l♦I Natt00al Research Counal canada canada Institute 1or SCientlfiC and Tectmical lnlormatton ON LOAN Please return to your library by the date shown below: An address label is enclosed. Consell nat10nal de rechercheS Canada lnstrtut canadien cie l'1nformation sc1ent1tique et techrnque OUVRAGE PRETE Veuillez retourner a votre bibliotheque avant la date indiquee ci-dessous, Une etiquette adresse est annexee. CISTI, J_ H. Parkin Branch National Research Council Canada M-2, Montreal Road ouawa, Ontario K1A0R6 C~NADA CISTI/ICIST 549 A FI T I AIRCRAFT· FILE No TITLE· C 105 A . V ROE CANADA LIMITED MALTON • ONTARIO TECHNICAL DEPARTMENT (Aircraft) Ui• ' I " v , REPORT No 7/0510/12 I I - N o O F SHEETS -~-------- Duct a.nd E~ln.a Bay2 ..,.,.._: _ c1eT1 AERO I M.E. LIBRARY 87- ~ 2 l 0 B18LIOTHEQUE AERO I G.M. CNRC - ,c,sT E: Augustine P REPARED B Y c. Rur~ll Gu'ldesen C HECKED SY J l ndrews S UPERVISED SY ,e; / &,,,t 11 • /I,. APPROVED BY DATE DATE DATE r ,;~ ~ DATE ISSUE NO REVISION No REVISED BY APPROVED BY DATE REMARKS L A IR CRAFT ., r REPORT No IL NO •1 /IICN JI I 11111r10 ~ ~ ... LTON ONTAR TECHNICAL DEPARTMENT SHEET No 1-1 I PRFPARED BY C 105 Duct and Engine Bays C J:n,,.,.~ 1 l CHECKED BY SfHAMARY U"•,. 1b l.s repo!"t conta i '15 an eleven redundant analysis 1 ' of •.he C 105 Du~t ana Engine Bays. Stresses and dryflections for the struct1re under the action of fif'teen •m1.t loads are computed, This data is rearty f 0r ~se in the complete aero- plllm analysis and fo· use in detail stressing of the the cor.iponent. - DATE .C:an+ 1.;I,. - DATE -------· l A IR CR AFT REPO RT No 7/0510/12.__ ~AL TON ONTAR/C, TECHNICAL DEPARTMENT I Duct and E SHEET NO __ l-___,,2~-- ___ _ . -- P R EP A RED C 105 ngine Bays c. Burrell C H ECKED --- ---~----- .mm 1-Summary f Index 2. Introduction ),Geometry 4,Frame Analysis - Introduction 5. Fr.rune Analysis - Scale Drwgs. 6. FraJ))9 AJialysis - Main Frame Calculations 7. Frame Analyeis - Light Frame Calculations 8 . Frame Analysis - Combining Main i right Frames 9, Computer ProgrB.11! U. EMrgy Matrix 12, Redundant Matrix 13, Static l))ter-minant Matrix 14, Stresses 15, Donectiona BY BY ' DATF -- Sept856 DATF --- I I I t AIRCRAFT: I . ~ / H RU AIR,NA/. I L I MITED MAL ON O NTAR IO TE CH NICAL DEPART MENT ' R E PO RT No. 7/051o/12 S HEET N b 2 l P R EP ARED B Y C 105 !Afct and engine Bays C . Burrell CHECKED 'By Introduction. This report contains an overall analysis of the C 105 !Afct And Eng,ine Bays for both externally applied aeropl.ne loads 1and, internal joining loads. The structure considered extencs from stations 485.coln to 742.50in. Stresses and deflections due to unit loads are predicted from a strain energy analysis based on a method developed in Avro Stress Report GEN/1090/336 which permits the handling of a large nurobe:r of redundant11. Since this component analysis is to be Joined to the rest of ' the aeroplane, no consideration could be given to alterna.te 11ethoda of solution, Simularly, the requirements of joining have ' determin<·'' the degree of detail to be considered • . SPECIAL FEATURES In al), fifteen loads are considered as acting,on these bays, representing inert.la, engine, alr, and internal structure loads. Five redundancies are eliminated in the preliminary sulrproblems solving for the coefficients of the frames, In the main problem, six more redundancies are considered to make a total of eleven, The main frames have been considered separately under the action of three distinct types of statically determinant loads a nd one redundant load, These are a triple over the -- DA T E Sept '56 D ATE - AIR CRAFT ~ ----;t,iiri" ~ A VRO 11 / RCR 1/ T / / ;t,1/TLO REPO RT NO _7_/_0510/12 - --- - ---- • M'°'CT O !\l ONTAR I O TECHNIClfl DEPARTMENT --- ---'-'------~--..._j SHEET N o OATF PREPARED BY t------------.1.......-- ---- G 105 r... Ri,..-rel 1 CHECKED BY Sent__,• 5c....::6'-----' DATE I I>;et ""d Engine •B""' 1------------L-- -~--__L _____ ___J__~_ - frame, a side force balanced by side skin shears, and a balanced shearing set of loads, plus a redundant load applying a ~Jrizontal force to the top outboard points of the fra:r.e .. ' A si:nrlified procedure for calculating the frame energy has been established, 'lhls ~alls for establishing a Zab by cornputor a.r:d desk calculator This 3 by 3 mat~ix !s then modified for the effect of . lumping t~~ fd~q~r-t seconder/, tght frames to tne main frames, This result is introduced into the c1k of the main prol:.le'l'. For a d,.,tailed explanation o! the frame operatlons the reader is referred to section four of this report. The shear i:anels "l£.1e been comr ,ted by taking· the vertical load as ,cting on the side projection of the side walls and the fore and aft loads as acting on the plan projection of the bottom skins. This neglects a local stress required to balance the pane::.s, whic-..h would, h,,wever, contribute little t t • t d length "h'' '!xji = a ress a pr □Jec e ~ '!m = shear stess quoted hi h 2 = prr- jec•vd length at the two ends, i A IR CRAFT· ~ /l t RO AIRCR .-IFT //4117 1:D MALTON • ONTAR I O REPORT NO. 7/oslo/12 TECHNI CAL · DEPARTMENT SHEET NO 2-'3 P-REPARED BY C 105 Duct acd Engine BIIJ's c. Burrell CHECKED BY • The frames are completely bala...'1ced in themselves as between . the concentrated loads and the resulting shears. ' The longerons have been considered as axially loaded members with cross se ctlonal areas as supplied by ths Duct and Engine Bays Sectln-:: of the. Stress Office. Tbe Inner Longeron is considered to consist of all the ele~ents[Bottom Longero~, Torque Box, etc, ] of t e actual structure that can take a.xial load and is located in this region. Rib 4 areas hav!!! been calculated from ""rbal data suppll-,d by the Wing Group of the Stress Office. At this date the PS 13 installation had not h ~n sufficiently well defined to provide ~ata in report fo~m. CALCULr IONS From the geometry data, ~he, coefficients of the elk• Kip' and Tia matrices are calculate~. These 111atrlcea are sL:r;m as "t.¾J.mmy" matrices on pages 2- 5 and 2-6, When these :natrims are completed, they are operated on, using the computor, according to Type Programme No. l of Avro Report GEN/lOS()/334, The final results of the computor operatlo~ are quoted as the Sia and Zab matrice~. The s1a matrix gives th• stress at ead1 stress point in kips per square inch per kip of unit appli~d loop, The Zab matrix expre~ses the .DATE Sept 156 DATE ' A IR C RA FT; ~ ; H R O 1/RCRAFl /l~'1TL /J MAL."r QN • ONT,ARlO TEC HNICAL DEPARTMENT G 105 IA.let and Engine Bays c. REPO RT N o ---2/.IJ5_J.O/.J2 SHEE T No 2-~ P R.E PARE D BY Burrell CHEC KED B Y ' relationship between the deflection in inches at each load point dt.:.o to the individual unit loads of one kip. Tneae matrices are disp]ay&d in settions 14 and 15 of th is report. APPENDIX ONE Since the original analysis, it h~s been decided to take load 14 by differe ntial bending of fin and lower longeron rather than by twisting of the fin beam box. Appendix one makes th1s adjustment. - - DA TE Sept ' 56 0 A T I=: - - PLAN 0.f",r WING INTACT II I I f=-.- -~,-,~-., . . • \ \ ,\\', . --~ ,' \ A /c- (;_---'---;+,--_..'.kc-- --= ~--==== ~ I ----~- -=-=---- ..-.-~ t £1,ELTR!C.S ~ ~ V,·/ NG FPOF!L£ Fusl-s ,oc-- PLAN 0c,r 1 1 WING 'ri--*---.---- /tffACr I V,·!Af; PP CF.'LE f:._U.Sf:.i_J ! DF: --- r ....,· - i FIN E~A . ,L .3 ::!' .538.77 I I i !~ r I I +---'- l --. +- I -- + A c77cM .t A-A .53 8 .77 - --+ _.:_ I r I I -- l 5 91. 65 --...-r-- _ --. _ ,- _ .Doo ,e t~ w.£,,: ,,...N£A L~-~£4 ~,v ( ': .,r- .fN, ,.. ,.. c.- /;,,,<;.,£ ~ t:..,..,,£-..<.J) -r J l> 11/ I I j 6 'J 7' I I ___ --- ~~ ------ L--;-- ✓ --\. - - ---- --"---+-- .538.77 - ] 7JJ I 1 - + ~ 1,10 + CJZ71 / _:_. I ---------- 'I _ J - • • I I ~ I + ., t e r .:.8 • + 11-591. 65 . • - --=- ' • _J_ - - - ~ - - - - 't"' - -T- ~ =;«E>f"'?~-ffr::~ r:--~?3"1 - - - I ~-= ~ ~--- _ - \ WI/, - -- ii \ ! I /, / , / -- l I I \__ Co, ---- ... ,.,. \___ lOt>,;'Qi/R Cl\ ,C 7 113 .bM-t;-✓lt'.-~---W:~~K-i> ____ - __ • __ --- -- · 3,S" Pfc>'[.; _ '- REPOF:'T : ~c. JULY, !956 1 Sc1 [·-..:---:--_j_____:_~c - T/1.Jf.- 7./.i.5 " / l'.IJ, liHi ... :.... /.'lDf:'c../J. JULY, 1956 r I/ (7 ~ u i.. __ ,....,- L , , EI r I', - \ - ~ - I L (: / L ..,_ "-" 7 cr-1r / ,- JI\. L Pt::', ORT NO_ ; I ---,. 4 1 ll O 1/ R (/? ~ I I // 11/TI-/J MALTON ON~>-R 0 TECHNICAL DEPARTMENT A IRCRAFT ,, -S'-'EET No -----t --+ 1-- -1 -7_ PRF.<'ARED £,j V DAT E I \ /, i - ~ CHECKED B'r DA T E ' - --r- , - • ' ._ I • . I~ .., ~( ' '<.. " 1 -4 ':: I v ' , ) µ \ J r ) I - ~ ~ /11,R0 A/RCll>1l··1 Ll,WITEO M ALTON ONTARIO SHEET No. . TECHNICAL DEPARTMENT PREPARED BY DATE AIRCRAFT· C !D5 7)jCT f cVG B/IY J UNE.. ,, 5"6 CHECKED BY DATE I -- ---· /tSSvMPTl'."N'J -.=--- ' 1) SKIN ,11(' .A OF T()P l{A ,1 2} Arc·1; LOc~,_,_ y AT YA' tl o:)!-, IS <-<' 0 -' 'I ~, 7 /fll r'.> ~t/l TH AN £fiJtv-<~1;';YT A .,i:_=A oF (). 84) I N:,:' I CF ::-1 l:. !=.L ;:;·PUCE:. A J0e:D J. ::rv;; .... i . ,=-- ".fl:i._, A 2 - A* %" j_5fA. I 1E \II ' A /..I Ay Ai/· /:: z d __ / =_ ·:.t::J~ ':...=_,1· ..) T. s. . IZ C'J r; 5 , 1;:c 5. (17D 14.; 76 I 2.Z 5 6 5 1.4(;~ 9 ';J 06 - 00,,.. • t96 ; 2 .{()0 0 I - ':, t, . ;106 " . 0 0 B. S. .060 0 0 0 I ~ 1,005 ,,. /3 0 c. [4:f· 14 57€ 2.Z3l. ' J 57crr: -1 r - - T S" . I 2. 0 5 2 t . (; 'Z.4 5. 24'; I . 2.c 5 5. 2. I. I 6 ~ b. 084 9. 3.?9 .,,"'2 I 712 2. , 810 0 CJ a ,- 2 .,35 . 99 I lfi s. j._'.. 060 .. 0 0 0 I I - t l I E , . 2. 1 5 " 2 • - 1 oA I. 'I 8 9 1 32 9 I. 4 7 ~ 6 6 S ,.:,,4 r - ·-:1 1~ ) . , IZC .3. 5 . 4 20 /,470 4. c:!6 I .Z25 3.5 . 7 {', 'l, z. 75t .'835 742 2. . 47 0 0 (J 0 _, 60 d. B. 5. . ot.D 0 6 0 I ~ ----J . 8 '7 5"' 7.0 /.2 0 ~ 4 .22 6 M-- - - . • • • (.~~ I ,e , ,,cr1 m ~r A~•., ~ AIRCRAFT fee- A4 8! cc OD £.£ FF (;G II R O ~IIIC/?Al-1 l titlllu REc. 'ORT No _ __:) / (2_.5:L....,,.J ~ __ MALTON ON-.-ARIO TECHNICAL DEPARTMENT SHEET No __ -:._-_l_l _______ _ ------------~------ C 10.s- ---:s'- /.J,v,Sj.J; 0.q _. 0 q y ,l,Z.5' AIC.t.:A r ' ' A,eEA o,= wet:' A~~W/M~ F:>R f?vu<::;..JNGr ::: pt? Jr .051 -t- c,.6) ,,7SI = o.,, ,,;,. J_ -lt1:t:.,,i/ .4Re.A f/!"r'/:'L! C4P L o.._...e3-,-, CAI" /,?f'~,22S ,?!>x,z. ?S l,?J"x JS- I. ?S',. . 4 S' /,?I's .], /, 7.; '.<15' ;,?r,. .. H I. ?J " ,4 0 / .?s,. • 2.? /. ?S- )I . 2. ~ I. ?S- ~ .~o /,?-, x • .?.() / , ;,,s-~ ,/7 /, ?S- l. ,/$' /,o x 1.0 A o. 110 = O, 2.1 ,4~£A ex-r,-,,4 CAP ,4a 4 .N 156' ,. -;, f' .( . 2. 0./" .,.r 0, I>: ~. 7 ,7.! .. .1,7 Q,/ ',,. .:J, IJ l (?,fx 2-e.l' O,I )j. 2,1'70 O.J Jc / ,(,;;. X ?, -f l '1 ,<,? J'f ,2.? v'>"f,/? 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I I - 411 ' I I I I , .{), TECHNICAL DEPARTMENT ---- - - I ~~-:~,,,, #I;/ I..,.(... - t - - -- -1 ,,:-_ •~,.,:I,.;;'/ '..,.>,$ V / - • • ..,.-4- , • . a_.,,,,,...-4-' } j- . u1;,; 7.,.: C' .. -.: I 1,...- I . {)/; J /7;, C' ,~"' 'tf,f✓,/ . ~ , . vtJC::J7/ t • c ,,, ,:/ p .,3' I ,CCC~?'/ I' Cl'i:' //4-1' I ?:t _..,_;;,,,/E.. "'"/'J'/" ' ~~ ,. 7~7 j I , .._ / ;,, • . , { ', . 1•~ vP ..,, - ----- i - , __ I I . - I /"A /% l ~,.. ·,,,.. ; ,,_,. • /#_,.. I t' .., ✓✓.. ' I' ,., ('..y t .. '~1<~.-, • . -- --- r .!??if!_ Lvt" .. 0c:r L~?~:: _ • UG~0~C I· Oc2!( ?_ii.~ CC/7 ~ I I . c)v!?O:J,, I ,aoc1.7~ 1.CtJ/J.:,,-/" I I - -·· PRF'P4f?tD RY . / F ANTJDFWS rtRrR •ll-1 /l ~l/ 71-U '"1A fQN ONTARL) ~ TECHNICAL DEPARJMENT 11 I{ (} REPORT NO ,. I -✓ " , .L I SHEET NO ~_!__r¥~ -l P RE P ARED BY CHECKED BY ' _ , 6-11',:1 / II/ I ' . ,... f, .(.. :.- ,,,, / PRf P4r?rD BY . I F' AN/JDFW<:; ,.,..,..,._,bi,r -~ ~ - •11 II() ,II II r ll II I I I tf/ T /- /J "1 TON QNTAH 0 TECHNICAL DEPARTMENT 7-1 I I"'~ )?h -~ ,. '',...; • , ~: 'l ,. ,,{4A,V.1/ tft/.f.f {iJf I c.,; r. --l I ; . - ,- • - 1 -- -~ -1-+- ,,,,,, .., ,. I,, ., ""·-'I ~ « -r ~-1 . "r ,-,,,¥,.. t' ,,-~, i :,,-,..,....~., )-"/..,_,,... ~ . -- ,,,__1 -< ~ . ~--· - >-t --- - Flil,,M,f [--,: I /4, ~,; •. I,', • I """"t .-". 7 > ,,. . r.~ P. I ·I ' PRf PAJ?tD BY . I F ANDRFWS t - + I I r- 1 J I - t I •- - - I _;_ - I I f t-· +-- 1 I I l_, -· ·~ --♦ ~. '1 . -:'~ i .. ' ,J l ' ' '-). ' ', ,. ~ -i ·;1 ~ I t\ i t + ...... -- l ' l1 I 1-- ' ➔ J PRE PARE'. D BY . I F: ANDREWS ""z"l'\/l>lrf ~ /ILRO AIRCR ,IFl l/ ,U/710 M A L. TON ON TA R 1'0 TECHNICAL DEPARTMENT SHEET NO ==-L-_---'---"-.,.- - ~-- AIRCRAFT 1,-,.1 - 7 ...!- ,"7 )?. I,-; ~ I r .,,, ~ .,~ 4 / L ·I ,,.~ / I I !i f', / ,· ,.,...,. ,r ., " ~- ~/ u·..:,, tf.,fj: J-',/4 1/~ f/' ,,,, ,...-, . .,. 2 . 2645 • I 2.46 1.~ I 2', 5 34-0 2. ?J,451 2. 2645 I 2. COO 5 2,7318 . 2.?.{4 5 2. B 6 3 o , 2. 2 6' 4 5 I :! 3. 2.7 4 31 12.3 870 I 1 3 .r a551 .·z 5'o95 , . 3 ,9 b (i '3 11 r /" - \ 2 • 5 Y ?.. 1 I 4, 2350 I_ , !I L. h r S b 1 I 4. :_: - 50~ • 2. G 7 r; 8 , 4 . 2 350 . tt 2; 6758 I I 4 2 :, 5 o 1f I 2. t 7 5 8 l 4. 2350 i 2 t75B 1 . j PREPAR£D BY J. E. ANDREWS ~ Al/RO AIRCR,1/.T IIM/TEO MALTON ONTARIO tECHNICAL DEPARTMENT AIRC RAFT: PREP ARED BY Frame Lumping Alex, Grzediie~ski CHECKED B Y b!lI'e frames, ela~Lic ~~trix, -1 . = Zki, Oare .frar.es, s tif .fness l\la trix, added stiffness matrix, exuressing addit'ional half frames, correctl0os to Zik• furivations: Dik 2kl = 0u (DJ.k + d1,) (zkl + zkl) = bil Combining (1) and (~) ( D11e + dik) 2 kl "' - dik ZKl Dik zkl = - dik (zkl + zkl) (,.) is solved for z. • and lhe rt-sult is suu.s titute :f in (3) U) (4) ZKl "' - zk; dir,n (Zril + 2 r.1) (5) (Dii< + dik) zkm d.x:l (Znl + zr.l) = din Zn1 Reioo:nbcr.i.ng (.i.) 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PREPARED BY C H ECKED B Y _ • \?; ' -1 -=-~rJ ti I 4 > ..__, )(,l't 4c,c,'<.' > I DATE DATE ' AIRCRAff V" I ·I \/ ~ ~ AVPO A IR CRAFT l .lMI TEO MAL TON • ONTARIO .TECHNICAL DEPARTMEN T /O'f er. t , REPORT No / / > ~ I \ / I '2 I 2 ; SHEET No I - 8 PREPARED BY CHECKED B Y ,- - 2. 't \ "t i ,.1 \ _) l 'I ·' - iJd\ -1\•"'!• tI1)·1~"r, DATE ,i l R O A I R CR ·1 I- l I IM I rt D MALTON 0/\iTARIO TECHN ICAL DEPART-MENT -,_ I ,J !,' )0 ._ 2. l ·. '0:• :_2l_,_, I l < I 2 o+ I V ~ I~ DLI ~ A. i L 2 I ,4 7 A 4 1 ·- - 1 ~ .- I ' ~ ., :'." _,:_ _J ' - ;) ~' J I. ., I• I ✓ 1 , ''l.c-7 ,.. - ' I ~ '; •io . . ~ l l' .. .,. V ~e,(.. ' , \ ~•"<+ ; ; I ) l 1, 112, l1~ ': ' r ~ ;:-,.-I l-- _ __,____,__. ...... I 'OTAl I ~)'(f ~-- -1 I --- ! . , , .. r- J, ~ !::, l ' , . -, ~ _ _____, ;..- ll '') ;cfiP ,~-' I , , :,; " 0 1· 5 - - REPORT No. - '/ ,:'/ r;- / / ;:: ~.,,_-!,'---1--.:_:,,_ ___ _ SHEET No PREPARED BY DATE t' CHECKED BY I n ~ l ... ,~i, 1,,-~ i... .., I -~ , 7 "-• ) I I >' "'' •r."' \ :.,\ 's ~ 8:. - t -- - .. G . - , L' ·:; .,. 1~. ~ ... • J . - ; '77 ri<>Q ~-1~~~ ' ': -'- f, •• ~ .. l~ )'.2 . t 'LO .,__.. 1' 1 11 0 /l /R CRAl- 1 l / U I TtO' MALTON ONTARIO tECHNICAL DEPARTMENT R • .ORT N o _i/_e:,___,, 1 _,_C)~/-'_'-~- \ b SHEET NO PREPARED BY D A TE AIRCRAFT . 10C. L:::- t\,/ ---/ (' ~Ii- I I ~ \ CHECKED BY D ATE '. •r, ( - ~, -~ L~ I· -= ,)t I I ·1 L1 - ,~ ' * , !f L, - .., " I 1-:) ') I 1\ \ \; \ \ l ' I ... -- I ➔ . I "~- v-,.., "t'c-, ' C: < l ~ \ A t' ,..~ I l I I . ~ I L, I • I -,., \,...~ 1...;, _r., C 'i. L, {'P 11( .:r,c i I • ; l, I - J I ' ,II'(;' 1Cao--~,\ ."'4 ... ") 0 L, (, ll I_, - ,_, ' \ -~ ;; , .... , c.+~ I L, 2v ' J - ,CJ•'\-( I oCc- ,1 • I • . ·~ :i :.c; I ~·1 i t ,ur-· • I ,11., \ ')_ \'-J..,. \,._ .. ,-) t ' '- i:. " t I l ~ ~ ,I <.. . .., I 1,) \J /1 < 0•• < i, ,., , . , ff.~ / I' ·1 t.., ' r ;-Jt"' I ll/10 A/IIC/l 1/T 1114/TFO REPORT No - , / O C, / , .:_ I------- MALTON ONTARIO TECHNICAL DEPARTMENT SHEET NO \\- ,:'. PREPARED BY DATE ~1RCRAFT C t, C 105 CHECKED BY DATE IN,: "')4-...t,. C - L I • • k .,,.._. /.. Q, _, I r-i I • lr I , ,. : l b.ee 1 L. ~ c..J•r r . ,, I I ' ,- . ··~·) t -~-! ./ .. ( .,. ' .. A~ ' , r-,. I I , 'i l( L p y I' ., ,, ( (' I ( I ,< (-.,.;- f I I •-"'·-'' (1 <. (. t A tl ~ .,~ l t L ,., e\ ,. 3-1~) ... t ~ ,• ( l ~ (-:, t. - ·/ / ' I <1 /;,,~ , / ,er.,. 1 I _;, le. , ,.., f,,. "~ "' ,1 , l ;I -;f ; " .... I' I [ , ;(7-/ I{ "' 0: ·~ I .;,I I , , .r( t £ , ( :1 ,I. /4 t' ,. r- ) < :...,· /4 (; , t, • ~,?. • I) ' {) I' /2; , I. 1~~ '• I ..., ,... , !i Ii ,, ~ ' r' '/ '1 t" ~ Al ( ,, If'"'/,.,_, ,/t I , ,, [.~ 10,n TECH~ 'a ) k......... ~ ' l - t I AIRCRAFT 2V = I r, A. ,, 4 A"-' '- t J 1.., j ➔ - 7 $ \, z I f1: + h.J WEIGHT t ;(,t, •.~., I \ ,, >\4 ., < c. G. POSITIO~ 2 3 4 5 6 7 8 9 10 11 Li"'' A • . , t, ' ; ). A, " A .... ,., L,.., ., , r '·, Ali, kn A ' K ~: A,,r.; A \ i t" ~/ I .• ~ \ -· ---+ r ~o t ' 't rr. ~ ;::-,,..0 fl ,'l J!-r" -'I F-r 't J SOCJ I.C/8 -?] ;/ J.j ~ /. 000 2.'1(..7StJ 3,/,:),J,:J) ,,,.1-'1 !; eo ~ '1? 9 2 ."1?0 j- .820 J "-" +~ S. I-, o •'i'J,.S-862 :t '" ;; f."•• t I I I• 2 , 1(,0 I.:~ .520 2.4 8 7SO 2.:u.2.s-0 &·?6 '/6-2 ~-5'' 1,.,- = 8'" 4, r I 2..soo I-S-20 I, \-- \\ ,f."f S'OO 0018 77{, ""-4" I 2 .-1-50 2 . 2 73? 2 .-1 6. Z.91 .?c?/;J"/ 173 I 0 /. 5'20 . 6, fJ 0 "'1 ~ "' 1Vjb:. y, -4,I '7 5- ,0'178 8 /,0 r ? ) /, 'l / S' /.6 79 7;; it'fZJ 2$' OCJJ6 (,.4·0' I r; . S'+ - 14,7~ ) 4. <'! ~2 _? 3 ':15° OJC4<' 1.f-. I. O " ' I.S60 ; ,4-?o o 1.,oGZ OQZ"f 08: /.,? . 60:J .la )0. \~ \'\ er.::-, ~1 2. , 7 t~ 0 (;Q(X.8 /'7 I,"> :H C ) . (,20 /,ZO O • '/. 2.1?) . O'J~i 2.2 /.0 2.454 ,... Z.450 00/;I /4 .,., C' z. 08550 / .. , Non : SEE: PA6:: 3.442 .00034 3"- 7 1·~-7' 0 4,912.3 ' t, 1/ JI 215' " • ! 5'I .992 . 9ET300 1.35'6'50 , 001 3 94- .. ,, 9 J, I Q 0 .. p ] so .... , ) t, AVRO AIRCR ,·l /- T LIM/TEO TECHNICAL DEPT . CAIRFRtM E) AIRCRAFT WEIGHT C . G. POSITION 10 11 A 1.00:; .820 . r. - 2.4-5 4 J, 21 5 12 , 13 14 15 L, J 1,6 4 ? \ ,, 7 0 1 0 4 . 712.JJ t,L.:.. > 5-b 9 3o .1600 10 .0533 2.- 090 REPORT NO. SHEET DATE PREPARED BY 16 l.327Sv . 32 'J I !:2.0 ,(,/ 5? ' 1. 524 75 .9€0 17 Of)) '181 ,(JOJ'"/2 7/ 0 1/, f37 I .or-14-0 /JC 3;; , .,(J:f I II - ; 18 19 2. ,,-1 Pr ~ rt•' /-1r1 I• e J '"'02.2. I '7 ') . ,: 174-7+ ,, I ;;,ift#.1 ,,,_]~-2.•1 /.o 1,0 .00138:J .tJO/'/S3 .000802 ~ JIV/?O All?ll?AFT L I M/TEO MA LTON ONTARIO TECHNICAL DEPARTMENT AIRCRAFT· P R E PARE D BY C.( D A TE CHE C KE D B Y DATE 'Re DLJN.DA\lT 4 te.ovP, - ' > ' '' L' g,c.g u P1-i<; 1_F t, 111:'i ~ t (. ~I ' '= ,Q\~\ .t'o,ur ArF ci'":r.- • I 8 J ~ 'C ~ l'\j'~ ~-- E qjf'!·~ I r / le-,~ ► l F'o, .. I :.,,--... I • l __ ----' l I) I , ...... ··- - ,. ,. ~~ -- -_____ ,_ - --- ~ l ,,,., TE _, \-\ '- ' 1:), " ,, I AIRCRAFT L I a.I -" WEIGHT -· G . POSI TI -- -- 2 3 4 5 6 7 8 9 10 11 / 7 l C • t_\l ,, I 'C ,, - --= ~ 51 7 ,:-, 0 ~14 5..j C () .. 0 :'". ) <; l . ) r-,..-, " I - --- :, ,_ I\ . ~ .. ~.-, "', .. I 7::> r •t ~ ~ e ' >- 1 " I, ,c-rk ~, ,. I 71 _ ., • -·--~ --,..,,. ,._·-~ --..---.- -- - --· --- ~- - - . . . . ' AVR O AIRCRAFT LIMITED• TECHNICAL DEPT. (AIRFRAME) 1--------------------------------1 AIRCRAFT WEIGHT C. G. POSIT ION _,,..,, REPORT NO, I 'I SHEET 1·, DATE· _u ·11 r Y. r !. f'f ,, . -- : .... / -PREPARED BY ==;====::::;:::::===,:===:;=====r==~½:c .... ·===r====;=====;====;=====:====;=====;===:;== 4 5 6 7 8 9 10 11 12 13 14 15 16 17 ' .; I ' ,. A \ ~ ', .,. ~ l \ .:; I . "' .:. ·---- 1 + ' .,. 0' )' t ., I • ;;,. j-'"'· :, r • C (. 'I ' AVRO AIRCRAFT Llh/lT£0• REPORT NO. 'I I) l) ,. \,'. TECHNICAL DEPT. (AIRFRAME) \ ·,_ - ::, SHEET 1-----------------------....j AIRCRAFT WEIGHT DATE ~'l A~ ~ •c:1 r • 'Ii "'• ~ j ·, I C. G. POSITION -PREPARED BY _,_ 9 10 l 1 12 13 14 15 16 l7 18 19 I A r i I l. I • r< I I' ~- \ . . , ·1 .~ii I I 2. It I .... + C ~ ~- , • I ,oob,, JIV/10 JI/RrRA/7 I r-1 ORT No._J,t '")", \ .--,, \ 2, ... I/II/TEO M AL T ON ONT A R I O TECHNICAL DEPARTMENT , SHEET N o I .. P R EP AR ED BY DAT E AIRCRAFT ., I '[ ,.- ~ ,.. __ ~ ~ •, C t '.i H.~ \/ (;1.. l.,; ~-= I CH E° C KE D B Y qA TE . ' i~ rr -~t --r - - - - - .. - I 1-, I 1-, . l I I ~ ' I l V' - t I I I X1 X. z. x, X ·~ ' . ' ~, l,,1•n ... LoA.U t) r- ,-t .!! f, t.. 11.- l ' • I!' \ .,, .. .Je. ?;. I Q "' ;<'.. 4- 6_. -p ,e !,; ' ' · \en , f' I. ~ 't,' ,. ,~ • - ' . f... 2. 1.., <';:. ~\ , l, I , \ -. ._ ") , ' " i:. r' ,.. ( ' I I ,.., I , ,. ,,, I _b,;: o._ ' \~._,, 0.) b:.3:. - ~. I = 1.~. - :::: ",, h t - 'h1 \._: I \ -r '1 ,v { ~ T . . . '"' "" :/4 - I ' .- . ' /. ,_ - /.~ h, - _]ut - x..., I {,, I:. t X.-,_ - 'I - I ,, d("' \.,.("" I (11 J - I h -~ - \, 0 l""J11.. \ f. - I 1.,, ~ C .;' ( (- , _ I ,, li_~ .,, -l .. Li ' I - , h1. - i'--' l , .;. ,. < -; .. ~ * ., ' ' - ,. s ' ..., .. . " ; " ) . ,.. : . "; ,t ' " ' i * -ll- 11 * * -r.• •. ~- ~ i! ,... ':- ; --i r, '") . - I"' - T r .._ ., > ,t ... .r ,.... "( ~ ... r- N \ .. , ..._, ,- ~ ) . •' ... c.{). ; ~ d - :- .... ' ~- J: '} ;, • * * ) r (\, .') et,; C ~:)"')t.() . ~, ... <'\ ..... r-- °' t'- I " -- f .:>Cl l,i ~o.::. .~ ,..,..,.-(" ~ ...': n J \.ts-' \rt 0 • ~ ,... 0 . !- N o • ~ r-- 0 (, +-tl~ ~ • 1 1 ,d- ~ l'i" i- I· t § ~ r= l. t ' + ' + "q- -et-- -- - -. I~ tl"" 0 0 -.Jl -.J) o • -../- -t 0 0 0 0 t '_ ~ t -, i- / I L - l 2 --------------------------- i - ------..... -------------------------1 .&fud,. ====::;=:==============-=-==-"-:====--'-=- = 4 5 6 7 8 9 ~ ~ ~~ C' .' ,! .4 ' . ; t 't -' " -· , 1 "'- I ... ' .\- ~-I '11\ • I ... . '· ... . ~ ., '' ( P-1 ' ..... , I l l ~ " \ ,--c-1 r I , ,, / / , ; -\ + t '\\ " ~-. 4 bC l"I • I.. . ' J - + 1 \- ,:H~t• I , ' \ '1 . -t- -+ s~,-n . \~ + " .I t~ ~ \ •i- \ ' :, I~ ~ 7 ., ·, 1 ' - / / / / AVNO AIRCRAFT IIMITED Tf.CHNICAL DEPT. (AIRFRAME) .a.lRC AFT WIGHT C ,.; P ITION 0 11 ' 12 I c..,, - 13 1 , /' + ,\\ \ ,/ \ •·· \· r '\ \ '.., :: ' 11 ' ,) ') ' \ ~ 14 \ / 1 .1~ : 4 .. .\- l i· ' ' " ' / 15 ~ tj " I... 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C-105 Duct and engine bays Report No. 7/0510/12

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