*****AIRCRAFT
“Ilyushin - IL62”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: Both sides of rear fuselage
Tail configuration: T-tail
Landing gear: Tricycle retractable
Wing Span: 43.2 m
Length: 53.1 m
Height: 12.4 m
Power plant: 62: 4 x 103 kN Kuznetsov NK-8-4 turbofans.
62M: 4 x 107.9 kN Soloiev D - 30KV turbofans.
Accommodation: Flightcrew of five and typical 174 passengers in
IL-62M
(186 in IL-62, 195 in IL-62MK).
Notes: Medium to long range airliner. In service since 1967. Russian
version of the VICKERS VC10 concept. Improved production Il-62M, appeared in
1971. Third model Il-62MK, with higher MTOW and passenger capacity, since 1978.
Production ceased in 1994. More than 250 aircraft were built including over 75
for export. In 1999 aprox. 49 aircraft remain in
service.
Alternative names:
ILYUSHIN Il-62.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 166.000 kg
VMO - Maximum Operating Speed 460 KIAS
MMO - Maximum Operating Speed Mach 0.82 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 O° 000 380 km/h gear down
2 15° 000 340 km/h gear down
3 30° 000 290 km/h gear down
*****Take-off*****
max weight: 167
t
WTC: H
Distance: 3300
mt
V2 (IAS): 150
kts flaps 15°
*****Climbing*****
-(to 5000 ft)
IAS: 180
kt
ROC: 1000
ft/min
-(to FL150)
IAS: 290
kt
ROC: 1500
ft/min
-(to FL240)
IAS: 290
kt
ROC: 1500
ft/min
-(mach)
mach: 0.72
ROC: 500
ft/min
*****Cruise*****
TAS: 460
kt
MACh: 0.82 data max 0.83
Ceiling: FL410
Range: 4200
NM
max for weight
165t 000lbs 9.600 mts FL000
157t 000lbs 10.100 mts FL000
141t 000lbs 10.600 mts FL000
126t 000lbs 11.100 mts FL000
115t 000lbs 11.600 mts FL000
<109t 000lbs 12.100 mts FL000
*****Descent
*****
- (to FL240)
mach: 0.72
ROD: 800
ft/min
- (to FL100)
IAS: 290
kt
ROD: 3000
ft/min
*****Approach*****
IAS: 250
kt
MCS: 180
kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 130 kt
APC: C
Distance: 2300
mt