*****AIRCRAFT “Ilyushin - IL86/87”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Wing position: High wing

Engine position: Underwing mounted

Tail configuration: Regular tail, mid set

Landing gear: Tricycle retractable

Wing Span: 48.1 m

Length: 59.5 m

Height: 15.8 m

Power plant: 4 x 127 kN Kuznetsov NK-86 turbofans.

Accommodation: Flightcrew of 3 and 234 passengers in two classes, up to 350 in high density configuration.

Notes: Medium range wide-body airliner. In service since 1980.

Soviet Unions first wide-body airliner and model with underwing engines.

Production ceased in 1994 after 107 aircraft were built. In 1999 approx. 90 remain in service, all with Russian and CIS operators (one by Chinese Airline).

Planned CFM re-engined version has been delayed indefinitely.
Alternative names:
ILYUSHIN Il-86/87.

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs - 206.000 kg

VMO - Maximum Operating Speed 490 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                      000

2                      000

5                      000

10                    000

15                    000

25                    000

30                    000

40                    000

 

*****Take-off*****

WTC:               H

Distance:         2600 mt

V2 (IAS):         155 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 185 kt

ROC:               1500 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:               1000 ft/min

 

*****Cruise*****

TAS:                490 kt

MACh:             0.82 data

Ceiling:            FL360

Range:            2000 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:               180 kt

ROD:               1500 ft/min

 

*****Landing*****

Vht (IAS):        150 kt

APC:                D

Distance:         2300 mt