Lockheed Martin C-130J

GENERAL

Description
Variants CC-130J, EC-130J, HC-130J, KC-130J, MC-130J, WC-130J
Manufacturer Lockheed Martin
First Flight 5th April 1996
Launch Organisation United States Air Force, Feb 1999
Largest Operator United States Air Force
First Registered In India 5th Feb 2011, Indian Air Force
Users In India Indian Air Force

Wake Turbulence Category M
Aerodrome Reference Category
Approach Category C
2900 nm
Range
320 Kts
Cruise Speed
134
Passengers Carried
Total in India
19,000 Kgs
Payload
40,000
Service Ceiling
US$ 75.5m
Price
516
Number Built


Takeoff 1,000m
Landing 780m

RUNWAY REQUIRED AT MTOW/MLW

SPECIFICATIONS

Crew 3
Passenger Capacity 134
Length 29.8 m
Wingspan 40.41 m
Height 11.84 m
Wing Area 162 sqm
Max Ramp Weight 70,300 Kgs
Fuel Capacity 20,500 L
Engine RR AE2100
Thrust 4,637 SHP

Fleet Detail

MSN TAIL MAKER MODEL ENGINE CONF FIRST FLT LESSOR REMARKS

GALLERY