TUPOLEV TU-134A JETLINER

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP78-03066R000400030001-3
• Release Decision: RIPPUB
• Original Classification: K
• Document Page Count: 15
• Document Creation Date: December 19, 2016
• Document Release Date: April 7, 2003
• Sequence Number: 1
• Content Type: REPORT

Apprpyed For Release 2003
STAT
STAT
TUPOLEV
TU - 134 A
Jetliner
General Informat.
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p P*
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.A. GENERAL INFORMATION
. The '113-134 A, a high performance twin turbofan airliner, is a low-wing
monoplane with a swept back T-tail lay-out. The fuselage is of pressurized
semiraonocoque design and has circular cross section,
Its two turbofan engines /type D-30, 2nd series/ have 6 800 kp take-off
thrust each /under ISA conditions/, and are equipped with thrust reversers.
The engines being mounted on the rear part of the fuselage, there is a very
low noise level in the passenger cabins.
The auxilliary power unit TA-8 make the TU-134 A'independent on the
ground equipment for engine-starting, air-conditiorniing and power supply.
On board of the TU-134. A is all the modern radio communication, navi-
gation and radar equipment /including?SS',Z transponder mode A, B, C/, which
ensures high safety standard and regularity of flying under all weather
conditions by day or night, Being so equipped the TU-1.34 A is capable to do
automatic approach under the Weatb:er Minima corresponding ICAO Category
I conditions.
0
The steerable nose gear /max. 55 / as well. as excellent field of vision
from the cockpit enable very -rood. maneuvrability on all airfields /runway
width of only 4.0 in is sufficient for a complete 180 o turn/.
The flight crew consists of two pilots and a navigator.
TU-134 A aircraft,designed for short and medium haul passenger and
cargo transport, can carry 8 200 kgs /1.8078 lb/ payload over 2 000 km
/ 1080 n. m. / distance and 5 000 kgs / 11023 lb/ payload over 3 200 kin
/1730 n.m./ distance.
Standard version cabins offer seating accomodation for 76 passengers.
Three air-hostesses take care of the passengers comfort.
In the rear part of the fuselage, just before the rear cargo comparixrcent,
are two toilets.
There are two cargo compartments -- forward. and rear; both c,n be
loaded through doors on the right side of the fuselage.
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B. MAIN FL1.GHT AND TECiINICAL DATA
Lrei ht limits
Max. ramp /taxi/ weight
Max. take-off weight
Max. landing weight
Max. landing weight in emergency
Dry operating weight
Max. payload
Max. fuel tanks. capacity.
Normal lift-off speed
273 km/hour
147 knots
Decision speed
/V 1 /
255 km/hour
138 knots
Rotation speed
Take-off safety speed
/V /
A.
/V,)/
265 km/hour
?143 knots
273 km/hour
flaps: 20- : Landing-gear retracted
0
147 knots
flaps : 0
: lan.ding-gear retracted 310 km/ hour
167 knots
Take-off run /2--engines/
actual
1 400 m
/4595 ft/
required
1 760 in
/5775 ft/
47
200 kgs
/ 104056 lb/
47
000 kgs
/103615 lb/
43
000 kgs
/ 94797 lb/
47
000 kgs
/103615 lb/
29
000 kgs
/ 63932lb/
8
200 kgs
/ 18077lb/
13
200 kgs
/ 29100 lb/
Take-off per. formance /ISA' TOW : 47000 kgs, flaps : 20 0
/
Take-off distance required /2-engines/
balanced take-off runway length /flaps: 200/ 2.440 m
Climbinn performance
Practical ceiling - take-off weight 11 500 m
.47 000 kgs /103615 lb/
Time, to climb take-off weight
47 000 kgs /103615 lb/-to : - 11. 500 in /FL 380/
- 10 000 m /FL 330/
6000m/FL200/
/ 8005 ft/
/FL 380/
37 min
27 min
13 min
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C limbin
ISA,GS 000 k s,-2ics, nomin~II- rating
- --- _..ti---------------- -
FL
50 100 150 200 250
310
330
350
3"
in/sec
14 12,5 11 9,3 7,4
4,8
3,8
2,8
1s
ft/min
2756 2460 2165 1830. 1450
940
740
550
2
ISA, 45 000 kg,-,l-engine, nominal rating-
F L 50 .100 150 170
m/sec 2,3 1,4. 0,5 0,1
ft/min 450 275 99 20
Landing performance I.SA,LW 43 000 kes 94797 lb_ /,'flaps: 380
, s o ` -
air brakes fully extended, reverse til.rust/
Min, threshold speed VATO
Normal touch--down speed VTD
Landing run
Landing runway length required:
- ICAO /k 1, 43/
- BCAR /k = 1,67/
Landing distance /I1 = 15 m/
Speed limit
Max, IAS /fuel tanks No 3 empty/
Max. IAS /furl tanks. No 3 full /
Max. permissible M
Minimum speeds
Flaps 0? 10? 20? 8?
km/hour ? 330 ? 300 270 270
knots 178 '162. 14-6 146
265 km/hour 143 knots
248 km/hour 134 knots
780 in /2560 ft/
1 920 m /6300 ft/
2 240 m /.7350 ft/
1 340: m /4395 ft/
605km/hour 327 knots
505 km/hour 273 knots
0,82
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Landing speeds
Landing,.,,
V, FD
weight
,_,
_
km/h
_~
knots
km/h knots
47
278
150
262 141
46
275
148
258 1.39
45
272
1.47
255 138
.44
268
145
252 136
4,3
'265
143
248 .13
42
263.
142
245 132
41
260
140
242 131
40
257
139
238 129
39
253
137
235 127..
38
250
135
232 125
37
250
135
232 125
36
250
135
323 125
35
250
135
232 125
f lcline, /1SA, FL 50, G = 41 000 kgs/
Con sumption
T= V
M D V = 1, 05 V. V MD max
V 1,1 V MD max
V = 1,15 VMD max
2 170 kgs/hdur
2 200 kgs/hour
2 260 kgs/hour
2 330 kgs/hour
Aircraft dimensions
Wing Span
Qvera.ll length
oJeral.l height
Wheel track
Wheel base
Speed Knots
338 km/hour 21.0
410 km/hour 221
430 km/hour 232
450 km/hour 243
29,01 m 1142 "
37,322 m 1470"
9,144 m 360"
9,45 m 372"
15, 83 in 623"
Passenger entrance door dimensions
Width
0,7 m
27t56'e
1leight
1,61 m
63, 39
Threshold height above ground level:
2,415 m
95,08
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Carc eC)171 art111C'11ts
Compart- Capacity l;loor Max. YMax.
merit area specific load
load.
forward 6 rm 3, 2n2 600 kgs/m 1920 kgs
42301b
3 . 2
rear 8, 5 111 4, 5m 600 kgs/n 2700 kgs
5950 lg
? Car. o compartment door dimensions
49,21 29,53"
Compartment Width Height Threshold height
m m above ground level
Capacity /in kgs/ of cargo
COT~m rtrnent if to led b~':
Baggage- Car~'o, Mai
3
150 kgs/m 285 fkgs/m`7
900 kgs
1716 k g s
1.985 lb
3770 lb
1275 kgs
2420 kgs
2810 lb
5335 lb
1,250 0,750 2,350
0,905
35,63
"
1,220
48,03?
92,52 11
2-, 341
92,17 .,
Center of gravity limits /with landing gear extended or retracted/
forward limit
21% MAC
a.ft, limit
'38 % MAC
Caution:
At 51', 5 % MAC the aircraft would tilt over and rear end of the fuselage
would fall to the ground; for safety reasons the limit value of 49 % MAC
should never be exceeded. Therefore it is strictly forbidden to load first
the rear cargo compartment or to unload first the forward cargo compartment.
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Maximum permissible crosswind component for take-off and landing-is
14 n1/sec. Maximum permissible tuiilwind component is 10 m/ sec.
Maximum. permissible crosswind component for taxiing and. towing is
30 m/sec.
When towing the aircraft at wind speed higher than 15 rn/sec, the control
surfaces must be locked.
Grow d handlin ee]uiprnent:
For TA-8 A.PU starting: 27-28,5 V DC, 32-36 kW.
For D-30-2 engine starting: 'compressed air 0,635 kgs/ sec at 2,5 - 5, 2 kp/cm2
and
For at oil filling: 103 292 Cfine. 2
oil filter with 8000 - 10 000 holes/cm.
AC ground power unit: 400 Hz, 1-phase 115 V, 6 WA.
u
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Ri 'C) O
? ri ?O
c O NJ F3 `
U ~N U F a
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Ponol ,;ri.th oocapo rope
i'or?taw.o ire 153capo S1lciO
oxtJngulohor si;orod - 1
lamps `~0 -U0
Slido for ova-
,ouatibn through.
ornorgoncy exits
i;scapo
slide
Life jackots Lnorgoncy radios
Slings "Slide Ti 3 . fixing poi :ts
'EMERGENCY EQUIPMENT LOCATION
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 Approved For Release-2003/0.8107 CIA=RDP78-03066R000400030001..-3.
Ft"CM IN31D
Pull the handle up to the stop,
and pu:;h the door in the cabin:
N
NO 01~' x, 'I~RCF.? CY E'S CAP0 HATCHE F, 3
Push. the cover and remove it
Take th handle out?of th.e Eroove
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Lift the lover of safety catch
Pull the handle izaards up to
the atop and remove the door
OPENING Ii ATC ff
FROM OUTSIDE
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No:e whool anglo (degrees).
Lr) - C) LO C) If) Q IC) Ca IC)
Lf) if) `y+ V+ [) C) C\2 C1 I--I
Qa
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T t! ~? 13 ' A
WE G11T ~1) BALANCE MA 1UAL
6,2. Passenger Comb rtlnonts dins nsfon.i
1 ength
-\Vidtlti
Height
Floor ifYi'a_
C rapt 01
1.82
2,71
1.96
4.93 11
Cmpt 02
2.15
2.71
1.96
5.82
Cmpt 03
2..25
2.71
1.96
6.09
C rapt 04
Z-47
2.71
1.96
6.29
Cm.pt 05
2.25
2.71
1.96
6.09
6.3.E Maximum permissible specific floor load in passenger com-'
partrnent: 200 kg p. sq.m.
6.4. Maximum seating capacity:
6.5. l~ reight 11.olds
76 seats
6.5.01 ,Mean dimensions and load limits of freight bolds
F rei,gl-,
Max.
a
Lc h
Mean
Floor
E
lume
Max. spa--.
Maximum load /k~g/
old
he~ig~rt
width
area
.
floor
luggage inail+cargc7
No ,
load
/r~r./
/m./
/m./
sq.m./
ca.m./
kg.p.
150 285
S
/ 1 c,P cum . i - - -
5
1.8
2.5
1.25
3.2
6.0
600
900 1 710
6
1.9
3.2
1.4.0
4.5
8.5
600
1 275 2 420
6.5.02 Freight hold door dimensions
F r?eight hold No. Height Width
~jrrr./ Jm./
Heigh to sill above ground
/Ill./
1.250 0.750
0.905 1,220
2.350
2.31+1
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