*****AIRCRAFT
“Tupolev - TU124”*****
REFERENCE INFORMATION (by Tupolev
network and others)
*****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: 25.55 m
Length: 31.57 m
Height: 8.08 m
wing area, m2 - 119.37
Power plant: double-flow turbofans Soloviev
D-20P with the thrust 5500 kgs
(54 kN – 12140 lb) each.
When needed, the emergency power boost system can increase the thrust to 5800 kgs (56.9 kN – 12790 lb).
Flightcrew of
four/five and typical 44-56 passengers.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 38.000 kg
VMO - Maximum Operating Speed 000 KIAS
MMO - Maximum Operating Speed Mach nd 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 degr KIAS
1
2
5
10 215
15
25
30 140
40 183
*****Take-off*****
WTC: M
Distance: 0000
mt
VR=210-230 km/h (113-124 kts)
V2 (230-240 km/h - 124-130 kts)
TOW tons 38
37 36 35 34 33
32 30
Vt km/h 260
255 250 245 245 240
235 230
TOW lbsx1000 84.2
82 79.8
77.6 75.4 73.2 70.9 66.5
Vt kts 140 138 135 132 132
130 127 124
*****Climbing*****
-(to 5000 ft)
IAS: 190
kt
ROC: 600
ft/min
-(to FL150)
IAS: 000
kt
ROC: 0000
ft/min
-(to FL240)
IAS: 000
kt
ROC: nd ft/min
-(mach)
mach: 0.00
ROC: 0000
ft/min
*****Cruise*****
TAS: 780-800
km/h 421-432 kts
MACh: 0.65 data
Ceiling: FL380
Range: 1134 NM
*****Descent
*****
- (to FL240)
mach: 0.00
ROD: 000
ft/min
- (to FL100)
IAS: 216
kt
ROD: 1370
ft/min
*****Approach*****
IAS: 146
kt
MCS: 135
kt
ROD: 0000
ft/min
*****Landing*****
Vht
(IAS): 000 kt
APC: 0
Distance: 0000
mt
Landing weight,
t Less
than 30 32 33
35
Landing speed, km/h
220 225 230 235
Landing weight,
lbs Less
than 66100 70500 72700
77100
Landing speed, kts 118 121 124
127