Originally designated as the SA-16 for the USAF and the JR2F-1 and UF-1 for the USN and USCG, it was redesignated as the HU-16 in 1962. An improvement of the design of the Grumman Mallard, the Albatross was developed to land in open ocean situations to accomplish rescues. Its deep-V hull cross-section and keel length enable it to land in the open sea. The Albatross was designed for optimal 4-foot (1.2 m) seas, and could land in more severe conditions, but required JATO (jet-assisted take off, or simply booster rockets) for takeoff in 8–10-foot (2.4–3.0 m) seas or greater. The Royal Canadian Air Force operated Grumman Albatrosses with the designation "CSR-110". In 1970, Conroy Aircraft marketed a remanufactured HU-16A with Rolls-Royce Dart turboprop engines as the Conroy Turbo Albatross, but only one prototype was ever built. For details of operational history and variants, click here. Specifications below are for the UH-16B variant. Albatross
