B 4 N65317 From 337 Major Repair 2015 12 10
User Manual: B-4 N65317 From 337 Major Repair 2015-12-10
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rorm Apgovet
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US
OMB No. 2l?ff-0fl:ff
ililAJOR REPAIR A}IB ALTERATION
neP.knent
{Ai rframe,
0l Trenspsrlation
For FAA Use Gnly
Powerplant, Propeller, or Appliaxce}
Oflice ldentificaii0n
Fede.+: Avialion
AdsHinisaratiffi
INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix *, ard,AC 43-9-! {s. subsequent revision thsreof) fo. i.st.rctions
and disposilion oithis form. This report is required by law {49 U.S.C. 1421}- -ailure to reFort can result in civil pena*y nat tr exceed 51,0$0
for esch such virlation i$e**cn SOt Federal Aviali*r': Act cf 1958).
Male
I'r
{. Aircraft
1a
Model
lri :l
F4
r'.1 65,11
;:ea:€r
B._,;:rl:crr;aa
It::g Club
I
Address {.qs sf}srAfl &ri resisara*on ceftifreate)
:3: Ei:l ST.
Nam6 i.As sftown ofl rcgr$fratron cedrficat4
ffwiler
PC.t
&l*tianelity and Regisiration Mark
$erial Ns.
19,J
3.
-
Itrr:
."isedham, Ma.021!l
3. F(}r FEA ljse Onlv
4. lrn:1 ldentification
Unii
5=
Model
Make
Serial No.
Type
Repair
(As descnbecJ rn ltem 1 above)
\}RFRAME
}GW=RPLANI
lROFELLER
Type
A?PLIANCE
Manufactu.er
6. Cs]}:orin;ry Statemext
A. Aqency's Name 6ftd Addr€ss
B=
.Ifrar=:r TruC--ru
2:2 E=-ch=:in,*n
I-13 . it1i,,.:2
ll S CediflEle.l
l*l.l .
F,l{r.
:.:)9444,-.)9
tule.har
Forei. * Ce*ili€1ed A,,lechanlc
_ioir:€.
D.
C. C€rtific*te
Kind afAEency
Certificaied Reoair Staiian
I cer':i:y ths: tale repai. andlor alteration made lo the rnil(s) ider:tiied in itern 4 abcve and described on ilie reverse or attachments herel*
have bee* made in accordance with the requi.ements *f Parl 43 of tire U.S. Federal Aviation Regulations and ihat lhe infermaticr:
fumisled hereil !s lrue and correct io the hesl of my knowledge.
uate
Cdi 1J
7.
Approrg{for Retyfn
TfSeMdE--
Fursuant lc the auihority given persons spe*lfied b*law, the unit rdgfiiified in ftem 4 was inspected in the mann*r prescribed by the
Administratorof :-eFederal AvialionAdmin;strationanda$ /7 l< APPROVED tf REJFCTED
: FAA alt. S:*ndards
I inspeclor
r Manufucturer
:,
: lnspection Authorhation
BY
t AA I les!ilne-a
Drte ofApproval er Rejecton
iir'74 ii.:
: Repair Stali0n
Ce.tificate Gr
Desigration No.
429+4e-?:;l
: Person Approled by Transpori
I Canads Ai,tnrorthiness Group
'*"ff;:-':w
FAA Form 337 i12€s)
-
ulnsr
r$pec/ryl
Alteraiian
I.ISTISE
Weight and balsrce or opcralhg lir:dafian c$anges s&alJ &e entered in the apprap{iate ar-rcraff record An att€ration rnusf 0e
campatibl* with alt previous alferaiibns fo assuxe coafinaed conformity with the appliable ai"nvortirress r*quircments.
8. Description of Work Accomplished
flirro# space is req*ir*d. aiach addtlionat sheels, ldentify with aircraft natianality and registration rnarl< and date wark completed.)
Rem*ved prev;*L$ repair doubler to canopy hinge. Rivets were pulling through the skin a*d radiating cracks
were obserYed in the rivet holes.
Repaired torn out section { 1"x2" areai by inserting a i.8S0"xS", .050 u clannei} made up of 2024 T3 , ar:d riveting
in place with 19 CR3213-4-3 rivets acrcss the tap of the channel ar:d 6 CR3212-4-2 along the sides oi the channel
using the factory rivet hole locaiis.rs.
The Pilatus 84 Mair:teaa*ce ar:d Relair Manua! Do*ument No. 23-1 1-00-01482 was used as the repair guide.
As simiiar amounts ol material were .emoved from the previous repai: a *egligible weight change resulted.
:.:
Additianal Sheets Are Attached
-
u.s.G.=.c. 1990-7s1-753
.l
I
I
' l'lliTi:'{
'i5 t,r.J.gtmer{
MAJOII REPAIR AND ALTERATION. '' "'
pl ia n ce)
(Ai rf ram e;' P i,iierpl an t, Pro pel I tirj' or np
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