*****AIRCRAFT
“Tupolev - TU134”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing (anhedral
with cone)
Engine position: Both sides of rear fuselage
Tail configuration: T-tail
Landing gear: Tricycle retractable
Wing Span: 29.0 m
Length: 37.1 m
Height: 9.1 m
Power plant: 134: 2 x 64,9 KN Soloviev
D-30 turbofans.
134A: 2 x 68 kN Soloviev D-30-II turbofans.
Accommodation: Flightcrew of four and typical 66 passengers in two classes-, 72 in
single class configuration
(84 in
Tu-134A, 96 in Tu-134B).
Notes: 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 44500 Kg.
Alternative names:
TUPOLEV Tu-134.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 47.000 kg
VMO - Maximum Operating Speed 430 KIAS
MMO - Maximum Operating Speed Mach 0.75 Mach
Turbulent Air Penetration Speed 000 KIAS/.00 Mach
VLO - Maximum Gear Operating Speed 000 KIAS
VLE - Maximum Landing Gear Extension Speed 000 KIAS/.00 Mach
*****Maximum
Flap Placard Speeds*****
Flaps degrees KIAS
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: M
Distance: 2200
mt
V2 (IAS): 150
kts
*****Climbing*****
-(to 5000 ft)
IAS: 180
kt
ROC: 2000
ft/min
-(to FL150)
IAS: 270
kt
ROC: 1500
ft/min
-(to FL240)
IAS: 270
kt
ROC: nd ft/min
-(mach)
mach: 0.70
ROC: 1000
ft/min
*****Cruise*****
TAS: 430
kt
MACh: 0.75 data
Ceiling: FL390
Range: 1200
NM
*****Descent
*****
- (to FL240)
mach: 0.70
ROD: 800
ft/min
- (to FL100)
IAS: 270
kt
ROD: 3500
ft/min
*****Approach*****
IAS: 250
kt
MCS: 180
kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 150 kt
APC: D
Distance: 2.100
mt