*****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