The first 22 aircraft built were PBYs and were built in the USA. Also built by Boeing Aircraft of Canada at their Vancouver plant, as the PB2B-1. Fifty-five Boeing Canada-built PBY-5 were eligible for conversion to 28-5ACF status which allows further conversion to air transport category.
Production as a pure flying-boat ended with the PBY-4, for the last of these was converted to an amphibian with retractable tricycle-type landing gear, under the designation XPBY-5A. Subsequent aircraft had this as standard.
Production of the PBY series would be undertaken by Consolidated in the United States, Canadian Vickers and Boeing of Canada in Canada, the Naval Aircraft Factory in Britain and state factories in the Soviet Union under the Lend-Lease Act. Between 27 and forty Model 28 Catalinas were built in the Soviet Union as the MP-7.
Initial export aircraft went to Russia, where the type was built subsequently in large numbers under the designation GST. The RAF acquired a single example for evaluation in 1939 and almost immediately ordered a batch of 50, the first of many to serve with Coastal Command. The name Catalina (adopted first by the RAF) was used later by the USN for the various versions which entered service. The type was also to serve with the RAAF, RCAF, RNZAF and the air arm of the Dutch East Indies.
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The RNZAF operated 56 Catalinas, both PBY-5 and PB2B-1 models. They were used for maritime reconnaissance and air-sea rescue between 1943 and 1956. The PBYs were withdrawn from service post-war and sold for scrap in 1952; the PB2Bs soldiered on until replaced by Short Sunderlands in 1953-54.
A number were operated by the USAAF as OA-10As. Seventy-five went to the USAAF as OA-10B in 1945.
In 1964 the province of Quebec, Canada, was using seven modified PBY to reduce forest fires. Field Aviation of Toronto modified the PBY to carry 800 USG of water that could be dumped in 0.8 sec and refilled in 14 sec during a touch and go on lakes or rivers.
Canso PBY-5A
Engines: 2 Pratt & Whitney R1830 Twin Wasp, 1200 hp.
Wingspan: 104 ft.
Length: 63 ft 10.5 in.
Fuel cap: 6500 lt.
Empty wt: 20,913 lbs.
MAUW: (military): 36,400 lbs (16,51l kg).
Max speed: 179 mph.
Range: 2350 sm (3728 km).
PB2B-1
Engines: 2 Pratt & Whitney R1830 Twin-Wasp, 1200 hp.
Length: 65.1 ft (19.83 m).
Wing span: 104 ft. (31.7 m).
Weight empty: 14,240 lb. (6,465 kg).
Crew: 8-9.
Armament: 4 x mg.
Max. bomb load: 2,000 lb. (900 kg).
Cruise speed: 180 mph (290 kph).
Ceiling: 24,000 ft (7,300 m).
Range: 4,000 miles (6,400 km).
Canadian Vickers PBY-5A
Engines: 2 x Pratt & Whitney R-1830-92 Twin Wasp, 1200 hp
Wing Span: 104ft (31.7m)
Length: 63ft 10.5in (19.47m)
Height: 20ft 2in (6.15m)
Speed: 199 mph (322 km/h)
Range: 2,545 miles(4,095 km)
Armament: six .303 Brownings and 4,000lb (1,816kg) of depth charges