSTRUCTIONS: Print or type all entries. See FAR 43% FAR.43 Appendix B. and AC 43.94 (or subsequent revision thereof)' for instructions and disposition of this Cos; . . . - - -- - • MAKE Boeing • . MODEL - .. • - • - 77-31. 1. A11101411 SERIAL No. .. 20115 . NATIONALITY AND REGISTRATION MARK • .. N505T 2. OWNER' NAME (As shown on registration certificate) - •Tenheco Inc..-:.. ' ..-. ADDRESS (As shown on registration certificate) . 16951 J.F.K. Blvd: i . Houston. TX 77032 3. FORMA USE Nu • . : • . • . . ignitions Ismlilim Ise is unklISIRIMP •: . , - tilleiteNMS and Is On/1W Ss. i - , ' Wiest to orkentay Is II • I • ., 13.7 D*). • : . :. ‘..... •:pra. . • • -• 4l ' _ , - . . ,...........a. _ k - " I. Will IISTIRCATION S. •TYPE *SNIP . • • 4...L • • SERIAL :40.. MAIM • AMA- ATION AIRFRAME' • . • . •••••••••••••••••••#14 ilestrist in item I abowderamma re••• • : . . • j(X POWERPLANT , I .. -• • , -• ' " • • • ' • FILOISLEILv. ' -c.5 ;• , ..,.. • . . •.. . . . . - .. . : ) ! •. • . . . ...• . , ' • .... . . .•' - - . • , - •••••-• ' , APPUANCI ..._ : . . .1. i :.• .; . - •• . ' .. ".. Lionisation • . .. -. .- • t - 1i. •• . . ,. . Jam : a - £ collethITI STATHAM • , A. AGENCY'S NAME MO Amens • t - y - IL. KIND OF AGENCY C. CERTIFICATE NO. • Tenneco Inc. • , tit. COMFOCATID MECHANIC 16951 J.F.K. B 1 rTrinift- MOO* anararto istamtc ... . . . ' . vd . Houston, TX .' 77032 ' • x. pumnommmmessmnom • '205-10 . • -. • D. 1 certify that the repair andinialteritiois• snide to attachments hereto have been oat in Scootalta with and that the infortisatioo famished, berth ii was and the unit(s)•identified in Item 4 above and described on the reverse or the requirements of Pan 43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. - • i ... ' . DATE 1 . •!•• ' .. : • - '';' . • 8/3/84 ...!: •!.... :,. ;.• .,- •:‘..", •'. SIGNATURE IN • - • , . • . , 7. RIROVAL FOR IfIRM TO a Pursuant to the eutbarity given persons specified below the unit idendfied in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administradon and is'. al AP/MOVED ORFJECM Ls RT. stistacts . . spareast AIDNOINZADON IV ... ..... . PM OWONft y ...- ... CAM STATION COMIX034 DEMITlect Of CRAMPONS IMPECTOR %en • • • DATE OF AITROyAL. OR CERTIFICATE REJECT107 g it OR . .... . DESIGNATION NO. SIGNATURE. OF : INDIVIDUAL • 10 1/4 ' ‘.7tir r ,.. rditiM;TA: - " 1Z-- . • • ••• • • • %I "flet. EFTA00277937

NOTICE Weight and balance or operating limitation charigei."shell be entered in the appropriate' aircraft record, 7 ' An alteration-must be compatible with all previoaalterations to assure tontinUed canformity with the previous. 'alterations applicable airworthinessrequirements. • • I. DESCRIPTION OF WORK1KOMPLISNED (If more. space is required, attach addit I sheets. Identify with air- craft nationality and registration mark and dote work completed.) -- - • . 1 . • VIDEO ICINITOR ND VCR -INSTALLATION ' . ,L1 ?P•41.1, . Revised-interior (which was preiiously installed and a "proved by Airesearth'; Aiiation Co.. Los Angeles, CA.:.4/7/01 on report. No..C-3588).as follows . Modified Coat Closet (Ft/H.Side"..Sta..814*t5) to.remive_moUnts f.01‘ . installation of the following: * • ;•••:k.r.;1; yipeo• Recorder -MitsubishiNS-33OUR:' it;;;Ithed.,PiOnttoi,,,: :,mit.;sithisht CM-1901 3. Infra-Red Transmitter Nady 1RT-200 -A: Altitude Cut4Ut Switch -.Anint 90500 ,5:.' Power Receptacle ;":7777K1 • • ...,.: . .6. : Pewer:SUpplY..:AC4C: AdiOtehl':',:.NadY,I.A72420 .....:._:::: ,.......: . • . i i Modification of coat clOset in accOrdence:With Structural Substantiation RepOrt NO: 243. and. Draividg-No. 266e submitted and approlied:on'FAA.fOrm.8110-3 by ..L A:. DOgel by.i 0.4.- . it::Ttirettutoleelglileering ',Company, Sin Antonio, TX. : Reports and drawings are available to the AdministratOr:on-request..: ' ' . . , . , . • f A;;', Pei,oer Supply as follows: . . • A. 28V DC Bus No. 1,(Drain Valve,: Shower 3. amp CB, existing). . . • B. .115V AC 60Hi (Utility Outlets Aft .Cabin - 15 amp C8, existing). ! ... • . : .• • • • • • • • : • • • .1 • . IV.. 'Utilized existing !Al tee..755E:Speamers:at.Sta....730.0_. _ : V. 'Systems installation is in aceordanee "N505T VAdeo* - System': dated -7/26/84. : " • _ VI. All work performed utiliii0g4CciOtable methods, techniques, and , practices '.0er AC 43.13-1A4.-Chpi.15:6:04C..43.13,2A -Chott.: 1t6._24.. , . • _ . VII: 'intiallation- waefoiktiohally Itettedat ground level. end at'altitude dUring -performance check- flighti;ihd:.operitedsatisfactorily-404tdid:hOt adversly affect the operation. of .anY'.1)thet:licsterifs-._ - Rircraft' weighed ' ileighnana Bel anCe-a0d . at amended. .. . • ... . " ' - • - • • •-- ••: . • - • • *MS. GOVEMIliata PRINT.04.4 OFFICE: 1977-77,421/2/10 ••• EFTA00277938

MEM OF montoitinnow - • • Ff00AVIATION ADMINISTRA110"4 Fitdpmeived Beiges Bureau Noi 94—R060.1 ' • MAJOR REPAIR AND ALTERATION - FOR FAA USE *NIX- . s lAirfr ok am . Pow•rplant, Propelkr, *r Appleana) ON A6DENTMSATION -6,-17>e, INSTRUCTIONS: Print or type all entries.- See FAR '43.9,, FAR 43 Appendix 'and AC 43.3-1 (or subsequent revision thereof) for instructions and-disposition of this form. . MAKE Boeing •- - MODS • • • . 727-31 I. AIRCRAFT SERIAL NO. • • 20115 . NATIONALITY AND . N5051. REGISTRATION A' i 2. OWNER . NAME (As shown on registration certificate) - Tenneco Inc. • . ADDRESS (As shown on registration °edifice* 16951 J.F.K. Blvd. Houston, IX 77032 . '' . 3. FOR IAA USE An I. . . . . • . . . ' ' . . • : . . . . ... • - . - . . .— . .— ___,....... / —. , • - .. 4. UNIT IDENTIFICATION- .:. 5. TYPE Witt . ,SERIAL NO. /SPAM ALM- Anon AIRFRAME memomennennamne (As dasaind in item 1 above) XX POWERPLANT _ MOMS • APPUAtICE roe . ` • . NANVIACOMINI 0....r. - 4. OINTORINTf SIATEMBIT _ • A. AGENCY'S WALE ANDaRESS. • , • fr K*40 Or AGENCY C. CERTIFICATE NO. Tenneco 1695! J.F.K. Houston, bat Inc. Blvd.,/ - ...I j.:-. TX 77032' U.S. Cternicana maawac :205-10. . twins OVITMCATIO AtIOIANIC •X Penman ammo station, - '''' - tififimpArmana D. I certify 'thin the repair andiot ii/Miatliali'Matitio the ank(e) identified in item 4 above and described on the reverse or attachments bent* have been made inateardateee with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information fissnisbaLhereits:le !tend correct to dribs, ofmytemerledge. •. . . . • DATE `;'..,i ' ! i ; ' ;.i.'1.• =Wart Of. . - " 8/3/84 . - . • t • . ., . - - . ‘,,..- . .. - isenvia fa MINI TO SERVICE I.'. ' • • Pursuant to the authority given persons specified below, the unit identified io item 4 waszbasted in the manner prescribed by the Administrator of the Fedetal•Avistion Adsninistradot; and is igi pPROVED. QM Pm Ittelininsl. . aiiiiii veire.." :.". itelebtleata isitte:MIAllUile...:'c: °M .. _. 4 ._ . '..::.c. . . .. . Nub, ottitanet: - - x ISM ;SIMON Of 17.011f 0t1 SIVE= Of EIMOKAPT - • •••• DATE Of APPROVAL. OR, , REJECTION ' ' ' ' ...... 8/3/84 • CERTIFICATE 01 .. .; . DESIGNATION NO: 205-10 SifirbiPmg. OF . UTK . ..040,M.04'...t.-: - • : - • - •• •: ` 4 • • . I ., '• ' ‘ • d i .• ... • • S s • • • . 1 ••• • ••• : • S. • • • • • • • • • . • • • . . • •• • • • • • ", • •••- : p • •• .15 c.f . -'sr.t .‘ ,;:ri gtettn. ;.;-‘.. • . - • ---- ••..• ••••••••••• EFTA00277939

, I. AA AIRCRAFT REG TR NO. ) DATE: "e".!'•• • . E - Weield'and balance ar..ope ot.npp limit Lion chaeges,shisn be enter.e.d inlipe.appropriate aircraft record. An alteration must be COnqicitible with oil :preirioio.alterations to assorseentiOuod conformity with-thit applicable airworthiness requirements. L7, • • ;_ O. •DESCRIP1104 OF WORK ACCOMPLISHED• (if more ipaai is requires attach additional sheets: , identify with oir- croft nationality. and nigidrallon.:inadc. and dcd• work-annialided.) '". " • ... .• . • . - BODY STATION .950 BULKHEAD FORGING REPAIR • . • • .- • .; --• • Repaired left and right BS 950 foiging, lower Section, *in:accordance with • instructions• provided by Threshol d ,Efigineeri nve.ompany Of :San Antonio, TX. Subject inStrUctionS..t.are identified, in,:i*.eports:K.• 242 and No. 244. Reports We're drafted and apprOved'on- J. A. Dii01 fp E .R and'. are.:avai l abl e the"'Aihnf strator -on: request ' = • _II, All :work performed utilizing accePtahlk, methods;, techniques,- and practices . per..AC 43.13.61A. • --7, I I I • Airctlift and' Balance aliendecl..h . -:- • • •- - • - • .. • ADOIT(044 SHEETS ARE TTACH6 • • . . • • - • • • • • . , . ',':•X•V • .: ,.. . ..;•-•••• --•.• „..; . .. 4 .0 411, - _.... , • EFTA00277940

• . (,- VITNERIT OP. TRANSPORTATION . C . • flittsif AVIATION AomimstRATioN Oat Appeared Budget Bureau No. 04-Rollo.s • . MAJOR REPAIR •AND ALTERATION FOR FAA USE ONLY • , (Airframe, Powerplant, Propeller, or Appliance) ' • , e IDENTIFI ATION OFFICE ..8_7 . INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 4319—I. i7.4 ot sub2s!quenr reeis•ioe,thatoe for instructions and disposition of this form. ... . . . . . . I I. AIRCRAFT MAKE • , - Boeing' MQ0/1 ≤ • ' 727-31.. . • SERIAL NO. 't ' 20115 NATIONALITY AND REGISTRATION MARK , - U.S.A. - N5051 - 2. OWNER NAME (As shown on registration certificate) Y. Tenneco Inc. • 1 — ADDRESS (As shown on registration certificate) . 16951 J.F.K. Blvd. a Houstor, TX 77032 ... • • 3. FOR FAA USE ONLY . • - ,.. , • • ' - • • - 1 • SliarnsiereetsWoremaInloor e alr e ini i:.•,:. ,•>1., _ gMy for tho Omit -- 1,-, -: ISSIRS ell 6 Ishitieboti f 11&,•:.: .:!:...,. .t. .. - Set IP ea* • , . .. , , ULM • .. . • - ' -7 619 • ' I - 4.•0111T IMMOLATION • S. TYPE UNIT MAXI , NOM • • . MIA* NO. MAII WEI- ANON AIRFRAME • . - • -• 4****1•1•••••••••••••• AR deicamed in awn I X . abovounaroonekeenosee FOV/EPPIANT . • : t - ! ::- • .. PROPELLER :...; " • - ' . Mt • .. ._ . . - • • • . . •... ... : . . • , .,.. - - . -• . APPLIANCE NANUIPACIall ' 6. TY STATISM .. c. A. AGENCY'S NAME AND RODEESS . & XIND.OF AGENCY C CERTIFICATE NO. *S. OIRITFCATED MIKKAPRIC . Tenneco Inc. . . 'MOON CRIMPIC.ATED NIGIANK • • :16951 J.e,..K. Blvd. - Xparincaras RIPAJR STATION 205-10. Houston, TX 77032 . . • LoArrusavate . . D. I certify that the repair and/or alteration made' to attachments hereto ban been made fits:cordate with and thin the information furnished hereinh true and the-onii(s) identified in item 4 above and described on the reverse or a the require:Senn of Pan 43 of the U4 Federal Aviation Regulations correct to the best of my knowledge. DATE r - SIGNATURE OF *mat= INDIVIDUAL • -.. ' 7/19/84 . ; . . . . ..:. -- idi—. • ....,..rder - ..• F. APPROVAL FOR RETURN TO soma Pursuant to the authority given venom specified below •tbe•unit the Administrator of the federal Aviation Administradon.and is •IEWPROVED identified in item 4 was inspected in the manner. prescribed by ORM • . MA RT. PANDA= ONSPICTOS N. NANUTACTOOft. eistecnctrAunionrAnoii. Ma Seits) BY ---..- MA .DISIONSI - eon STATION Of TITANSOIT INSPECTOt Of ANOWT - . .... . • DATE OF APPROVAL OR . REJECTION -7-0, 57- ay CERTIFICATE OR ., DESIGNATION NO. .72,os-io SIGNATURE. Of AUTHORIZED INDIVIDUAL . • . . I • ,,, ....S • . • d 30.Pr evsjaL.c. • nr-- tar/ eie 204 011 6f !j sz ..; ;. • • id s *Pk: : — . • • • • • • - , . . • • 1•• ••• '-.• • • 'sr ; - • • e • .• . ...NIZIEL.:•••.w.......•.•••••••••=.•••••••• •••• ••••=immm:PA.momi: EFTA00277941

Weight and balance or operaing limitation changes AO 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 air- craft nationality and registration mark and date work completed.) • - . . . . INSTALLATION_ OF 115 VOLT SOCKET .& HAND VACUUM WITH CHARGER BASE. Installed 1 each Cutler;.- Hamer aircraft electric safety socket - P/N1.777-Kl.in rear cleset.rleft hand side, station 1137. Wired new • • plim'itite-lititchtng.15/1i5r.volt AC supply from utility plug in vanity. . „K:n.7 rf.:1z; e: • ;;; The safety socket incorporates a switch, which connects the supply to the vacuum:. battery Charger-when the charger plug is inserted in the socket, and is protectid,hy i'250-MA:fuse. . • _ Installedthe following Platird adjacent .to. safety. socket. . ,..:`. .._.....:' , • ::••••••• Asir me sage imusomom oricamotethavii,ants 40 . • ire, tnie0 IV. Installed-1 each Black & Decker cordless vacuum clearier with bittery :::charger base.P/N 680982=00. Thisziniit is Underwriters- Laboratories • - • approved- and has the following specifications: 120 Volts, 60HZ, 5 watts! -• -*7.2 V.D.C., 125 MA. The total voltage.draw from*thebpower supply will be approximately 1.06 MA::, ' . - . V. The charger base is mounted adjacent to the electrical outlet at station *1137 and.attached using AN526-8-32.screws, AN97073 large Area washers and AN305-8•,32 fiber:: lock nuts. . • • 4`F, VI. •Weight 6 Bilariee and EquiPrnent.Lisi intended. ADDITIONAL SHEETS AM ATTACHED • V • . • .itus.Goverisoitm PRINTING OFFICE: 1977-771421/200 -11c.-A • ,r•zrt, ••": EFTA00277942

• • • P DATE: yma? _K., DEPARTATIrk 4 - 1 TRANSPORTATION. : . ' . I . FEDERAL .A.ViaiN ADMINISTRATION • cci Form Approved . Budget Bur.rau No..04-4060.1 FOR FAA USE ONLY. MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, or Appliance) OFF ••"• IDENTIFI TION a /zor (-5Pitp0.3 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. • MAKE BOEING MODS: • '727-31 1. AIRCRAFT SERIAL NO. ' 20115 NATIONALITY AND REGISTRATION MARK USA N505T 2. OWNER NAME (As shown on registration cortificatii) • • TENNECO INC. ADDRESS (As shown .on registration certificate) • ' • 16951 J.F.X. BLVD. -,HOUSTON. TEXAS.. 77032 3 FOR FAA USE ONLY .. .., . . s. .. ., • • •-. .... - , .. •11- - . .... . -•• • ,• . - 4. UNIT IDENTIFICATION • S. TYPE • UNIT • MARE • , i MODEL - SERIAL NO. . REPAIR ALTER- ALT ER C4 1-1 AIRFRAME *o , . • ' r iannatimeno•tanne Asderribird in 'item 1 above)' • .x POWERPiANT ) . ._., ......... . PROPELLER i • I . . .., • . . . • . • - -.• • I. r :I: i • 4 • • - - - TYPE ! ' " • -. • • APPLIANCE MANUFACTURER' ..,' , . • ., ... , . — . . . . . ‘. . - .". " 6. UNIFORM STATEMENT ." A. AGENCY'S NAME AND ADDRESS ' . •!,:• - • : S. IIND OF AGENCY . C. CERTIFICATE NO. G. C. Kolb . 'Li.. 4.- . .. : ..:..; :. iil it: . U.S. clISTIFICATE0 MECHANIC • • Tenneco Inc; : i 'i • il ' : : . : .0SEION tEETIFICATIO MECHANIC ! .A:+ • P 16951 J.F.K. Blvd.. - . . '• • CIITHICATED REPAIR STATION - 1337480 Houston, Texas.:.,77032. . . -t. . . MANUFACTURER s. .. ., - . - . . •—••• D. I ::ertify that the repair and/or alteration ;nide to attachments hereto have been made in accordance with and that the information' furnished herein is true and .-. . . 'the units) identified in item 4 above and described on the reverse or the requirements of Part 43 of the U.S. Federal Aviation Regulniuns correct to the best of my knowledge. : ••• • ..• —• DATE - • 'Iri• .• il • September 19,' '1983' 'SIGNATURE OF AUTHORIZED INDIVI AI. •' •• • ' i•i-ii . • i '• • • ! 7. APPROVAL FOR RETURN TO SERVICE Pursuan tit the authority given persons specified helow the unit iilentified in item 4 was inspected in the manner prescribed by . the Administrator of the Federal Aviation 'Administration 'and' is 014 APPROVED 0 REJECTED FAA ELT, STANDARDS INSPECTOR • - • mmairicruieit: '" •• . - • • , • •0 , • : .. . . . OTHER (SeA6601' ' I I . ' 3..'; II ' i z-- . • BY f AA DESIGNEE • REPAIR STATION • • : I ' CANADIAN DEPARTMENT • • OF TRANSPORT INSPECTOR OF. AIRCRAFT •-• • DATE OF APPROVAL OR REJECTION ' 'September 19. 193- CERTIFICATE OR ..c... DESIGNATION NO. IA 1337480 SIGNATURE•QF AUTHORIZED DIVIDUAL. ' • • •• • • 1 - .: . .. ./...--- • • • . • EFTA00277943

1 ... • . NOTIcE Weight and balance or operating tirnitcsiion ;banes shalt be entered in the cipOrOpriate aircraft record. An attoratialniuse be canspatible ., ,igs.ag.grOiaus alterations PO Waite continuedconformity with the appiicOble airworthiness requirements. . . B. DESCRIPTION OF WORR.ACCOMPLISHED (If more space is required, attach[ackiltional iheeti.; ' Identify with air- craft nationahty'and registration mark and date work coinOeted.) i ., ,. • ' • ,: • ,I f ! Removed Montgomery Ward Trash Compactor P/N SBW-5621A S/N 08D-00489, Hay.ing -10 AMP Load. . . Installed Thermador Trash Compactor P/N TMC48B'S/N 3066438, having-6 AMP ;- load, -sanielocati0n. . : bnitlfunetion tested satisfactorily; unit :operatien.does_ not adife'rsely affect `the safe operation of ,the aireraft : V. Initillation was, replacement of unit previciUslyrapproifed-447-81 for Airetearch Aviation CO., Los Angeles, Ca. (See, previous _Weight. and Balance 'Data Repiirt #C-3688.)• V. Instal ration using acceptable :Methods. techniques,* and ,praCticei dance With AC43-13-1AChapter ;11; and ChiPter.13::. VI. Weight :and Balance and. Equipment ListReviSed. c411010:0•6%, • EFTA00277944

D OP TRANSPORTATION • FIDE WATI0N ADMINISTRATION am" Form Approved Budget Bureau No. 04—R060.1 . FOR FAA US£ ONLY MAJOR REPAIR AND ALTERATION . • (Airframe, Powerplant, Propeller, or Appfrance) . . • OFFICE IDENTIFICATION 414-4 f5i2 0 er c INSTRUCTIONS: Print or type all entries. See la 43.9; FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. . . , . tita. . MODE! • • • lei c. .10-31 .. • • 1. AIRCRAFT . • sittido. .. • NATIONALITY 'AND REGISTRATION MARK . U.SA. 450ST • . .. . • 2. OWNER show re ;tertian certificate) NAME (As shoWn on registration certificstsj .. ' trekt n Ina. TO ; 18C. • • . . • - • • tea, Teas MOS 1. FOR FAA USE ONLY ... - . . . , ... • . _ . . . • . ... • . . , . ... . • . • • • _ .... . 4. UNIT IDENTIFICATION - S. TYPE UNIT .' • moon ' • SERIAL NO. - ' REPAIR ALTER- ATION AIRFRAME ' ' - • . . , tnynonieisinns• (Ai described in darn I obove)eiNtenn eene • - . • er X POWERPLANT . • . a - PROPELLER ; . . . s. • , TYPE . • .• - ‘ APPLIANCE MANUFACTURER - • AA • O. SONORITY STATEMENT . A. AGENCY'S NAME AND ADDRIAS . _ I , 1 . P 4 D PF SlocsENCf. • a .. CERTIFliATE NO. . AinseardsAvlatlea Ca. • . . , r p__ it. D.R.cORTIPICATED MECHANIC' ' • A/C CLASS 2-3-4 • .. . .. .. 4150 Donald Donlan Dr., • •• • • HAMM FRITHICATED MECHANIC RADIO CLASS i-z-& •4. ..- Long Snobs CA 90400.. ...: _ a_ it ... actitIPICATED REPAIR STATION kJ MITED IPSTR UM ENT 1 _ ,. • • ".. ' . . . • t pANUFACTUREI ' • SioECIALIZkID SERVICE D. I certify that she repair and/or al • ion made to the unii(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- infornistion furnished birein:is true and correct-to the best of My knowledge. ' : DATE 'di . - APB .1: 7 1991: . ' ' • SI • TU OF.A , IVIDUAL .. p • • - . - • • . 7. APPROVAL f R RETURN TO SERVICE Pu suan to the authority given persona specified below the unit identified in item 4 was inspected in the manlpegiptli " y . the Administrator of the Federal Aviation Administration'and is "APPROVED ,CIRR)ELft) e .. • - FAA KT. STANDARDS INSPECTOR . m•smunclutut • . . OTHER (Sperify)' : ; ; SAY INSPECTION AUTHORIZATION • . • /98/ BY DESIGNEE X REPAIR 'STATION CANADIAN DEPARTMENT `GB FAA Of TRANSPORT INSPECTOR • - Pane% • • —‘ I 65 DATE OF APPROVAL OR • ,' REJECTIONApR 1 7 1981 CERTIFICATE .0*-, ' itt oidgiN NO. SI TURE AUT E • IVIDUAL . ,...;..!. . . • • • iiiiilik atillib . -• : rn elbalej*Ir itteN •;.0 EFTA00277945

4 t ."• AA AIRCRAFT RE RA NO. ga, c.Y.1 F • t t ancisa""J".61.2 • • . • * • 0.- . l. . " t • . Weight and balance or operatintlimitation ch ng(ez shall be entered in the appropriate aircraft record. An alteration must bp'compatible with all previous afteeatiots to assure continued conformiti, with the applicable airworthiness requirements. OTICE DESCRIPTION OF WORK:ACCOMPLISHEO (If more space is required, attach: additional'sheets, Identify with air- craft nationality/a0d registration mark and date WorlitomPleted.) installed-on' of Dual Delco Careisel .1VA .TheitiiitifiviistionAiltas .01 74accordance with STC SA4164ME.Ammendeset dated.April,16,..1981_to include,: ' 727-31 model. Flight manual.seD004.11t-idlieed.datede4Pril 16*,19$1e- , ..• •• • It his been determined that theinterielationihip.between these, changes and. - : any other previously. pprovad.ladlii4Otions will_not.adversety_effect.the 44rworthiness 014,this-alraInft • " • . . • • . Air0raft.hli been eeigbed. ileight_and balance and equipient_lief_reirtsud:' .The end. • t( • . •fr V • •4' •••• • . . • •••••$‘4:4?..:•4;;..r.. e . . . . . • • • ) . • • : ::$. I - • • • .•:.'• !. • . $ . . . 975-03.0.7 i7021-14/673-200/ 175 . . - .•• ' . . . • ' $ • • EFTA00277946

- M otycHT OP IRANSPOITATION EI • VIATTON ADMINISTRATION 0 Form Approved Rkiiign Bureau No. 04-RO60.1 • MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY sae • (Airframe, Powerplant, Propeller, or Appliance) 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 foam. 4 MAKE Boeing MODEL - 72'-31 I. AIRCRAFT SERIAL NO. 20115 NATIONALITY AND REGISTRATION MARK USA N505T 2. OWNER NAME (As shown on registration certificate) .. _ Tenneco, Inc.. ADDRESS (As shown on registration certificate) 16951 JFK Blvd. Houston. Texas•77205 _ 3. FO( FAA USE ONLY I 4. UNIT IDENTIFICATION 5. TYPE UNIT . MAKI MODEL SERIAL NO. ripAit ALTER- ATION AIRFRAME • ensonennermenee (As des sr and in item I ekes* nenneeneseinen . X POWERPLANT . \ PROPELLER Tal APPLIANCE MANIOC-TURN -- 6. (ONFORMITY A. AGENCY'S NAME AND ectousS _STATEMENT IL KIND OF AGENCY C. CERTIFICATE NO. G. C. KOLS X u.s. OINTIPICATED MCKANIC Tenneco, Inc. IDISION CIITIPICATIO MECHANIC 16951 JFK Blvd. tionricmus REPAIR STATION - Houston, Texas 77205 '!itiodurAcruant 205-1 D. I certify that the repair and/or alteration made to attachments hereto have been made in accordance with and that the information furnished herein is true and the unit(s) identified in item 4 above and described on the reverse or the requirements of Pan 43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. DATE , • 4-22-81 SIGNATURE OF AUTHOR ZED INDIVIDUAL s- 7. fetfltOVAL FOR RETURN TO sinful ,---.-- Pursuan to the authority given persons specified below the unit identified in item 4 wasNG;ted in the manner prelcribed by at tne Administrator of the Federal Aviation Administration and II ILAPPROVED O REJE ID • ?AA FI IMPCTOT. STANDARDS R mmilm'Acimms A _ IKIETC1/0114 AUTHORIZATION OTIMI (Soma') BY PAA DESIONaTt WAIL STATION CANADIAN DEPARTMENT OP TRANSPORT *4$PECTOt OF AIRCRAFT DATE OF APPROVAL OR REJECTION • 4-24-81 CERTIFICATE OR DESIGNATION NO. 1337480 ' SIGNATURE Of AUTH RIZED INDIVIDUAL A trib-/ ,, • • 5 ife wat ql,,;‘cmuL ii.n.werh•ite).6se‘. • • • • 4;t: • . • ‘••••••:•--• •-: ' • -,.••• EFTA00277947

NOTICE . 40 - Weight and balance or opering limitation changes shall be entered e 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 air- craft nationality and registration mark and date work completed.) .supplempitail tights Grimes Smpplementary,Lighting System installed on wing tips.. Installation was in accordance with goo shop pratices per AC43.13-1A Chapter 5, Sec. 1, and Chater 6, Para. 48 and 249; Chapter 7, Sec. 1, Chapter 11, Sec. 1,2-3-4-5-7; Mfgs. Sp cifications; and Airesearch Aviation Co. Drawings I/1359002°A" (Mephanical) and 01783009 "NC" (Electrical). System was functionally checked.and operation was normal. Weight and Balance and Equipment List revised. Er In-CiOVERIEMEW(PAINTING OFFICE: 1071-77b0211344 tik) . • e . • • . - str—Iste.o•-- ali)t • , ;•-• . • IP • • .--••• ' st. • . .• , • • EFTA00277948

DRAMMEN! SANUORMTION ' -; I fond . Fast AVIATION ADM INISTRANON . . din stream No. 04-R060.1 • FOR FAA USE ONLY MAJOR REPAIR AND ALTERATIONS . • fFta IDENTIFICATION (Airframe, Powerplant, Propeller, or Appliance o Ireg" 4- . INSTRUCTIONS: Print or type all entries. See FAR 4349, MR 49 Appendix katid AC43.9-1 (or Subsequent.revision thereof) for instructions and disposition of this. form: . • . .' • • MAKE ' MODEL . • . . 727.31 - , • - I. AIRCRAFT SERIAL NO. . • NATIONALITY AND REGISTRATION MARK 11.3.11. /1105T • 2. OWNER .. • .............10115 . NAME (As shown on tapir: Varian cartincots) TEMEC0, INC. - ADDRESS (As shown on registration oett4ficote) - UM S.P.A. 11vd. aistapo Tans 27205 3. FOR FAA USE OILY •. . . - . 4 UNff IDENTIFICATION • S•TYPE UNIT MODEI • . ULM P.O. mama . AMR- *WOO AIRFRAME • ... 000nnanewanntren (As dastrisad in Mom tabovA)nortan•••••••••••• • POWERPLANT PROPELLER . '. f . •`- 4 ... : . . . : .... .... .-ta'.1...i . APPLIANCE mAssusAcostA . . . ! • :. • ."-- • •• • • • — --.' . • 101191MITI - • : . . . i. 'SWINT • .. . .. • . " . • A. AGENCY'S NAME AND* awn. ' - ____LLE "ND OF AGENCY ' ' ' C. CERTIFICATE NO. u.s. tastmcstro awssrnc R. S. 4022 A AIOESEARCH. AVIATION CO.; mints« pormauto msatmoc • A/C CLASS 2-3:4 4150 0oneld Douglas Or., a protcatem WAIN VATiON ' RADIO CLASS 1-24 LIMITED INSTRUMENT. . • Lang kith. CA- WIN ki#Numainsa • SPECIALITro Q.re:yrs D.. I certify that the repair and/or alteration made to attachments hereto have Woo made in accordshee with . and thit'the information furnished herein IS true :and• the, unit(s) identified in item 4 above and described on the•teverie or the requirenient3 of Pan 43 of the U.S. Federal Aviation Regulations Correcsto the best', of my knowledge.., ,, ., • • • L • • DATE • . . . . a, • . . APR.0 .3 1981 -.;.: .:: . ... • •• , .. . . . . . i . .... SI R2 A l/ED I DUAL . . • ' • . • . .. ... ." • • - - f . 7 APPROVAL RONAN TO 1 Minoan to the authority given persons specified below the unit identified in item4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and 'is - Ili bPpROVED .O RfilEtttO . FM RT. STANDARDS • INSPECTOR kisv timiusiduna ODOM (Specify) :_ „ • minds:xi Mmtextusnost . BY FAA DESIGNEE ' x • - , . • .• • - REPAIR STATION - cAMa01AN DEPARTMENT Of TRANSPORT INSPECTOR Of - • .. DATE OF APPROVAL OR REJECTION ApR 0.3 199. 1 CERTIFICATE OR DESIGNATION NO. R5 4022A SI0 RE AUTH . . . • EFTA00277949

NOTICE Weight and balance or operating limitation changes shalt be entered iir the ;Appropriate aircraft record. • An alteration must be compatible withfill preYlous alteratiolii to golutetantinued-conforMity..with the applicable akworthineli requirements. • • 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. - Identify with air- craft nationality,antl registration mark and date work completed :Y.: , • • , • • • , Installation of ciaal Delco Carousel IVkilnertintNatigetiOdir!iin accord= . ma with STC SA4104WL Flight Manual SuOOTement issued' deted,June 27..1980. • Installation of dual HF Communisationslysten usiwe'vertioal.lin.loading edge slotted antenna in' accordance Eastern ..A1rlineo RIC MVOS°, Oka* fOr. the. following deviations: . • • • AAC prawing.1418108.7.HF .;.1.Ostme CeStrOl Head Med. MC Draidig161019r .2' Ostia PAM Head Nod. It has been deteriaineethat'ths iniarrelationiblOibitween theie changes and ant:! -- other previously pi:proved modificetions will noCadversely affect the air- -- , worthiness of/this aircraft.': !*:, . : . . e ' Aircra ha been weighed. Weight.and.Belenee and Equipmint Litt anvil:ell , - . • • D OHM' SHEETS ARE ED ATTACH . • • : 1" hAi. 011 _NIENT PRINTING 6PPi:Ei'lliiii:in.021/780 -': • EFTA00277950

r . , DIPARTMEhilit TRANSPORTATION Fenn Approved Blke! B.:tram No. 04-R060.1 . . FEDERAL AVAWE ADMINISTiATIOt4 ,. FOR FAA UP: ONLY • 7 -------• ' =.- 1 OR REPAIR ANDALTERATION .' • - • OFFICE IDENTIFICATION (Airframe, Po nf, Propeller or Appliance) 41-e t'500 4 al INSTRUCTIONS: Print of type all entries. •See PAR 43.9, PAR 43 Appendix B, and AC 43.9-4. (or subsequent revision thereof) for instructions and disppsltion of this.form. - "' Le log MODEL . •• , • ., •-•.::: 727-31 ...-. I. AIRCRAFT SERIhrti . • . Pitierify Afi qrTitATf N MARK 1. OWNER NAME (As shown 'on registrotion.cortikotol .:.17779.5 TOMOS) • ilIC• 7 . .. ADDRESS (As•shoWn on regi &ion certificate) John F. Blvd. WHIST:Ott g T 1 . 14 . 3. FOR FAA USE ONLY .• . • ,. . . . . ,. . . , • . 1 re data identified: herein compliei with Appli • , • . • :, airwoithiniss requirements and Is approve liforabou • .. . . • .. . : :.-.;,...• %, “.. • . i described aircraft subject to Conformity, 1 p.edionby a • • perio uthoriied in,FAft 43.7... • ' • • •• eca/d (icey, A4-efirieor,....attab% /e lc' •: , . , . . • • 4. UNIT IDENTIFICATION - - • 5. TYPE - 'UNIT , . • MAKE - • - SERIAL NO. - . • : - IIEPAM AUER- ATION AIRFRAME • • . ..enewomengeoesee (As described !known I ohowt)swaimenneemene : - POWERPLANT -...,*. ' ..; • ‘ 0.:0-1 PROPELLER . ••: • . .. . - • . •••• .4 ins • ' • . . : . . . ,.. • , .. • .. .. APPLIANCE MANUFACTURER * trielltr : I 4 ( . . • A • • ' NT CONFORMITY STATEMENT . . • • A. AGENCY'S NAME AND ADDRESS -,r• . - : - B.' KIND' OF AGENCY : C. CERTIFICATE NO. „yr AiRe lt searcb Avtatlon Co. . • • Y.S. u.s. nitSATEDatECHANIC . • F. ' n. s. 4t.)24 A A/C 4150 Donald Douglas Dr. . . ICIRElpi CERWICATED MECHANIC :. •:. ' CLASS 2-3.4 RADIO CLASS 1 Long beach, CA 90808 CERTIFICATED REPAIR STATION -2- LIMITED INSTRUMENT• • MANUFACTURER SPECIALIZCD SERVICE‘ ji U. I certify that the repair•and/or alteration nit 'i to attachments hereto have been made In'accorderspe with and that the information furnished herein is true and -... the unit(1).identifieci in item 4 above and described on the reverse or the requirements :of Part 43 of the U.S. Fedeiil Aviation Regulations c EMI to the best of :m leukaalerlge. • . . . . • DATE • APR 03 1981' ' • SIG ... TU AubtraR ,,,, I :. tt 7 ivioum,, . • ••. I • . 7 pPR0VAL AR WORN TO SERVICE • : • Pursuan to the authority given persons specified below the. the Administrator of the Federal Aviation Administration and ‘n:t Senticed in item 4 was inspected in the manner prescribed by . is laAPPROVECT OREJECIL.3 , FAA Fn. STANDARDS INSPECTOR MANUFACTURER ' imPtcylori;AsamotaAnoi4: " OTHER geerifit ' . . -.• • BY FAA DESIGNEE X REPAIR STATION CANADIAN DEPARTMENT _ OF TRANSPORT IKSPKTOR OF AFT z• , - t. . DATE OF APPROVAL OR REJECTION APR 0 3 1981 CERTIFICATE OR Rs Des 40 ioN 2 A a IRON NO. SIG .?T • , i E HO IN IVIDUAl.. .- • - E • il . ..• FAA Form 337 11-67) EFTA00277951

• a • ........................ Wegfp... Nil • IcL) NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible. with all previous cilterations.tO assgre cobtinued conformity with the applicable airworthiness requirements. ' 8. DESCRIPTION OF WORK ACCOMPLISHED (if more spare ii.required, attach additionarsheets. Identify with-air- craft'nationality and registration mark and date work completed.) — • • The fol owing 'systems were installed complete and .in accordance with manufacturer's- speC?fic ions; ACCS-32 all sections; AC4;3.13-2 Chapter- 2, 'para.• 21,22,23, Chapter 11, para. 1182, 183, e,f,g;--AC43-1A Chapter 16, sations 1,2,3;4,5; AiResearch Aviation Co. drawings Di. 1500553 avionics radio, DL 1600562 avionics elect and Hill Kennecky. DER FAA 8110-3 data Dual Collins 618M-3A coma system • • . Dual Collins 51RV-1 VHF navigation system. 7 Dual Collins FD-109Y flight director-system..J.1.i. Dual Collins DME-40 DFIE system', _..* Dual Collins TDR-90 transponder system':.'_. Dual Collins DF-206 AOF system_. .. . • . . Collins FPC-75 groUnd proximity warning systaa vo Collins 54141C comparator warning. system _ Collins 51Z-4 marker beacon system ., RCA Primus-400,14XD coloradar system , Wulfsberg fligpkfone III air. to ground radiotelephone • • Flight Instruments: 2 IOC 521-28007005 servoed encoding altistetets 2 IDC 422-30510-130 static_defect corrector_and SAT/:TAS computers.. , • 2 IDC 575-25820-739 mach/airspeed indicators. . • 2 IDC 513-24660-101 TAS/SAT/TAT indicators_ ._ _ . . • 1 IDC 540-25100-001 altitude alerter. • 3 Davtron 8118 digital clock/flight .time recorder 2 Collins 329B-8Y approach horizon indicators., 2 Collins 331A-96 course 'Indicators .Rosemount 102AH-2A6 dual timperature probe, Cabin audio entertainment system, .. , . The following systems interface and wiring_alsti initalled in accordance with AC 43.13-1A chapter 11 all sections 1607032 shaver outlits, mod . 1608092 utility outlets,.ftld cabin . 1608093 utility outlets aft cabin' 1608099: service outlets, mod 161013' ac power distribution, 161013: ac power galley, service;' , . 1611031 Freq.conv. static 115 vac, 60.-HZ 1636212 dc power distribution 1668006 engine oiler remote. pimp . 1683354: sch-electric oven, mod (Jena-Or) 1683355 electric oven, mod (Jenn-air). 1683371' galley, IVid unit, . 1683372 galley, aft unit.. • • . „ *19764".0.-1703-1.1/673-1104,175 r • .4 • EFTA00277952

; The following systiMsinterface andwiriagalSo installed in accord#oce.with.AC.43:.134. ,,..chapter 11 all .sections: • 1584011 sch-pniO, zone air cond, - ..„. . 1684012 sch-ckt, air cOnd.:,(zone temp,:cont4. 1684013 ...:sch-ckt..air.COnd-,,(00rhe0Jlont.) .. 1685073' air'Cond.zohe tem0_Ontrol: . .1687047. air'cond. sensot.fons..:::' ' - 1692234::' . water blister, galleY.C184::.:..--- -.., 1692240'-- water heater, maStee.lav::20 gal:. 1092241. ' water system line_heater0+NC.::... , 1692242 '. water system line.heaters4-aft„. 1692316 water heaters; laVatories; mod.: 1700040 - '..' vent blower galley..... . ; 1755039:--: air cond. zone temp'....indicatign.... .,_ 1782110 : • a-We-lights, tabin....,. ...-.. , • • • lights - ,.. 1784137 ' storage compt and closet lights...,;., 1789059 - . ceiling its essential power • - 1792150 - cove '„lights, creVi„compt, ' ,..,..„ 1792151 cove lights, galley...:.., ...._ • .,.... -:. 1792152 cove lights(' lounge, 7- ... 1792153- cove lights, fWC*.sttite.room ...... 1792154' ceiling & read Its.:,trew compt.. 1793268 Ceiling tts galley,,. ,.... :—.... .... 1793269 ceiling & read Its;.lounge----..:7,. 1793270 Ceiling & read...lts,.flitd stateroom 1793271 ceiling & read...)ts...oft stateroom 1793272 ceiling Its, aft)lavatOrY ' - ,.....: 1807045 table lamps cabin:..,. .„ . ..;... 1808212 . thoWer fan/ It &J.drain_valVe ..,. , 1813061 panel ltg. 3rd crewman's . ..„.:. 1813062 switch & panel ltgi.cabin ,....i:,..- 1821059 ceiling its, fkl.vettibtile . . 4-...0i,,........: ,...- 1821060 ceiling its', aft ;vestibule r,,,I.-.... . 1824242 work & effect its, lounge bar, :. - 1824243 vanity lights. aft:vestibule,.:, . . 1824244 work Its, fwd and.aft.attehdagt's. 1832400 . attendant's panef. fwd,vest..... 1832401 . attendant's pane1.9010 1832402 attendant's panel aft vest • 1832103 vanity disconnects, laVotorieg s". 1832,j.04 circuit breaker panel. 0114n% . 1832405 circuit breaker.panel,,mid cakin.„1. 1832406 control panels,-„cabin.:. , .2-- . 1832407 electrical equipment.:instl. g4110: .. - . 1832408 electrical equip. inStl, mid lapin::. .: . 1837026 spare wires. electrical.: ....-. 1838211 electrical flusk.toiletS. 140(1,,,,: ....... 1838212 '.drain valves water,syttem .,..... .., 1838213 air compr.• & qty.i0d.,water system:: 1880028 air cond. overheat' control 1883071 emergency exit ltg,.mod 1886193 call system relAy.assy,„: 1886194 call system cabin .:..'.-:... 1886195 call system crew..H.... ••• . • . „ . . . 221141V ..;!..fa*•••!,.,,j, „atg_kt., „i;•;212.%:;, ., t-uz.k.z.:,:eir,„;.;;;;,. • ••:. • EFTA00277953

• • • •• . „ : 147:417:5N"C• Wilk ” . grz. • • • •••• • • • • • • "*.. - • • . , 1. • EFTA00277954

The following systems.interti a and tiring also installed.in()cordance chapter 11 all sections:, . 1887205 '' passenger warning signs.. ,,..„,... 1888050• smoke and flame.det...sentor aqt,i.1. - .1888053 smoke and flame.det. bag CoMpt. l.': . . .__. 1%1388. rad'o power feeds 150222, , radio.lights _. ,-...,:". 1503178 ' ADF-i system OFT.206.,4:L. 1504137 • . ADF-2 syttem OF206..„::_. 1505284 NAV-1 system 5181(71,t_ ' 1506266 mV-2 system 51111144„. 1507304 FD4 system FD-109Y 1508276 FD-2 system FD-109r..-:.. 1509281 DME-1 system DME740-,,,;. 1510184 DME-2 system DME1-40,.., ,,-. 1511058 DME indicator 1-.... .:. ' .1513193 marker setem 012!74.,:..:.:, 1514066 Selcal symtem 45SC.! modif "__ .1515205 VHF-1 system .610-38516207. ._,- ,. 10.6207 VHF-2 system 618t1-3A ..., .,.,.. 1520127 flltefone sySiem , : ,,..4;-.., 1521225 atc system tdr-90 (dual) v.-;.".. 1523254 pa/inph (modif), •••• 7 1524057 stereo system (cabin). :_. 1525090 tv;antenna (prbv). _ 1527211 cockpit audio (modif)., . 1529137 comparator system 54W-1C : „..:_ ..... 1530149 weather radar primUST400. • . ... ;._ ., 1533204 no. 1 radar• nitimeter ale-51A, modif 1531205 no. 2 radar altimeter ela-S1A.(modif) 1535205 autopilot. systen.interface . 1536231 comp-1 system interface. • 1537221 comp-2 system interface, 1538174- altitude system_interface. 1541186 ins-1 system CIVA. . ..: _ 1541188 ins-i system interface,. 1543187 ins-2 system CIVA. . ..,.., 1541189 ins-g-syttem interface. , 1544264 1.h. altimeter/alerter ... 1544265 .r.h. altimeter indicator 1544266 stby altimeter indicator 1545117 Mach/airspeed indicators 1547116 1.h. sat/tas system,...., 1547117. e.h. sat/tas system..,.L 1548034 scat system (modif) 1549249 annon system _ . .. 1550178 .reco accessory box .. ......: 1551077 digital clock system .j., 1'552007 oat indicator (modif).:.:',,. . ,„-._ 1557091 data select system ,. .., •.%. 1558010 rate of turn system (modif) ,;,. 1560020 GINS system (modif) . , ,,_ . . .1571017 ins relay unit _ .._._ ',, 1570028 nav relay unit ,. . v.,;,..; . 1592046 annunciator cp1r.diagram ..,., :,. 1594097 cockpit hf/inph_control. . ... 1594098 cabin flitefone/inphooatrol .-.%_. . . EFTA00277955

. . rev m-t‘ • • 0747.7 . 7.777WWTT•ii • • . . . . . . C's,s24,1rtatT 3/4"-• .'`‘'.1)••••• • Vti 7:56175771-Prror P.:c7,eirart . . 'POSIR01.4sIt.4USWitObOlVV-0347411qpus 446tek epatlem 3424340i £'L5 •. • ti plot 3Y aspi43 vart -•Sdigt ' 6'I8. ti pvai'm cannin tiltUAOU itnoi •sdam act Si. APedt3-00 iv=o1 129', ppa `SZO-Vtatreff 3t1 amigiu0339 u4 6ZL£-3 vu od so3 uoirti:mt tpasianny Jaalipso wag Ivy spiting plot 3v-30 tvoI.4oat° liv EFTA00277956

• COARTATENI; ! TRANSPORTATION ' . ; ' I r: 1(..' FEDER.4. AVIA ADMINISTRATION Form Approved ' Budge Moreau No. 04-R060.1 • • • ' • • . FOR FAA USE ONLY . ! - - .'MAJOR . REPAIR..AND. ALTERATION ,- (Airframii, PowforploSt,,pfcpollfr, or Appliance) . i • . leFICS,,ITTIFICATEI:ls„.....--• INSTRUCTIONS::Print or type all entries. 'Sei FAR 43.9. FAR 43 Appendix B. and AC 43.9-I (or subSequentsevision thereof) for instructions and •disposition-of this form. • .• • . ' ••• ' MAKE hImalf/e31 ., • 1. AIRCRAFT SERIAL NO: . ' ' 20165 . NATIONALITY AND REGISTRATION MARK • . - NA I605! . Z. OWNER . NAME (As shown on registration certificate) L, •. 7 . .. ..teensa . ‘ sate ' ? - • - • • • . • ' „A - • ADDRESS (As shown on regidration certificate) 11796 ASA. 91vd. illestos. Tees 77205 .. • v FOR FAA USE WILY • -_:.....: .: The airworthiness _ . iascrib .... ' Pe . _ data . . . - • • :We . ntitied herein. complies. with Applicable .. requirements and ,Is approved- only for above .. • • •• ' , • aircraft subject to conformity inSpection.bya. • • :7 - . . • -• . thoilze InTFAR 43q.' 7.- . . - ,.. . .. ._ • • • . • • -:-, 4.-a0756471TSIT IDENTIFICATION -S. TYPE • UNIT - ... :,...„.:,,.;,.. . • • • • - • • '. • .. , MODEL SMIAL NO. 'REPAIR ALTER- ATION . . . . . . , . . deals:it:di; iti.trik abiwOniiintion . . , . I AIRFRAME • . nenninentieeiwiie (Ai . .. .7 . POWERPLANT ., .. . .. . .. •• . ; 2:17:::: .: . . • • . . • . . . PROPELLER • i ,_ .. .... ... . ‘...7•:•-; ' e.1 1-1 • • g • r .. • ' -• ' ' • . . .. . , . . . • • • • • - . . . , • ,. . . . '' APPLIANCE .• t' . MANUFACTURER ' . , . . • . - . . . . . . • • 6. CONFORMITY STATE ENT A. AGENCY'S NAME AND ADDRESS • -• • • S. FIND OF AGENCY • C. CERTIFICATE NO. :.AiRosaarat Aviation 0. : •• :, • ; , L-..; .1.. '': lk-SZIgetICATID MECHANIC R. a 4022 A :MO Oonalot Onolos W.- - , - - . , •.; _;i:,,,;_., ., !QUIN' ORITIFICATED MECHANIC • A/C CLASS 2-3-4 RADIO CLASS Long 9sack..CA 90000; • .. - . .... .; „. • ,..-, 44IIIITIFICATEDtEPAIR STATION X-2-3 LIMITED INSTRUMENT .' , .7' •• • ' , •—• • • • ' • tent4U1ACTUItIlt• SPECIALIZED • SF ITT V I Cr . . . . ., . ...- . . • . .- • • . • . 'I D. certify, that the repair and/or alt ion made to • . attachments hereto hive been midi iti accordance .w1tb.therrequirements ' and that the information furnished•herein is true and ._ .. the anit(s) identified ici•iiem 4 above and described on the reverse or of Part 43 of the U.S. Federal Aviation Regulations comet to the best of y knowledge. • .__......-- DATE . • .. • A R.:0.3 1981 • - :!... •• . - • . _ S D INDIVIDUAL• .n.... .. ; :t. - . , 7. -AfflOYAL FO lETURIF TO SERVICE Pursuan to the authority giveepessons specified below.ithe unit gentified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administrition Ind is • -APPROVED 0 REJECTED R , • FAA RT: STANDARDS INSPECTOR • MANUFACTURER — • - . • • ,• ,• .. •... : - • . INSPECTION AUTHORIZATION - OTHER (Specify) __'..- — ....... . • . - -- - .. ...— BY FAA DESIGNEE _ I - , , • REPAIR STATION CANADIAN DEPARTMENT OF TRANSPORT INSPECTOR OF . . . • • .. - DATE OF APPROVAL OR REJECTION . ...- . APR 0 3 1981' IFitil CERTIFICATE OR. gthigION NO '• sagar i • :. SIG • .It . I . ,-. ... I.: ,. t • :; • ` • e ' .-;esedi•-•;&*-41111‘..w.i.:;:,;:---en.• ..-- . . . ..• . . .. ...., . ..fleSatalialharairiEt • S"‘thrivoi'v 1 irilci'v '-'-'' 'r -- - # ••4" 2L.elarair:az - i "4" .rA.. . 1"‘JI / °'' J ' ''' LAI 1 .,.. 4,14L, ' •.. '•'../it -` ?ILL'S" ••••":2-7.11,:t -' '.7..-:-.:"S• 1 .: .iPix....—•-z...!t. - ' :4_::..!..C......s....1. 4.-sec.:(-2-- '-`...:t1/2? et 1.5.7.V.` •—e: -..:. --... . . EFTA00277957

NOTICE . ". Weight and balance• or, operating limitation changes shall be entered in the. appropriate aircraft record. An alteratiOn must be:compatible with oll'previOtis'alteiations to assure continued conformity with the applicable airworthiness requirements: 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space .la required, attach additional sheets. Identify with air- • craft nationality and registration mark and date work completed.) 1. Inslpilled .the fellowtagAw:acortiance with ACCS-36 ill _sections. M43.13-2 chapter 1 Para. 1:454-.7-8-9-104142 AiResetrch Aviation Co. drawings, 11.13011611 401,1_ 1 analysis contained in Howard Pattervon.. gei 1102034 Installation table•Cocktell, !atria f/O2Of4 110244- table,-cocktail _ 1102046 ° table, cocktail wt:folding leaf •- 1104065 ' table, foldout • galley 1124232 " divan. r.h. 3_ place....„; ". 1124235 6-divan, 1.h. 2 place berthable 1124236 divan, curved, 4 place,_ 1124237 • " divan, transverse:.3.plece_ ___ 1124238 " divan, Motels. 3.place_lvd, facing 1124239 " divan, riviera, 3,21ace •ft.facing - 1124241 " kibitzer seat 1130090 6. closet/ desk. 1130093 clospt 1.h. 1130094 closilt, linen 1130096 6 clu coatroceicart 6 1130097 ° closet linen, 1139111 ." ledge 1142171 ° cabinet, refresiseigt.,_ 1144127 6 table, with folding.leaves 1146114 ° pull-out- table 1147184 ° cabinet overhead 1147185 " cabinet overhead 1160200- " fabrication bulkhaid.and.iloors 1160201 'Fabricates turn. panels. _ 1160228. FabrjgatleVniltkondAPOd.iiiiidi ills - 1160233 Installati nift•mitioeid_ _ 161-STD-052 Iestallation std.-blowout door eeilkultheat prey. 4164038 InstagiF on fittIng,..tnathead ti0418100. 1164046 ° bel and partition_uPPor 1164050 ° parti ons• eind.efet • • 1164052 ° pass partition and, attoch. 1165470 ° galley, r.h. frd,feelacing, 1165478 ° galley, r.h. fid aft_f4;inie_ 2176173\° cabinet. vanity wi..gggt... ....__.. _ 1176174 I cabinet, aft lay... 1214196 " shower - - ' • 'I 1214200 "" aux. water tank 1214271 " hot water tank 1214329 " aux. water tank, aft.. 1220153 ° pallet, single Mt.. 1220155 ° pallet, single seat„ 1220158 ",pallet, 4th crew eieber_ . 1220159 6 floor support ends pallet .!tDDMOtiefil SHEETS Ald ATTACHED . . . • EFTA00277958

• 2./' **stall« the fuliculagi ta$44, eltsactläni and Ailkisaarch Mislike Co. : • . i 1245409 • Ploorplan • Intall4101, 11 11:1 9$ a. ALIS« sats :In ralstlao- -N to aergancy snitt 3‘_ oZ_stalled the follaul_8$ 4.1'082 all action.. 4b.353 Slø 202, 203.'204. VIL 206 (b) si 12g;17 44994å-tiOPSitplist-,f.likift. Instsliiitiiie"1;11‘1-ag 1b accortissicamith ACC5-32 all .sectias sACC5-33 all action. AC.43.13,1A depter 15.sect,..14-3-4-5 dustar 16. sen. 1-2-3-4-5. AC 43.1.1,2~ir 2. para. 21-22-23 tastar 3. pa 31-33-34-35-36-37-38 ad AiRasarch »Idiom Ca. dralon", . • • _ . 1410337 Layout- rodio rack EL 1410338 Layout - radio rad 14.,25. 1425272 kutal 1 dim fli telen motane ... 1461190 lostallatiou wasther.nar.rit sid.aat. 5. Installa da sofrotrustural,Itatin.acconlact with etui .*11233259 181405 :4191198- 1401205 1411225 3I4+18COg 1449004 Installation- air.ictuator.sotasi • flat calling • -. i Layout instnnont Layout control 'hal Nodification pitotistatic, layout- radio controls. . Installations. snor total _to"- layout overhead panel Lanat flt effir. Itation . . . -•*wre;e. '-• •et.....,.:.•-_:*-- .... • -•-•- :•••••-x-, - --t • • . • . . • • . • . . . ...: , ••%. • • • • a • • ............... . . ..t.:1. eMiLLISId 'it ilti :SaL‘• :.4,.2..'. ?.::-ir..1 g. t.".? ". .1a.• . L ..... . 4. :1,... - SiSilik Datia•SikAiC :;“2S :" . aNtS"... t.:••• ... " . i& ..;.k4,...&-I.S.:: ....:. ...:......:..: • • . • EFTA00277959

.r 凋 」 l i l ］ 凋 ］ } , t . ？ 翠 譬 对 割 胃 剖 叫 到 恫 4 训 翮 阁 耕 ， 捌 劃 踊 啁 制 1 嘉 渊 ＄ r 滅 瑚 蟈 萋 劍 斟 目 凋 辆 爿 淄 封 1 － 直 雌 崢 蠻 瘫 ， 廬 ． 蠱 濞 ~ 剋 薯 I . ； … … 一 ． ＇ 鯊 亏 ＾ “ 餐 h 凸 妒 y 翻 1 \ , ＄ 毬 t , i 曳 辐 扎 ． 』 密 箋 槛 跋 氓 P 舌 广 ‰ ． EFTA00277960

I MP' • , . •O11PARTMILNT Olt TRANSPORTATION ' FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIF CATION'- DATE , • APR 0 3 1981 ' • MAKE .. ' .I MODEL NO. . BOEING - ..727 -31 I • . TYPE istiriNany. Rados Nolthoptyr, NAME OF APPLICANT AIRPLANE AIRESEARCH AVIATION CO. „ 1:1$T1 OF DATA • IDENTIFICATION TITLE ' I . C-3825 ' . C-3688 :.-- DL -1300517NC . . .DL -1400319NC . g • . ...... -. .. . • • . . . . ., • . :. - . . . •-• • • . . . . r, .. - . • . STRUCTURAL SUBSTANTIATION -Interior Installation TENNECO, INC. 727-31, S/N 20115.- • . ..- . . • ... . . . Weight and.Balance for S/N 20115. . - • - ... . . . . . Data List. -Anterior FUrnishings: Data List -4iicionicsitiech. .. ... .. .. , . • ti , • • -• •• • . with a attached found .. -for ... ' • ••• • , ..• . • . • • • • • • •• . , . . , . , PURPOSE OF DATA Substantiate BOEING Final Aporoval.of the APPLICAOLIE. NEOUIKEMENTS ..- • - CAR 40.202, 4b.301, • CERTIFICATION • Utder attlaity •of appointment ender Part 183 have - • . 727 -31:InteriOr Modification..on N505T Serial ModificationW111 be made bilAA. • (Mot immeMS• nallono) • . . 4b.306 4b,260, 4b.358 and 4b..101' vested by,dinetioe of the Administrator and is oscosiosso of the Federal Aviation Repletion. data HAMA abiove and beet imuohisd is accordance with established medium and Aviation aestiathas. • • • • .. apPrivsl of thesiidis.: • these data • - '. . . • No. 20115 ONLY. . --. conditions and limitations Amos numbered to comply with applicable .. • . • • . - • lectuiremeats of the Federal DI Recommend I Ai/Therefore • • 01 Approve p EN0A SIGNATURE(S) OF DES NAT ! EERDIO RElItESENTAIIVISO all1SIONATION II IMIIIERSIO CLASSIFICATION(S) ,d.A....--...:_i. i Pa s 4. WE-663 • STRUCTURES .-- - ' , - -------- FAk Fore 8110.3 t trio) sissaftscoat *ominous EDITION r•n;Aiki_g41..€71:tafit t-•-: • n °. • ?....:26t (?;.249 e- hrj r Ssieditgas",: • • • EFTA00277961

3-%ra.,;•,. --, • - • -• • • =a= ‘41:itlaL.IctiCt ;"1 ;,!• EFTA00277962

FEDERAL AVIATION AGENCY tutPoLiCatitliFOR AIRWORTHINESS CERTIFICATE IFAR 211 ' ' : DISTINCTIONS' Print to type. Do not Willie in shaded oracle/ liwo ors in FAA um tidy., Submit original only to on su- thatind FAA Repro/Malin. II addltionol space b required, MN rano tide. _ AC o -t I. TION MARK 93 0.3 2. AIRCRAFT MAKE Boeing . AMOLA/7 MODE USIGNATON 727-31 <: ti, 4. AIRCRAFT SERIAL NO. 20115 ' 5. ENGINE MAX! .Pratt & Whitney 6. ENG0t MCGEE DESIGNATION Jilt - 7 I . . 1. v. 4' i .., 7. NO. Of ENGINES Three R. PROPELLER MAKE NiA . 9. PlOPELLER MOOR DESIGNATION IVA I0. YR. ARC. FACTUIEED 9 : 2 z 2 A. APPLICATION IS HEREBY MADE FOlti 4 X ORIGINAL CERTIFICATE-AIRCRAFT ES USED IMPORT 4 AMENDMENT OR MODIFICATON OF CURRENT CERTIFICATE ' . f OTHER (Specify) B. AIRWORTHINESS CLASSIFICATION (For mtmitifris ansfaaa., deal affmcriate ids° I, X t STANDARD (Indicate canary) NORMAL UNITY i ACROBATIC X TRANSPORT LJAUTED . RESTRICTED :14 ACIRCULTURE • PEST CONTROL AERIAL SURVEYING a."' ft • *SAL ADVERTISING .4,(ladicate (fereitios(1) FOREST (Wild Itfe cossersatin) PATROLLING i> WEATHER CONTROL % * to be econfiected) OTHER (Specify) Ai, EXPERIMENTAL RESEARCH AHD QEVEtOIMBaf AMATEUR BURT i.; EXHIBITION r. (Inciirate opn etia(r) to be cceedocted) RACING . TO 940W COMPLIANCE elte. WITH FAR tis.'sits NOV/SIGNAL (Indicate dais) mos I CLASS II g F g sad tl O A. REGISTERED OWNER (As than as Cat:fiats of Aircraft ResirMaraa) If DEALER - CHECK HIKE .1r X FLAME The Boeing Company ACCESS Maim Oren, (My, State sad ZIP code) P. 0. Box 3707 Seattle. Washington . _ 98124 B. AIRCRAFT CERTIFICATION BASIS AIRCRAFT SPECIFICAlON OR TYPE CERTVKATION DATA SHEET (Girt NA. Rev. No.) - ASeiB. Raves 1 6 AIRWORTEIRESS DIECTISI SUMMARY (Gin- year ;968 69-12 sad 411 card No.) AIRCRAFT LATINO (Gin page WO) • b. SLPREMENTAL ME 'CERTIFICATE (Giro No(i.)) C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS ,... X AIRCRAFT NEW—NO rtnictil .-LLSTORIcrN TOTAL MINFRAME 14O1)15 RECORDED RECORDS MAINTAINED IN COMPLIANCE WITH FAR 91.173 ?:25 I the hereby certify that I am the registered owner (or his afar° deist aircraft described above; that the aircraft is registered with the Federal Aviation Agency In accordance with section 501 of the Federal Mink.° Act of 1958, and appii Aviation Regulations; and that aircraft has been Inn and is airWorthy and eligible foe the cladailication s DATE OP APPLICATION NAME no nut (Priest or an.) SICK* JUN 6 1969 R.C.Ctuti 88 aillerthiII ell. . X' z gr Li A ; 1N ACCORDANCE WITH FAR 21.183, THE AIRCRAFT DESCIPMED MOVE HAS KEN INSPECTED ['FOUND AIRWORTHY BY: • t-- ,a.t CERTFICATED AM CARRIER iF (Gin C.ertificate NA) ₹ (GIN CESITIRCAND MEOULNIC DA) Crstifcam Na) CERTIFICATED DOMESTIC IIPAIS STATION (Cisco Cute No.) - iC AIRCRAFT 4' MAYARACIURER (Give mese of firs) ..- alit OPUS • .4,••- :,. ,. .. DAM ' .. SIGNATUE MOILV LNICOG SEINIMINICVAIIIV 'A A. CURRENT OPERATING LIMITATIONS AVARAIILE IN AIRCRAFT X CI. THIS. NSPECTION RECORDED IN AIRCRAFT.EO0RDS . I. CURRENT OPERATING LIWTADONS ATTACHED 14. STATEMENT OF CONFORAUTT, FAA FORM 317 (Attach itb.en Trquirrti) X C. CURRENT APPROVED FUGER MANUAL AVAZAILE IN AIRCRAFT I. nrnous APPWOPTHIMPSS CERTIFICATE ISSUED IN ACCORDANCE WITH D. DATA, DRAWINGS, PHOTOGRAPHS, ETC, (Attach cobra required) )4,4 CAR (Orrg at:abed) X E. CURRENT WEIGHT I RAIANCE INFORMATION AVAILABLE R4 AIRCRAFT F. AIRWORTHIPR,IS CERTIFICATE ISSUED IN ACCORDANCE WITH , E. MAJOR REPAIR AFC ALTERATION :FAA FORM 337 (Ansel ears req.) X 21.183(a) FAA) (Copy attached) 4 - g X A. 1 have inspected the aircraft described above, find it conforms to ks type crailscitt. and b in condition for tale operation. B. I have inspected die aircraft descrthed-above, find it Is In condition for NSA experinatual operation. . 4to / 11 4 C. Current Airword3inns Certificate amended. OAR 1. t - b 9 0 / 7 June 30, 1969 DESIGNATION FIOz) 6 DMIR (42129 OFFICE NO. t3ICA ASDO 24-0-46 ' F . 17teira7 .491// ) 41-2 9 3 W.A. O'Neal ••• ataeztgRZamt,...., nom. • 211.fis er.,&:$c-e$ • EFTA00277963

. . At!-- • 11 • • . . • • • -•-••-•^ -•-ws. • .• • -.Wr.'n7.77c.AW7•c*Th'..g.. ..n.771.1.71: • c9,-•• •• • • . • . ernm...••• ••••,•+ • 7 ...7 7:••24•••t.,10. 1-Mtap ifittrfiegiraa,f1-:*-`1Wir.o.f•k• • . • . • • • • • • Z • p : • t.i.•f K i .1 ' • .. ; r' N.:I ......".., • \ ZiN t,•`• .. C.:•t•e :I' •,..:,..'.1:;.1:.'::, _ . c .5 .1 Er T ii,t in, h't '••••- .1.4`' -•F--:1•''''.- 1/4. • ..2.- tn..' 'LT .P.:2"L'.... P... fit..."`n—I.5.• ,:; ...- ,... ' , • 4 1• l• ,1...3 t:.3.•,,. ...... . - fly,. :. . ., r. . . ....“. ...............m.y••••••••m....... -- - - .. - , 1 2 - ..„. •• ..„...... •• ._...,,,, A. r. . ., • .. ." i.li .4. • , ••...1...•.: • I.- • • ...• •• m• b.* • • • -. _ • tit S r ••• 2.0 EW. ,:•7"1.11014,:re 'Il.1.7::, 2 -, .., '.." _ , • - 3 r. • -.1•12;Zi-7,:rt,; •cf • v. cr.; I ..• :c. i • j Oh oap I WIT ' 1,1 - ▪ ..;" ••• It r. :11'...r ..,. i . cot . . : .. . ::-.7 ...: . i rt L.; ... 1.. : ., ••::::-..:•(::. wlvt.:...-..:::.:::,.;:.,-.....-...7-s. ‘',.... .., i c 4.'1 M. •' -; .... . I j..', fi rl i t's Iii•- •': • 7 El: •!'' . 1 .7.2...,..k‘.7:i0 4: r..-.11/...f., ; ; 41.. - ”- • ••••fietiV, .\ • . 1.%t" Cr;;...? .4:••. ti.q...1" -.. i..• . ...:- -_ .. -91w.C.--,--1.. ..,• .' -.1;:c.•: •- ''' •1 • -:' ',E kW P-G9 1 " - 1 . . s ) e4.-' 4 .. . _ . ;,., 1 •:. . .,.„:•!, ..,„ .„....,:,-, • • -kt — z i . • if; tti I. • C' - Lf 1- 11. ' . IS. C *C.:fir-Cry. V ;trio •,) - Tuses warrartst . west vf.teltrc.72.103;L:- • . ......' --. . : . : '. ...: 1 .. •-• ' . 4. .-.JSCI • V•tij:30111,911.%/kt. tij P:C.:9.. , - . . ; • - . '. f ;-... 1 • , •fl Z ./C a. tiliat i lr4IIII ASPr us Hitil ;:i . 1."..L". ‘a ;M : C:117 P;." ' .:- “.) •:. V•G :...‘ZciVic.r•Z 1.44,1 F."...Z . • - 1 , - ; - -•••••-." 4!" %."1 "'el . . . . ? 9.11•3, A CCZilil. G+[[ : ...::: I ! I:" • • 7 "._ --' 00 4. • .,. . • L t 0 103.4.13 el in ea . 4 • . • i - .,i-Osf.R • .• ,.... . , . :as.", 111;410 : • - -- - - - - COINg.1A8CE I: it.F.0 Iti T It .. FAA AIRCRAFT REGISTRY .__ _ _..... . . ... _ . . • . • r ou L r r • • • • OKLAHOMA CITY, OKLA _ • • , f J • ' - • C ...."- . 1 ...t ! Ir VfliCt :O. O::::., 1:',...... 4. •'1, •• • ..: • : ' ' • ... • : '. • I t'. '. :' : :- 4 i.••%:, .: .. . .- . ..... . . . • . . , . . . . .. . - I: •i: I 1.; i .5; : I vi,.."..-1,L(i..p.:::7;,1,o,;•• ‘...:".•-::-N, • • •:iv• •••;.:1 ,.. .: i•...7••;S r.;••::1; , •".;.1 • •4; In)....,'.;/ :::: .;.• , . 3: r- I ' •it.:C1 et.: ..•-•:•.III:"."••:- • " ' ' " : - ' • • " - " ' . 4; .7 "..; .7.: , . •.• :v.1 , .• •- •.::!' I I . • I 1 1.'.`.. Zr.) ', J vilic.".-,44. ay.•::.t;;;,.., 7 • , ,,••.:,77. --- ---- • -------- -.----7-7. - -- .. ... -. • ...;,,.. `22.2:::;:-..',... ,t ;pit::: ...-:::....:•1 ki:f.: :.- :-.• 1. -. -4; ,-.... ,.. :,.,, , , .... . :tv • 1%; 11 St • • . • • • • C'Cri E.. .• c••••`"i Cc:4. • .i, • • C! BD:: • • • • " -Pz: -Nis:rt;8 • 0. . • IV: t.:Zar.`..:72:1-.0. O V: l'•• • • V ••••• • • . . . i..;.•2:•:J•a•C•41.r ..*:•• • , J • ".: . ••b; r• ".•16. •.V.•••.) • 17.. • a i .• I . I ‘• 04 . • - ' - :e • C Yrr. • • ; • ; TV" . t :I:~;~:::E • • . • 1 - 21- 4 4I• •• • I , lei:lit:5.4dg' 3,••.\\,' • , • • . • . . • ^ . - • , , • • . ,• .• . 1.•;1•4•; I • 2 ' • "•-•e'• t Cr • C •IC . . • t t. .v • • • • 1 dl t, EFTA00277964

• ' • 4 UNITED STA DEPARTMENT OF TRANSPORTATIO -.STAN RD AlftWOR ,1 I. NATIONALITY AND REGISTRATION MARKS • 4."5 $7893 41 FACTURER A sL 0. A V1 Bo 727a t • • ERICA • Al.. AVIATION ADMINISTRATION 5. AUTHORITY AND BASIS FOR ISSU This airworthiness certifiazte date of issuance, the relict° therefor, to be in condition comprehensive and detailed Aviation, except as noted Exceptions: None 6. TERMS AND CONDITIONS Unless sooner surrendered, su this airworthiness certificate Is performed in accordance with P aircraft is registered in the U DATE OF ISSUANCE June 30,1969 F are l it I , revalued, a as long 's DESIGNATION NUMBER OMR 4129 Any alteration, reproduction, or misuse of this tort =tellable by o fine not exceeding $1,000, or len- s prisonment not exceeding 3 years, or both. THIS CERTIFICATE MUST BE DISPLAYED IN. THE AIRCRAFT IN ACCORD- ANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. . FAA Form 810D-2 (7-67) FORMERLY FAA FORM 1362 ) • COO: I417-0-270 631 • t. I, • .. ‘t. , EFTA00277965

EFTA00277966