T134
TUPOLEV Tu-134
TUPOLEV Tu-134
Aircraft
Name
Tu-134
Manufacturer
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
Manufactured 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 (metric)
29.00 m
Length (metric)
37.10 m
Height (metric)
9.10 m
Powerplant
134: 2 x 64,9 KN Soloviev D-30 turbofans.
Engine Model(s)
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
