C-130J Capabilities

Maximum Cruise Speed 355 KTAS (657 km/h)
Airdrop Speed up to 250 KTAS (463 km/h)
Maximum Engine Power 4,591 SHP each
Maximum Take-off Weight (MTOW) at 2.5g 74,389 kg (164,000 lbs)
Maximum Take-off Weight (MTOW) at 2.25g 79,379 kg (175,000 lbs)
Take-off Distance Over 50 feet (S/L, ISA, 164,000 lbs)
Normal
1,783 m (5,850 ft)
Take-off Roll (S/L, ISA, 164,000 lbs) Maximum Effort 945 m (3,100 ft)
Maximum Landing Weight 74,389 kg (164,000 lbs)
Maximum Landing Weight at 9 feet per second 61,235 kg (135,000 lbs)
Landing Distance Over 50 feet (S/L, ISA, 135,000 lbs) Normal 914 m (3,000 ft)
Landing Ground Roll (S/L, ISA, 135,000 lbs) Maximum Effort 496 m (1,630 ft)
Operating Weight Empty 39,094 kg (86,188 lbs)
Maximum Payload at 2.5 g 21,687 kg (47,812 lbs)
Maximum Fuel (JP-8) 19,758 kg (43,560 lbs)
Maximum Zero Fuel Weight (Structural Reserve Fuel) 57,153 kg (126,000 lbs)
Maximum Zero Fuel Weight (with Wing Bending Relief Fuel) 60,781 kg (134,000 lbs)
Maximum Range (without Tanks) 6,852 km (3,700 nm)
Range with 40,000 lbs payload at 2.5 g 4,408 km (2,380 nm)
Cruising Altitude at MTOW 8,230 m (27,000 ft)
Service Ceiling at MTOW 8,839 m (29,000 ft)