ILYUSHIN Il-62

Aircraft
Name: 
Il-62
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Low wing
Tail: 
T-tail
WTC
H
APC
C
Type Code: 
L4J
Engine: 
Jet
Engine Count: 
Multi
Position: 
Both sides of rear fuselage
Landing gear: 
Tricycle retractable
Manufacturered as
ILYUSHIN Il-62

IL62

Medium to long range airliner. In service since 1967. Russian version of the VICKERS VICKERS VC-10 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.

Technical Data
Wing span: 
43.20 m
Length: 
53.10 m
Height: 
12.40 m
Powerplant: 

62: 4 x Kuznetsov NK-8-4 (103 kN) turbofans62M: 4 x Soloviev D-30KV (107.9 kN) turbofans.

Engine Model: 
Kuznetsov NK-8, Soloviev D-30
Indicative Performance Data
Take-Off
V2: 
150 kts
Distance: 
3300 m
MTOW: 
165000 kg
Initial Climb (to 5000 ft)
IAS: 
180 kts
ROC: 
1000 ft/min
Initial Climb (to FL150)
IAS: 
290 kts
ROC: 
1000
Initial Climb (to FL240)
IAS: 
290 kts
ROC: 
800 ft/min
MACH Climb
MACH: 
0.72
ROC: 
500 ft/min
Cruise
TAS: 
460 kts
MACH: 
0.82
Ceiling: 
390
Range: 
5200 NM
Initial Descent (to FL240)
MACH: 
0.72
ROD: 
800 ft/min
Descent (to FL100)
IAS: 
290 kts
ROD: 
1500 ft/min
Descent (FL100 & below)
IAS: 
n/a
MCS: 
180 kts
ROD: 
n/a
Approach
Vapp (IAS): 
145 kts
Distance: 
2300 m

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