C-130J Super Hercules (Military
transport) – 177
Manufacturer: Lockheed
Martin
First flight: 5
April 1996
Introduction: 1999
Produced: 1996-present
Number built: 300
as of 18 December 2013
Unit cost: $67.3
million (flyaway cost, USAF, FY2014)
Developed from: Lockheed
C-130 Hercules
Crew: 3 (two
pilots, and one loadmaster are minimum crew)
Capacity:
92 passengers (128 for C-130J-30); or
64 airborne troops (92 for C-130J-30); or
6 pallets (8 pallets for C-130J-30); or
74 litter patients with 2 medical personnel (97
litters for C-130J-30);
2–3 Humvees, or 1 LAV III (with turret removed) or an
M113 armored personnel carrier
Payload: 19,050 kg
(for C-130J-30 – 19,958 kg)
Length: 29.79 m
(for C-130J-30 – 34.36 m)
Wingspan: 40.41 m
Height: 11.84 m
Wing area: 162.1
m²
Empty weight:
34,274 kg
Useful load:
33,000 kg
Max. takeoff
weight: 79,378 kg; normal: 70,305 kg
Powerplant: 4×
Rolls-Royce AE 2100D3 turboprop, 4,637 shp (3,458 kW) each
Propellers: Dowty
R391 6-blade composite propeller, 1 per engine
Maximum speed: 671
km/h
Cruise speed: 643
km/h
Range: 5,250 km
Service ceiling:
8,615 m with 19,090 kg payload
Absolute altitude:
12,310 m
Takeoff distance:
953 m at 70,300 kg gross weight
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