*****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                  210(3°) 200(4°) 190(5°)

2                  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