SGS 1 34 N1156S Form 337 Major Repair 2016 01 10
User Manual: SGS 1-34 N1156S Form 337 Major Repair 2016-01-10
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of
No.2l20{XP0
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TIAJQR REPAIR AT{D AIIERATIOI{
(Airframe, Pororphni Prupsller, orApplflance)
tts Oaartarrf
F..b.aAvl[dt
Adrl*lLtdo.i
tNstrarnrnxe, r'il,
rLid q
J
v'
tt'B au .,'rure6i
instrucilirns and disoosition'ofrhb torm
suc'r viilation; (49 U.S.C. g46301(a)
T
s€e l'Ee r4 GFfl
tepott
r
548,9' Part
ruqunr"oiii"*:raii
@
Ileo.to"'lEEiv*u",
I
4il Aepst*I B,
Ac zl3.$1 (or subscqu€nt reGion t *.og to,
uli.tn+zo{}. !n9
Fairure b Eport can resun in a civi, pena}ry for ea*
ar-r^--rL.--^::!-ri:iE.!F
N1156S
l. Alrcrafi
56
S€rl€s
SCI.fwEIZER
-'
2.
Nam6 (As
Orrpr
sfio*il on regt*atton
1-y
cp1liffif-
ioorass (As saoryn on ,pgtris&etion @rtifrcete)
Adao.sPplrgX6S!...,,,
_, . .,
cr, STERLING,.
GREATER BOSTON SOARING CLUB
zp 01564{655
cosry
i*utUa___
USA
_
THE TECHNICAL DATA IDENTIFIED HEREIN HAS BEEN FOUND TO COMPLY WITH APPLICABLE
AIRWORTHINESS REQUIREMENTS AND IS HEREBY APPROVED FOR USE ONLY ON THE ABOVE DESCRIBED
AtRCRAFT, SUBJECT TO A CONFORMTTY tNSPECT|ON By A PERSON IN S 43-7,
EA.FSDO.63 APPROVING INSPECTOR: MARK W. HESSELTON
DArE:
ype
5,
Repdr
Alksralioo
g
m
tr
lkrltldeilllcdon
ilake
&nodel
Sedal f.Io.
(Asdeccrbedh ttem 1 ebwe)
AIRFRAME
u
u
D
Unit
+/+/r{
P.OWERPIANI
PROPELLER
Tygo
u
tr
APPLTANCE
t/hnqtsdl'or
Elllotrt
N*
Aa*a
c*y
Fc:aEBT O.
2ClR
eunCmRD.--.--.-
Me tr\/.1v O/1an
crr*y
U. S. C€{rmc.SAUeotriG
ForeignCerliktedM€chanb
r9parwaon
NFlry.enAilvriffi
be 0r53i
D.
/l
,
USL
Cett'6cded Ma.intonance Organlzalion
!*,ttly thattherepairand/orafteratinn madelo flre-unn(g)krenttE€d hitern Satol_iend
have bcen
made in amrdance with ttt" r"quirm"nl J pad 43 of
u," u.s. redemr
turnished herein is true and conect to ttp tist ot *ifnovfeOge.
Marytacfur€r
--lc.Ce,tG'tBl6:
AP 1701249
fu oribed rrn tbe Everse or attachments hereto
eviIiilrErgulatbr rs and lhat th€ information
Exlended rarnc frrel
ffi;llcFR
Pan€ tr
Pursuani
b fia afioitv
Adminbl'ror d r.e
BY
//t/arl
qryL
tnspedor
fi,tafiut8cfurer
FAA OeeQnee
Repair Station
C€rtificate or
Desigmtbn No.
,;."s*
l*' ;)-
FAAForm 337{,toc)
tr. *it :'it^il;;
u"nffi ln item s- ryq9
-il inspecred in", ure %manner pescribeo
s '
;i;;;;
poP9ng ry".in"o o"nr*,
Fad€rer Avhrhh Adninistrsrion ana
'
P€rsons Approvsd @ Canatfian
Departnoril of Traftsport
lylalntenanca Oqanizatioo
v
lns@im tuthorizar&n
othr.
gp@j
by thf
ettt-Q.
Wkfut
?4td
bdeft,g or @fa.fr4c lfufrdthrncrrarBas daaflDe.aabled. h
ae lryryqtt3glgurafir.ffird.
frt dt.,t,,tmrst [e
dild;adfr;C&
tq,ahan*,'*-.
qpompromoffiffi
(rrnx)re
woe
ls reqrrg@.
affimldrseF.
@
d0,grq'cn.mye,drpgEqthn n,,fi qd rfu v,,rt%t
w)
l't56s
canopy Gr*s, part
Part number
nurnber 3427R;1'3
34p7R;tB uas reBhoed vdrr:an
vdrr an
:ff'&:'*'
offifiBffimFlf
offifn
#
oEM part ffTonno
rduoroo
o-f fire partua-s done lAw FAR-Ete i4- suHlapter€- Ahcrail pelt2r-cedfication procedur.ee
For
Products ard PartB, sitBpett A€srenat pa.i.
21,9 neUicoil* a:na uoniiauo*, hiiCiinu*oed by an o,^,ner or
operator fur maintainilg'graffirg that qnerof
pmdu*.
oper*ors
Fasiedtiofi and' {tstt6$on ff the nBfl 'mrt
wtr ffii{-d ard ernervieed bv,G[e*r Boe*on soarirlg Gtuh owner, and
Glub maintenanoe mansEr : Lau Ktun( a, mraium rAiayl
u,iil
b#tdds;m
tffi
ffi;'
Nw canopy Glas Fart NumtEr 3487R-l'0, 0.12s'Thi& Gher-AryybStanddd, wae
Schweizer Drawing # 3dlZll{l flrev.E By
LP Aero Flai*hs
1086 Boquet Rd.
.teannete; pA 1S644-q707
W€#0m910/6. tny. 10089345
,A**
tabriczrtrecl in
part tAw
Z?ZTAOM
Modiftcatfon tg the mnapV assernbly, Dras[rg
*227R1t2+e*E ure revibrpd by the cunent
Manu$acfrrrer K&l_ Soartil, Cai.rna, tW_ faOa*
rc Hokter ard cunert
xrcooqffi
Modiftetions urere:
l4harEe fire gbss mounfiru .hardrfare to.alf $:tainh*
S*eet.
ffift-ffiH$*Tlorrnoinungtrolesmfite
#Hffitr
number of mountirg
hols
Fnarp:Bqivtrom:,4-,equavspaceo horesto
in fire Rear Canopy FE,ne Bovr ftronr; Sequafy
speced hotes
b
I
10 equany
4-char€e the canopy glm mountirg lrartrae
5r E'--r
--r fularrl
--' v'+: anrr
.rear,canqy.
ErtvPt Earl--' hp
- on
Eo/eE rrrrln
ftom #s, i$160ggR€ scre\rvs
to #6iMS24693rCtr anO nf$2tO{+G1n
NG.
$At'd Dimde urahers, EmIlGSs unoerule.gte
nurn&rg snrenrrhearl* m,ffrq:top portim otle 3orwa,o
dnd rear
canopy
franre.tsor#€-
&Add DimSe uasfiere, [rFrosss tlnderthe gtass npunfrg
sobw heads abrq bdt side raits ol the canory.fiame.
7€n the irsiirte or,rp canopy:rndert* m*i,urg h.dmE;G;rPHc,te
ftrfdtipJiii .no ANg@D{L wz}shers
&Add 1 'll4'X1r16 ii fqam seafirE tape lefiteen
U,e ;dpy.fiArne ffi t e €nopy glars.
lmitU ard trimming fre canopy$lass uilas done tn acodareritrursHxhd faaicea in AG43.i3 -1B
&'Fiberghss and d*tlcs' sedion 4'wnostrHcs,indcur6.
and $Jhdore. par. 3-42 windshietd tnsfiathtion
9Yp.11
(aIb[c]
lnstnre*ions for continued Airu^ctthiness B ahdred.
Folhfl sardard prdces
and windoue
M Urcref qr,"*,Are
Atiacfred
bf the im@ion
of
Ainrat wirdshielcts
A/C Make:
SCHWEIreR
Model:
scs l-34
Revision:
Dab:
SIhI:
Reg#:
56
Nlls6S
REV.#I
This sixher ihm chockli;,* arc'hsUrrctioas for Centintrcd Airurcrthiness (ICA!.tu comply ryith FAA Hanitbook Bulletia
furAirwor{hiness(IIBAWg&I8Dflted&tohsq 1998), re applicahie to fu.airertfrfiitsd aboveu&pn,the foilouring
equipment is insalled:
system:
cAI{opycl.ass
ITEM
l.
CHECKLIST INTOMTATION
Introduction: This section briefly dascribes the qucnft, enginq propeller, or comporrent that hal been altered.
Iaclude-any otlet infor ation on the corten[ scope, purpose, arrangerrent, applicability, definitions, abbrerniations,
precautiors, units of measurernenf, refuqced public{ions, and distibutioo of &e ICA as,applicable.
Conment:
N/A
2.
rlescrlplton: oftbc maioraltemation, ib fimstims, iretdiry
ary-
ao
Comment:
N/A
3.
Controk Operation in&ryxioru
eomment:
ft
$pecial lroa€d,res, if Enlr.
lwA
Page
I
orylanatim of.ib iaterfme with othsr systems;
if
,:,,:
.t
:lr:.:,:,iti-i:ril;
'li;l
:...
rl,:r'
.J
;^
##sYi**e* $s{&}"$*ie**# $xt:k;r*
*r;ffi#**.! '
:
ltt*
it'lsp*rct;r\lr
air-r."la{1 Lns}cctcrJ
"'t-' -'-""'''
frrirgy;1p'1.
liag*
5
of Ligkr AircraS
"Tke ffbrtd's'
?*trh*rn it may concern:
rm requeting LP Aero Plastics, Ino. to
lenses, and/or caoopies forthis aircraft.
l;.:.,]t.
Number:-
-.16
$tr.tgs
uanufactur*
produced
locationtr$p*cial trim varixiondas per
sar*ple Color
Thickness
gnd**""-u
'-
/*v*"
ffi.
$"
^,{d#'.*e/3
vJ,i
tB
!lr
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ENGINEERI}IG NOTE OR Dffi@C'1,I$d{'#SBS$iS5T-
No. F-240
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TITLE:
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CONFIDENTIAL
lnlormation
rAllProprietary
Reproduction,
of Schweizer Aircrafl
Dissemination and Disclosures
STBICTLY FORBIDDEN
without the express written permission of Schweizer Aircraft.
All rights reserved by Schweizer Aircralt
Copyright Schweizer Aircraft (unpublished)
iity Control
Prod. Contro
lle chods
ilate.riaL Control
lchasiu
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gineering
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SCHWEIZER AIRCRAFT CORP.
ENGINEERING CHANGE ORDER
TITLE:
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BY
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CHECKED
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SCHWEIZER AIRCRAFT CORP.
CHG.
ENGINEERING CHANGE ORDER
C 6\ rX
TITLE:
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BY
ECO.
BY
ttj, +"{*;uif,
?*ed"-,*r1
DATE
i r.;
CHANGE:
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EFFECTIVITY
l.l0TfD
PART AFFECTED
\1 l- r.-
ECO, SERIAL
CARD POSTED
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TOOLS AFFECTED
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Form No. F-240
SCHWEIZEB AIRCRAFT CORP.
NOTE OR W
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ALL PART AFFECTEO
ENGINEERING
TITLS
lNc.
BY
SLIB
8Y
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A
EFFECTIVITY
td,
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CONFIDENTIAL
Proprietary lnformation of Schweizer Aircraft
All Reproduction, Dissemination and Disclosures
STRICTLY FORBIDDEN
.-i+
ta'"
without the express written permission of Schweizer Aircrafl.
All rights reserved by Schweizer Aircraft
Copyright Schweizer Aircraft (unpublished)
:
REAS0t'l:
( v;;
r.r n'ir)a
'i :r. tL- ,.^ 1t1
t 1! I .,'*
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Materiai Co,lEroi
rchas in
ginee r ing
PurctraJlnf
s
tock,
Eools
or
cost
OMB No 2120-0020
MAJOR REPAIR AND ALTERATION
(Airframe, Powerplant, propeller, or Appliance)
For FAA Use Onlv
Office ldentification
lNSTRUcrloNS: Print or type all entries. see FAR 43.9, FAR 43 Appendix
B, and AC 43.9-1 (or subsequent revision thereof)
and d'isposition of this form. This report is required by law (49
U.s.C.l+ziilirirrre
to reporican
a civit penalty not to exceed $1,000
for each such violation (Section g01 Federal Aviation Act of 195g).
,or,n.ilil
,;;;iil;
Model
1. Aircraft
S
Serral
)b5
CHtrr'tr'f 7,trR
No.
NationtlY
4O
Name /As shown on registratton certif icate)
MIT SOAR]NG
2. Owner
6rg:f
.L
- J4
esistration Mark
Address (As shown on registration certif ica@
c/o STEPHEN GLOW
1 LAKE SHORE DR.
ASSOC,
STERLTNG, MA 01564_1523
3. For FAA Use Onty
4. Unit ldentilication
U
nit
Make
.--*-*r
AJRFBAME
5. Tvpe
Model
Repair jAlteration
Serial No
(As described in ttem 1 above)
XX
,OWERPLANT
PBOPELLER
APPLIANCE
actu rer
6 Conlnrmitw
A. Agency's Name and Address
BURCHARD, ROBERT D
298 MCEVOY RD.
NEW BRA]NTREE, MA 01531
D
Qtrlaaaat
B Kind of
r'L U.S. Certif icated
C. Certificate
No
Mechanrc
Foreign Certif icated Mechan c
Certlf icated Repair Stat
AP 1 7
o.
07249
Manulacturer
l certify that the repair andlor alteration made to the
unit(s) identif ied in item 4 above and described on the reverse
o|.
lo*
have been made in accordance with the requirements of Part 43
of the - t Federal Aviation Regulations and that the
"r,""hr"n[
inlormation
furnished herein is true and correct to the best of my knowledS;. ' - u.s.
tr/to/ot
Date
eoministraioi.lth;
E"**rDBz^J*_J/
i;;;;r';\,i"Iffi;;i[is;;il'il;,"o1;''p[iE"#lEB'' ''il+]J3+l'Jected in the manner
FAA Fit Standards
nspector
Manufacturer I d
rnspection
FAA Designee
Repair Station
Dersgn {pp19,,,ed by Transoort
Canada Airworthrness Group
I
,4'r.
Date of Approval or Reiection
FAA Form
I
(12
BB)
Authorization
lother
UerIlT|caleo:.Sign31L]1.of,qLrthorized,ndivldUal
" '- "*
Designation No.
,/?? 73 7V
1
/speclfv/
-Zc-/a.2.*-z /t'( //yter-..*'<
,/
prescribed by the
NOTICE
Weight and balance or operating limrtation changes shallbe entered in the appropriate aircralt record. An alteration must be
coipatible with a1 previous alterattons lo assure continued conlormity with the applicable airworthiness requirements.
8. Description ol Work Accomplished
1lf moie space ls reguired, attach additionalsheets.
ldentily with aircraft nationality and regtstralion mark and date work completed.)
Wins: Repair compression damage to false Spar, PN 344A4G at station 190. Damage
consisted of : Distortion of the top and bottom spar flange. No buckling or cracks were found.
Other possible related damage was found at station # 85 , leading edge skin joint between the
first and second skins. The row of flush rivets, AN426AD4 in each skin were loose and pulled.
Left
1.
2.
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False spar as shown on Schweizer dwg. 34.10,1G, includes material list. Repair doubler drawing shown below-
Cold straightened affected area Per 43.13-18, Chap 4, Par. 58 H. ( Repair methods and
Precautions for aluminum structure.,, Straightening stringers or intermediate frames).
Installed locally fabricated Channel reinforcement (.05 2024-t3 ) from W.S. 185 to
W.S. 191, per AC 43.13-18, Chap 4, Par. 59,b.
Rivet size and spacing Per AC 43.13-18, Fig. 4-16, Cracked stressed skin and
AC 43.13-18 Table 4-9 and suggest by Schweizer drawing # 34404G dated
Aug. 27,2001. Reinforcement at spar rveb contains 12 ea. Equally spaced AN470AD4
Rivets each side of damage and 3 ea. AN426AD4 each side of damage in both upper
And lower flanges.
LEADING EDGE SKIN RIVET REPLACEMENT
For Access to the damaged rivet row; Installed standard Schweizer oval access cover and
doubler on underside of left wing,
Forrvard of front spar at W.S. 80 per Schrveizer Drawing 100403C dated June 25, 2001.
Doubler is .032" x 4" x 6" 20247-3 with .050 flanges. Patch is .032" x3" x4.5"
2024 T-3. Extra rivets used per NOTE #3. Patch is riveted in place with CM248-4 rivets.
AII rivet holes are dimpled to accept AN426 AD4 and CR2248-4 rivets per note #4
Replaced loose, double row, AN426AD4 rivets on outboard end of inboard L.E. skin and
the inboard end of the second leading edge skin at Station 85.
The repaired areas were preped for filler and painting.
Continued Ainvorthiness
Annual Visual inspection of the two repair areas to determine that the repairs are secure.
+++++++ END++++++
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