Grumman

Grumman J2F Duck

The Grumman J2F Duck, developed in the late 1930s for the United States Navy, was a distinctive amphibious biplane that combined the utility of a floatplane with the convenience of conventional land operations. Drawing on Grumman’s experience with carrier‑based aircraft, the Duck featured a welded steel tube fuselage, a large central pontoon that could be lowered for water landings, and retractable conventional landing gear, allowing it to operate from airfields, aircraft carriers, and open seas. Powered initially by a Wright R‑1820 Cyclone radial engine delivering 1,050 hp, later variants received more powerful Pratt & Whitney R‑2800 engines, boosting speed to over 200 mph and extending range to 1,300 miles. First entering service in 1939, the J2F proved invaluable during World War II as a rescue, transport, and liaison platform, notably retrieving downed pilots from perilous oceanic zones and delivering supplies to remote outposts. Its rugged construction and adaptability earned it a reputation for reliability under harsh conditions. Though modest in numbers, the Duck’s dual‑mode capability set a precedent for future amphibious designs and highlighted the strategic advantage of versatile aircraft capable of supporting naval and humanitarian missions alike.

Classification

Production & History

Units Produced
632
First Flight
1933
Service Entry
1936

Design & Classification

Country of Origin
Manufacturer
Grumman
Developer
Grumman
Nickname
Duck
Wikidata ID
Q1550402