TUPOLEV Tu-134

Aircraft
Name: 
Tu-134
Manufacturer: 
TUPOLEV
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Low wing
Tail: 
T-tail
WTC: 
M
APC: 
D
Type Code: 
L2J
Engine: 
Jet
Engine Count: 
Multi
Position: 
Both sides of rear fuselage
Landing gear: 
Tricycle retractable
Manufacturered as
TUPOLEV Tu-134

T134

Short range airliner. In service since 1964. Short range airliner development based on TU-124 (initially designated TU-124A). Built in a few versions:

  • TU-134A stretched, more powerful version with re-profiled nose,
  • TU-134B with a glass nose,
  • TU-134B1 for up to 90 passengers and
  • TU-134B3 for up to 96 passengers.

TU-134: Length 34,3 m Height 9,0 m MTOW 44,500kg.

Technical Data
Wing span: 
29.00 m
Length: 
37.10 m
Height: 
9.10 m
Powerplant: 

134: 2 x 64,9 KN Soloviev D-30 turbofans.

Engine Model: 
Soloviev D-30
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
2180 m
MTOW: 
47000 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
440 kts
MACH: 
0.61
Ceiling: 
390
Range: 
1020 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
2050 m

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