*****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