Grumman

Grumman C-2 Greyhound

The Grumman C‑2 Greyhound is a twin‑engine, high‑wing transport aircraft designed for the United States Navy to replace the aging Douglas R5D. First flown on 26 July 1964, it entered service in 1966 and has since become the Navy’s primary carrier‑based logistical workhorse. Built by Grumman (later Northrop Grumman) in Bethpage, New York, the Greyhound features a rugged airframe, a spacious cargo hold measuring 68 feet in length, and a rear ramp that allows rapid loading of vehicles, pallets, and personnel. Powered by two General Electric TF34‑100 turbofan engines, it delivers a cruise speed of roughly 480 knots and a range exceeding 1,300 nautical miles, enabling nonstop trans‑Pacific missions between carriers and shore bases. Advanced avionics, a reinforced landing gear for carrier operations, and a distinctive T‑tail provide reliable performance in harsh maritime environments. Over more than five decades the C‑2 has supported combat operations, humanitarian relief, and scientific research, proving essential for fleet sustainment. Its longevity and continual upgrades underscore its significance as a versatile, dependable element of naval aviation and a testament to Grumman’s legacy in carrier aircraft design.

Dimensions

Length
17.32 metre

Production & History

Units Produced
58
First Flight
1964
Service Entry
1966

Design & Classification

Country of Origin
Manufacturer
Grumman
Developer
Grumman
Nickname
Greyhound
Operator
United States Navy
Wikidata ID
Q1148532