Ilyushin IL38

GENERAL

Description
Wake Turbulence Category M
Aerodrome Reference Category
Approach Category
Variants II 38, II 38M, II 38MZ, II 38N
Manufacturer Ilyushin
First Flight 28th Sept 1961
Launch Organisation
Largest Operator
First Registered In India
Users In India Indian Naval Air Arm

5,130 nm
Range
M 0.70
Cruise Speed
64
Passengers Carried
Total in India
Payload
32,808
Service Ceiling
Price
58
Number Built


Takeoff
Landing

RUNWAY REQUIRED AT MTOW/MLW

SPECIFICATIONS

Crew 6
Passenger Capacity 140
Length 46.60 m
Wingspan 50.50 m
Height 14.80 m
Wing Area 300 sqm
Max Ramp Weight 190,000 Kgs
Fuel Capacity 109,777 L
Engine Soloviev D-30KP
Thrust 26,460 Lbs

Fleet Detail

MSN TAIL MAKER MODEL ENGINE CONF FIRST FLT LESSOR REMARKS