Pilatus PC-7 Sunspot36 337

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.
•
—
^ ~