*****AIRCRAFT
“Ilyushin - IL96”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing (winglets)
Engine position: Underwing
mounted
Tail configuration: Regular tail, mid set
Landing gear: Tricycle retractable
Wing Span: 55.4 m
Length: 63.9 m
Height: 15.2 m
Power plant: 300: 4 x 156 kN
Soloiev PS-90A turbofans.
M: 4 x 170 kN P&W PW
2337 turbofans.
Accommodation: Flightcrew of two and 235 (312 in IL-96M) passengers in three classes,
up to 300 (375
in IL-96M) in high density configuration.
Notes: Long range wide-body airliner. In service since 1993 (IL-96M
since 1998).
Russias second wide-body airliner based on the IL-86 with a
modern western design.
IL-96-300
standard version. Stretched development IL-96M. IL-96T freighter version
of IL-96M. New
twin engine version IL-98 under construction. IL-96M: Length 60,1 m, Height
15,2 m, MTOW 270000 Kg.
Alternative names:
ILYUSHIN Il-96.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 270.000 kg
VMO - Maximum Operating Speed 470 KIAS
MMO - Maximum Operating Speed Mach 0.80 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(pitch)
0 210(6°)
200(6°) 190(7°) 180(8°) 170(10°) 160(12°)
STALL LIMIT 150(15°)
1 1° 210(3°)
200(4°) 190(5°)
2 5° 200(1°)
190(2°) 180(3°)
3 10° 180(1°)
170(2°) 160(3°) 150(5°) 140(7°)
gear down 180(1°)
170(2°) 160(3°) 150(5°) 140(7°)
*****Take-off*****
WTC: H
Distance: 2800
mt
V2 (IAS): 150
kts (FLAPS 1)
*****Climbing*****
-(to 5000 ft)
IAS: 180
kt
ROC: 1500
ft/min
-(to FL150)
IAS: 290
kt
ROC: 1500
ft/min
-(to FL240)
IAS: 290
kt
ROC: nd ft/min
-(mach)
mach: 0.72
ROC: 1000
ft/min
*****Cruise*****
TAS: 470
kt
MACh: 0.80 data
Ceiling: FL390
Range: 4800
NM
*****Descent
*****
- (to FL240)
mach: 0.72
ROD: 800
ft/min
- (to FL100)
IAS: 290
kt
ROD: 3000
ft/min
*****Approach*****
IAS: 250
kt
MCS: nd kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 150 kt
APC: D
Distance: 2000
mt