COMPUTATION OF INPUT REQUIREMENTS OF THE AIRCRAFT INDUSTRY OF THE USSR

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP79-01093A000300020004-0
• Release Decision: RIFPUB
• Original Classification: S
• Document Page Count: 11
• Document Creation Date: November 9, 2016
• Document Release Date: February 11, 1999
• Sequence Number: 4
• Publication Date: October 1, 1952
• Content Type: REPORT

Approved For Release 1999/09/21 : CIA- 3 0300020004-0
Sb URT2Y INFORMATION
PROVISIONAL 07ELLIGEI E REST
CQMPUTATION OF INPUT REQUM=NTS
OF THE AIRCRAFT II ISTRY OF THE VS&
C TA/RB FR-19
Ober 1952
AJM
The data and tonc1 sions contained in this report
do not necessarily represent the final position
of MIS and should be regarded as provisional only
and subject to revision. Additional data or
comments which may be available to the user are
solicited
THIS DGCW ENT CONTAINS IWORYATION AFTE TING THE NATIONAL
DEFENSE. [ THE UNITED STATES WITHIN THE MEANING OF THE
ESPIONAGE LAW, TITI1 18, U501, SAS m 793 AND 794, THE
TRASAiISSION OR REVELATION OF WHICH IN ANY -YJN ER TO AN
1JNAUTHEIZED PERSON IS PROHIBITED BY LAW.
CENTRAL INTELLIG aI E A T
Off lee of Research and Reports
Approved For Release 1999/09/21 : CIA-RDP79-01093A000300020004-0
 Approved For Release 1999/09/21 : CIA-RDP79-01093A000300020004-0
C -TARR PR-19
(MR Project 36-51)
saN M way +~ 41i
ESTIMATED FINISHED WEIGHT AND BILL OF MATERIALS
Pounds
Y TE she .m.. - 1
aa~eri s
Ttarq
Wince.,,
of
P roes Dural Steel Total Dural Steel Total
Front Spar, O.B.
Web Dural. Sheet ,057
x -3/4 x 116 (10 in.
x .3 In0 hole)
1
4,3
643
Cap, Dural, Sheet @080
x2x114
1.
18
1.8
Rivets, 3/16 @ 3/in.
350
003
0.6
Front Spar, I.B. (E 'E)
Web,, Dural Sheet 133
x 7 x 1.39 (75-ST) 1
907
907
Cap, Alcoa 79-T x 139 in. 2
8.3
803
Cap, Zoo .265 in x 21 in.
x 139 in. 2
16.7
16.7
R.tvete, 3/16 0 3/ins, 8460
0.8
1.5
Rear Spar,, M,
0
Web,.. Dural Sheet 0975
x5-7/8x133 (U in.
x 3 in0 holes)
1
705
1100
Caps, Dural Sweet .093
x 2 x 133 (75-ST)
1.
207
207
Gap, Dural %set o67
' x 1 x 133 (75-ST)
1
409
009
Cap, Dural sheet 07
x1ix133
1
1.44
1116
Rivets, 3/16 ? 3/in0
4100
0.4
007
Rear Spar, I.B.
Web, Dural Sheet QO975
x 8A x 84
1
609
609
Capp Dural Sheet .093
x 3 x 834
1
2.4
2.7
Cap, Dural Sheet 067
x 2 x 84 (75?ST)
1
112
103
Cap, Dural Sheet .067
x 1 x 84 (?5-ST)
1
0.9
0.9
R.vets, 3/16 @ 3/ino
250
Oat
005
Diagonal Spar
Web, Dural Sheet .080
5z x 63 2
5.6
605
Ca a,o Steel "T" Stock t
3x2x63 63 2
1.0300
306.0
Bolts, @ 3/4 in. Pitch,
3/3 in.4x2in0 IV 170
8.5
COMAE
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 Approved For Release 1999/09/21 : CIA-RDP79-01093A000300020004-0
ESTIMATED FINISHED WEIGHT AND BILL OF LS
Continue
Pounds
~
"a s
te
Pieces
Dural Steel Total
Dural Steel Total
Nuts,,, 3/8 in- (Stagy) 170
60.8
608
Drag Strut
Web, Dural .080 x
6R3/4 x 41.5
1
203
203
Caps, 063 x 21R x 1L5
1
007
0.7
Rivets o, 3/16 in. 0 6 3/in
250
01 02
o.5
Cap la .+ Dural 631. x 1-3/4
x
1
202
2a2
Struts, Alcoa 79- 10
3
0c 7
007
Rivets 3/16 3n0 J,@ 2/in0
60
001
001
Drag Strut
109 x 2j x 41.5
1
110
100
'alse Spar (10B0 ford)
Caps, Top, 011x2*x214in,
2
101
l0l
Caps Lower, 01.1 x 2 x
U in,
2
0,5
005
False Spar (Aileron Hinge)
Cans Sheet Section, Similar
to Alcoa 22022 x 60 in, 1
2?2
202
Dra
g Rib
Caps, 0125 x 21 x 29 ino 2
107
,.07
Web Dural 0037 x 9 'no
x 98 in. 1
107
203
Rivets. 1/8 ins i @ 3/in0 '
(,e-4-n-
Sk n included) 900
0a2
006
Stringer, Loading Edge I o B0
(Extruded Sections; Closest US Shape Is Quoted)
1 Alcoa 10135 1003 x
76 C
1
1,2
1.02
2?}Alcoa 10135 1003 x-
q
1
6
6
1
9 P in*
1
,
.
3 Alcoa 10135 149 in0
1
101
lal.
14 Alcoa 10135. 0601
135 in0'
1
110
100
5 Alcoa 10135 0601
97 "
1
007
007
Stringers, Leading Edges O?B0
I 094 x.11 x 38 in.
1
005
005
2 ,094 x 1f x 98 in.
1
16;3
1.3
3 0091 x 1 x 148 ih0
1
0a6
o06
4 00914 x 1- x 59 :In*
t
1
008
0.8
x 98 in.
5 094 x i
1
l02
1.2
Rivets, 1/8 in 0 3/in0
(Skin)
2700
On 7
104
S- '-C-RREcT
s .sr
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 Approved For Release 1999/09/21 : CIA-RDP79-01093A000300020004-0
S-13--C-R- E T
'P.9fPTMA'N D FTNTSITED 1-EMIT AND FILL OF 14ATERIALS
'~4 MT AZIF11 ANn X.ANT~INC GEAR
Pounds
nis d ~ ~. BFiff of Materials
Item
Stringers, between Spars-
Pieces Dural Steel Total Dural Steel Total
6 Alcoa 10135 - 0601 x
64 2
0.9
009
7 Alcoa 10135 - 0601 x
1,31.9 2
1..8
1.8
8 Alcoa 10135 - o 0601 x
52 - 2
0.8
M
6006 x1*x54 2
005
005
8 006 x 114 x 70 2
100
1.00
Ribs, (Counting flap and
Aileron Ribs Tai .oe ) %
i
al Sheet,.037 x 82 x 62 9
2540
37.0
!3
x I in,. y Holes, t Flange All
Around)
Rib
Clips, 406 x1.2 x 7 in 36
2.,2
2,2
Riv
(I
ets, 1/8 in @ 3/in0
ncludes Skin) 5100
103
2,6
Skin s
Root 10B. A 00714 x 42
x 27 Skin (Upper)
1 805
9.5
Root.10 D0 s .100 x 42
x 2? Doubler (Upper)
1 117
1405
Root 10B0, 0066 x 33
x 36 Skin (Upper and
Lower)
2 1600
02
29
Root 10B,,, .100 x 33
x 36 Doubler (Upper
and lower)
2 23,8
43,6 .
L.E. Inboard, o072 x 50 x 102
2500
38x2
L E OaB4 .055 x50 x
102
1 24.2
28.6
Between Spara,,.054 x 30
x 125 (Upper and Lower)
2 31,4
420 0
T.E. inboard (Upper), .054 x
20 175
1 12,1
12.9
.Rivets (Along Spars) v
15
20
1
4
i
1 12
12.9
x
.
x
,05
s
Rivets (Along Spars),
1/8 Q 3/mno
3000
100
2o0
winTip, o5h x 24
60
1
508
1200
Wing Connector
,125 x 22 x 57"
1
3,5
305
Aileron Hinge Fittings
Steel- a063x6x4
2
0063 x 6 x 2
4
0063x2x2
4
0063x3 x2
2
Totem,
.0 8
1.8
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 Approved For Release 1999/09/21 : CIA-RDP79-01093A000300020004-0
S>E-C-R-E-T
MUMPT; RAE t~IJil LAI?dDIRiMFJI~~
C.on inTeZT-
Pounds
Item
Dux?al
Steel
Total
Dural
Flap Hinge Fittings
108
108
Spoiler Hinge Fittings
1,8
1.8
Wing Weights
65.o
65.o
Handhole Cover, Alcoa
23787 x 72
149
109
Aileron Differential
ac;ket (est0)
1
500
5.0
L.G. Hinge Fitting
(eat.)
1
25,0
3540
Fence (est.)
1
500
6ao
Wing Panel,, Total
317.8 .
&13.7
43 F-51,5,
am
Bottom Skins .0140 x
19 x 107
811
806
Top Skin, .037 x 20
x ].07
1.
806
902
Nose Skin, .0140 x 2
x 107
1
009
10
Trail Edge, .060 x 2
x 107
1
1.3
103
Ribs, .040 x 14 x 19
(See Wing)
11
109
3.3
Rivets, 1/8 :ono @ 2/i b.
2350
0,,7
:LA
Flap Hinge Fittings
2
l08
+08
Spar, 00140 x 14 x 107
3.
10 7
1.7
2
l1 8
2s5
26.
ate
2$
Spar,.0140x6x60
1
1,4
1.4
,
Tail Edge, 060 x 2 x
67
008
Oy;$
Ribe,~ 037x6x18
(See Wing)
2
0'8
1,5
8.1n0051ax18x63
2
n.4
12.14
Iiingea
2
1.8
1
8
Rivets (See Flap)
0a 8
.
4
3
8
6
6
.
.
1.8
1
.
1609
1.8 1847
W
Gough nctm*e
Front, 023 x8 x
52 } n0
1
1343
1303
L tongs, Steal
2
5o9
1000
Rear, Cap Steel T (Sea
Wing) x 56 in.
2
91 014
272'00
bb,, Dural 080 x 5 x
52
2
142.0
42* 0
Bolts (See Wing.)
805
1740
Nuts
608
608
503
111.07
167.0
a:
503 35B - 361.1
S-E-C=R-F.-T
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 Approved For Release 1999/09/21 : CIA-RDP79-01093A000300020004-0
Trail Edges e06O a 2
ESTIMATED FINISHED I:'EIG~iT AND BILL OF MATERIALS
-
MR t~Itt
A
IROOM AND'A
D:CN
-
ontinu
-
Pounds
Number
of
,.4..
niched
.--~'.~'
1 , 1 o mat -or, US
Item
Pieces
Dural
Steel Total
Dural
Steel Total
Total Wing (Tao Wings
Plus Carry-through)
76609
5II603. 131302
914809
1183.4 213203
Spoileis
1106
406
Total Wing Group
7710,
514603 191701'i
95305
1183.4 12136,9
Bo
Tail. Group o
Spar Cap Tee, 2 x 3 x
3/8 x 97 ino 2
9904
0
345
Webas Dural,, 0080 x 7
,
x 97 (75--ST) 2
1100
i6Qo
Lead Edges
0465 x 10 x 142
2
701
805
x,0465 x h x 142
2
208
303
Bolts, .@ 3/14 ir.,
Pitch 3/8 in-
1g,
x 1 ino
380
3210
3800
Nuts$ 318 ino
380
1104
7.104
Try- Edge, .054 x h
t112
t
1
202
2,2
S
tingersg Alcoa 710135 a 1003 x 125 ino
2
401
4a
10135L- 1003 x 122 ino
`
2
309
309
10135 1003 x 117 in,
2
3Q7
.
307
Ribs, 0037 x 6 x 36
(3 x 3 ino ~ holes)
13
702
1O i1
Ribs Clips Ob x e
x 6 ino
20
1.5
105
1 elage Attache
125
2
0
x
$ x 82 ino
2
4.14
4Q1t
Hinge Brackets, .065
x 4 x 3
>065x4x2 8
0065x2 x2 ? ,g.
0065 x 2 x 2 4 209 209
Skin, 0047 x 57 in, x 36 2 19'.7 2806
0037 x 24 x 147 2 8,,6 2141
Favets 1/8 ino $
2/in 0 2350 101 101,4
Total,
S-E-C-R-E-T
urc sam r.~ ~~ r ~A
6002. 114208 22300 in .7
391464 0601
- fi ^='~ w ~L7Ya~'SFe wi4']i Total
9.4
1 22:8
-16;7 2 43-2
9.4
1306 12,9 26.4
2.22 1886o7_111- -
Iongeanep Alcoa 12061
1
8
8
91
x 310 In
9
,
.
.
12061 x 154 in.
15,,2
1502
12061 x 72 in,
701
701
1,2061 x 260 ino
25.5
2505
Alcoa 10135-0601x
6
6
6,6
156in._
0
165
Dural ?065 x 4 x 156
16,5
Str.ngersg Alcoa 10135
4601 x 124 2
109
109
2
5
66
6
2
2,5
0
01 x 1
10135 - 0
- 0601 x 310
10135
2
4.7
1
,
4.
.
10135-0601x235
2
3.5
305
10135 - 0601 x 280
2
4.2
4,2
10135 e 0601 x'310
2
407
14 7'
10135 - 0601 x 260
2
309
3.9
10.135-0601x310
6
1.10.1.
14.3.
Station
1
10
,125x5x116
3.
6,8
6,8
20
.325 x 5 x 130
1
7.7
707
30
0125 x 5 x 145
1
8.5
8.5
44.4
0125 x 5 x 158
1
9.14
904
6
59
125 x 5 x 126
1
7.5
705
.
78.3
.
.125 x 5 x 130
1
7.7
707..
82.8
.125x5x134
1
709
7.9
94.5
0125 x 5 x 138
1
8