IL62
ILYUSHIN Il-62
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 (metric)
43.20 m
Length (metric)
53.10 m
Height (metric)
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(s)
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
