Q M S NOL 2120-0020 Bql 8/31/2014 MAJOR R E P A I R AND ALTERATION (Airframe, Powerplant, Propeller, or Applismce) us Depaitment of Transportation Federal Avidian Admlrttetration For FAA Use Only INSTRUCTIONS. Print t» type ^ ertries. See TWe 14 CFR §43.9, Part 43 Appenifix B, SBfid AC 43.9-1 (or stAseq^M** revisiontt«reof)for instriKdions and dispaeition of this form. This repwt is required by law (4S U.S.C. §44701). FaSure to report can residt in a dva penattyforeach s u * violation. (49U.S.C.§46301(a)) N a t i o r ^ and Re^straUon Mark SeretlNo. 480 N97GG I.Mrcraft Series Model PC-7 P I L A T U S Ackkess fAs shown on regstratiat c e r f i l i c ^ ; Name (As sfiown on registraffon certiScate) 2. Owner ASTRA 7 LLC AddlMs I g T E S t X H E VILLAGE RD City SANTA FE Zip 87506-0023 3. For FAA Use Chilv 4. Type S.Unttldaitificirtion Repai' Alteration • • AIRFRAME • POWERPLANT • PRC»>EU.ER • • Unit hJtodei Make POATUS (As d^cribedin Serial No. 480 Item 1 above) Type • APPLIANCE • Mani/acoiFer 6. Corrtomnity Statement B. Kmd Of Agency A. Agency's Name and Address Itomc N E t A . WEAVER X U. S, Gerancated Mechanic 1 ManUacCurer C. Ceitificzte No. Foreign Certificated Mechanic oiy c/u^soNcrrv Zio 89706 sate NEVADA CcuMn "SA Certificated Repair Station 2036732 CertSicated Maintenance Organization 0- I certily that the repair andAir afteration made to the uitit(s) identified in item 5 above and (fescrftied on the reverse at attadmeitts hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Re^iatiwis arwl that the mformation fijrr»shed herein is true and con-ect to the best of my knovuledge. Extended range fuel per14CFRPart43 App.B Si^iature/Date of Aidhorized IndivMual r—\ LJ 7. ApprovaJ for Re&gntoService Pursuant to the aiAlioiity given f»fsons specified bek>w, the urat identified in item 5 was inspected in the maimer {vesc(ft>ed by the Administrtfor of ttie Federal Aviatton A<*ninistration and is [ 7 ] Approved [~| R ^ c t e d BY FAA Fft. Standante Inspector Manufatiurer MaMenance OrganizatkMi FAA Designs Repair Station Inspection Authorization CertifKate or Deagnation No. 2 0 3 6 7 3 2 Si^iature/Date of AiMhoiized Intfividiel FAA Form 337 (10/06) Pagel Persons Approved by Canadian Department of Transport (Xhsr (Specify) NOTICE MfeBWand/tatanec oropenBngffnrfniinnthmgti ^tdl be ettemd m Ox tppnfriBtoakc^ AnabraBon must be uMiftaaJewmiaKpnyious aMwaficws foasstsv caaSnued conformiy imS> iheapptcabieaawotthkness requirBmant&. 8.De«o»BowcfWoi»Accow|aHahed naks ^ 1. InstallMian of AEROLEDs Landing and Taxi L E D bulbs FC7 " Rcmproi OEM amriledtncandesraitLaiteg and Taxi l % l t t b i i l ^ 2 &iniiiGBdA£ROLH>sLao£i^8odTaxiIJ9>lraIbs^ac^iiiaIIi^^ F/N^ 0i-10304.-A and 01-1030^-A I x ^ FAA PMA. Ckigmai S Amp ciicuit ixeafcas wax letmnesd v i d i oc^imai m a r l s ^ L ^ t t s were aimed as per <Kig^!^ and per raaais MaintoiHmce m acyqptrtte mnoiatt: of l i g ^ for n i g ^ cfiesaiions. AEROLEDs InstaOttifm M s o n l 0003-0004 Rev.C, is sOtadied. 3. WdghttSfEeatatialiK^Iig^a 4. Tnstmcrinn^ r W l m ^ J Atriff~««»i~-~ There are no lepaiisforbulbs. f«~Hi;«H m AF^'^T F T V i Ii«t»lbrinii M a n u a l N o 5. This m o d i f i c a t i m t o benaiiamMd/inspectBd lAW Pibtus Manual 0171S a i d AEROLEDs No. 0003-0004 Rev.C. tfadBagFoBowj ITTAABiooalgiBels AlfcABached ..^AFonn337(10/06) - » - . . . ^ ^ Pt«e2 OnOT-OIMK R e g . CL, tetalteiwiMagHat ICA CHECaOIST FOR FIELD APPROVAL N97GG PILATUS PC-7 s/n480 1. Introduction Replaced existing landing and taxi Kght bulbs with AeraLEOs sun spot buibs. P/N 01-103(H.-A and 01-1030-H-A. 2. DesoiDtion Replaced existing landing and taxi Bght bulbs with AerotfDs sun spot butts. AH origin^ nxxjnbng hardviare, moints and Wiring were utilized. Originat drcutt brealces (2) of 5 amps were retained as were ori^nal placards. All wiring is factory Instailed. The tights are aimed per originals. The installation produces an acxeptabie amount of i i ^ for night operations Aerol£D5 instaHabon manual 00034)004 is a t t ^ l i e d . 3. CoobroiaOperationInformatibn -•' (Opttonai) 3 position swii^lDrepiacEortginariandmgllgttswiliAWMA Udieied ON-OfT-AJtSHING. EATON MS24659-29A or e q u i \ a l ^ Other equipment and does not exceed 8 0 % of etechical output RH output was tested on pulse and found not to Intfirferewithratfios/avioniiss.' ' 4. Servidnq Informatjon Hlabis Aircraft PC-7 Maintenanoe Manual Document No. 01715 and AeroLBDs Document 0003-0004 Rev. C or later. 5. Maittenanoe Instructions Pilatus Aircraft PC-7 Maintenance htanual Document No. 01715 and AeroiJ33s Documertt 0003-0004 Rev.C or later, and AC43.13-B. 6. TrotAleShootinQlnfbrmaBon AerolfiSs instaUation guide 0 0 0 3 4 X » 4 Rev C or later. 7. Removal & Replacement Pilatus maintenance manual * 01715. & Diagrams AeroLeds installation Document 00030004 and PNatus Wiring Manual No. 0 1 7 i a 9. gpedailpstructioiB Attached. 10. ApptotjqpofPrevertivftTfeatffWffe — None. IL Data Pilatus Aircraft PC-7 Maintenance Manual No. 01715 and Aeroljeds Document 0003-0004. None. 13. Commuter CaH^mry Aircraft Not Applicable. 14. R<ynmm<wlPrt Overhaul Period No adcfitional overhaul time limitations. 15. Ajnwfthinesgtilrttations 16. None B ^ Q D . Revisions must be subnritbed to local i=SOOwitthpt(H»sed changes. • — ^ ~
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