Lockheed C-130H HERCULES

The C-130E is an extended-range development of the C-130B. A total of 369 were ordered and deliveries began in April 1962. The maximum ramp weight of the E-model increased to 155,000 pounds (70,307kg), 20,000 pounds (9,072kg) more than the B-model. Its fuel capacity was increased by over 17,000 pounds (7,711kg). More powerful Allison T-56-A-7A engines were used and a pair of external fuel tanks with a capacity of 1,360 gallons were slung beneath the wings, between the engines. A recent wing modification to correct fatigue and corrosion on the USAF’s fleet of E-models has extended the life of the aircraft well into the 21st century.

Similar to the E-model, the C-130H has updated T56-A-T5 turboprops, a redesigned outer wing, updated avionics, and other minor improvements. Delivery began in July 1974 [other sources state April 1975]. More than 350 C-130Hs and derivatives were ordered for active and reserve units of the U.S. services. The H-model has become the most produced of all C-130 models, with orders for 565 as of the end of 1979.

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