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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ry ipptg frry.tsbn of No.2l20{XP0 &il 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. $" ^,{d#'.*e/3 vJ,i tB !lr ;ll 'l' l -l ;* l-Fts FIE N B F_ rl_.-r L F H B FL \l- LE,/ -rL rrl h.: F' I -. scHwElzEB AIFCRAFT ccRP. I ENGINEERI}IG NOTE OR Dffi@C'1,I$d{'#SBS$iS5T- No. F-240 j I 'I j TITLE: 11\ rNc. BY SUB BY n n,.rp* ;} *..r,r. i-r,, iq EFFECTIVITY i'f$ DATE CARD POSTED I tr ?r.r,un PARTAFFEUTED I Al" t/2.< rcoLs AFFECTED I Yn.* cHEcKED f'f :!' "/6/ fri 'a. "' t'r- 'srocx DrsPosrroN 1 i EN . SEEIAL Il- fu:-3: *,:::';5 D.C.R. SEFIAL -3qZZ't DWG, NO. r_.se i i C,HANG€: l; tsln .Jn ^* r'\ U i{ AA"-} \e' i: :? J) .J4 zz?- '1 ti r\ 4r -'-, -I:ct {-L l- '7 baa t RASON: Fi-:i:;r,:,.:: r, r- ff) /, I ^ I d"rx tt tt L I c 3-c /)L t yLr":s , Irz 11'i I.^J A 5 (rCaS- q"- .AA Lt: &;!, ri Loa rIJ'qzt tb 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 i.fanq gernen t gineering Engi Pu rr neerin has i:rg Ari'. s tock, Lo'-r1s o: ar)Sl af. fecre,:'. SCHWEIZER AIRCRAFT CORP. ENGINEERING CHANGE ORDER TITLE: rNc. BY ECO. BY C A t-i'g;:: v l't.:,:;i EFFECTIVITY UJ, ii '.i rt I i: ?* *- *t> DATE ilMF:l-'l .F!E i D?'n CARP POSTED CHECKED CHG. /a "5 q.-..1 LET. PAFT AFFECTED i..i TOOLS AFFECTED Fi r) .FTOCK DtSPOStTtON i.) ECO. SERIAL 1z i'i ,. ,J t-. D.C.R. SERIAL DWG. NO. 'a.A77 ''i E' #rGUtrL-ti. i- il-'l :trl,Vi {1, r.::1":Li'. t.pEAT-[- *ro j; FRr-.1 tv,rL ,.\r.:;r' l -r.if^ru'I ia,Li t* -T O * j A53yl tXCE"F?-i- ])ELf-i-L 3*i Z,qi /; * L.iIili l),';:,:,"{ 1- ic6 "jjti;t. f-!?.4f,t{:; ?t,!d }ti;j:!i_.irl.i*..:.i :;'n:';:.,'1{i i-i * t*, -f { IJtr FRA Ftf;:. i f.{ * i # j} A;*.:},r,, 1 I GHANGE: i cEf.Ai-rg * lo I cANioTlv A59? IDEN-Itct\L- -i* _ zs A,.:::t,t'. E-r.LLPT 1CI5 FRAMH. ASEY RLTILF\*ffi.5 .-3 pp',rlr,:iri ,F\{":,1} Y E * L 13 GLA65 RE pL,qCES - tZ GLA ** . *!t3 GLFIS.; lI}ilNT-t*AL- j-**13 E;.;'-C#Fr tsLo\.{N EY SFlg lt{Sl*EAt; Ar c:}:tE-,r\-Tf_ It{ i.;;iA 'bLAi.K' AFT} }-3tu QTV{,I} c; REASoN: i--ix,-r-c.{*i #L"{f,,;; T}LlF{eFiEa;*ii.} ii}t, ,4}$sY FOIQ. {-36 cAf.tOpy ls 4]Er_i]Et] v,/*3f.ri,.}Tt i:ii\.] 3$;3$ili{ { *- i rib t I J)il" FRA Mr -R E &tJ iRL:l) r,}}{ -Ii? F:F.?:-ii i:.,q^i.-r LAT.jH tNsl-&uL_ATr*N i NAr 363ssR'). {-ri*45* }L,,}i.\d,"1 PV 5AC {#*7-i L€_5:} T'i-i ,?lrj }7Ll ff i,il.ri $E.1i C.LAlj"*,, SCHWEIZER AIRCRAFT CORP. CHG. ENGINEERING CHANGE ORDER C 6\ rX TITLE: rNc. BY ECO. BY ttj, +"{*;uif, ?*ed"-,*r1 DATE i r.; CHANGE: /tdghrr#Fl trM1et V EFFECTIVITY l.l0TfD PART AFFECTED \1 l- r.- ECO, SERIAL CARD POSTED '!+; .:, TOOLS AFFECTED N/-) O.C.R. SERIAL i:13'i' A.€,4A ,irJ , ,l ,t,l"i *"F Dli ii i'i/r t L ll K,q-{ iri i-i I }d & idtr-z r L-+ + ;";' J H .r E I PL '- ' .,., [''i'L i'i i''t .L (, F rj,, .,F:? l-, r- )lN lj f: it 17, i I /:ll; tu- f }tT.+ii-l; f."r ii i.)"i.;!'.,: Ilii;i{rii A V i) 3,4 --Z\ DWG. NO. DISPOSITION fu{'$"5,'i:+ STOCK CHECKED .-. i*. {: LET. \ ) . } -i- Fi}.*{a'} (- [5,] :iL : 1:'1NI {' ' 'l?.tvFT-E a'-.;1ruK {N l^'1?.A i',f i- * F, Lil :, i-i \, j , -, il ." ;_.1'P rA r. f- I ) l4-. -rI ! {4\, '\i. i \I, -t e,2:.4 I r-'ir !.-t.: .iali ,U-i.j -- --1'-',-*'- i ,-ri L.-l-: I t! j.:i lJ,:l !;; iit;..i-'1 -r\rTn ,rL tfllLlr ffi:- c A t't 0'P'r irrrt F{ I 'i' )) r.i,;f,. l) 8.r.4 i r*":, \-36 slr.t+4 uP | -.3+ T-i, a,?'ta'ptN,-\r-l h/irH 1-l *r ':, 'T\' EFSHEq ) 1eE\;'i :;[ I; i1 ?-i':i i * i L+ i: -ir,,-r L.[: r 'r-J !..!'f' : '+i;, t Form No. F-240 SCHWEIZEB AIRCRAFT CORP. NOTE OR W r i,4 B l*'/ ALL PART AFFECTEO ENGINEERING TITLS lNc. BY SLIB 8Y :". {:,I i i} r.:, 'l A EFFECTIVITY td, ,:-i0:r.. t,r CASO POSTED -'z-*) CHECKEO cHA!{G€: il'J E i'!t4 ,- }9 OATE :l* I Yg z 'i , ftAr'*'.',, , /-i iv I'it f)-T-\ ) ,n."{ € /", -. TOOLS AFFECTED "c tz'q'; STOCK OISPOSITION Utr< tL-j EN . SERIAL ND O.C.F. SERIAL i.rni.lf,: DWG. NO. -.'{ . 1 trrl}r 41 7)J"T 7 t {ill l'r , ,7. , (\\ Al*I i, :;! ' f F',1 t) - .i*L/,i..r l/.:-' r t -l'' i ',-i,!tt.!ft > i'v ! ) t+ [ \L" -2 , '"' Ll- -- / L:-', - , -r -si\t4tr {ccvexr 5 * Fj o#l<-) 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 .,'* 71 l').. r l^-T: t - t.i!.J ".\.., ,. /-l \< I ,'d 11 frRE lt{ s-io*:x e fr g'f r r -, ^ rPR rT"l -- $ :* ! I t' -i A\L?v ' lit i,1I FL i'.,,, ,)i;: 1-, -ir,i:" 1_ ! t'-;..:. :- r_ 'f r :i I:/\. lll ..tr :-r. '' i-, I i cy Concro I !!gd. conErol Arr: lletlrods 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. 3. 4. 1. 1. 2. 3. 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++++++ I U},, U) L.: \{... t,5 tSr& D 3Ll3-7 (zq) Rr"rE-rr{r,.rr-. 6<,r S p
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