PBY Catalina | Consolidated's flying boat and amphibious aircraft | World War II Seaplane | Upscaled

The Consolidated PBY Catalina is a flying boat and amphibious aircraft that was produced in the 1930s and 1940s. In Canadian service it was known as the Canso. It was one of the most widely used seaplanes of World War II. Catalinas served with every branch of the United States Armed Forces and in the air forces and navies of many other nations. The last military PBYs served until the 1980s. As of 2021, 86 years after its first flight, the aircraft continues to fly as a waterbomber (or airtanker) in aerial firefighting operations in some parts of the world. None remain in military service.

The PBY was originally designed to be a patrol bomber, an aircraft with a long operational range intended to locate and attack enemy transport ships at sea in order to disrupt enemy supply lines. With a mind to a potential conflict in the Pacific Ocean, where troops would require resupply over great distances, the U.S. Navy in the 1930s invested millions of dollars in developing long-range flying boats for this purpose. Flying boats had the advantage of not requiring runways, in effect having the entire ocean available.
As American dominance in the Pacific Ocean began to face competition from Japan in the 1930s, the U.S. Navy contracted Consolidated, Martin and Douglas in October 1933 to build competing prototypes for a patrol flying boat. Naval doctrine of the 1930s and 1940s used flying boats in a wide variety of roles that today are handled by multiple special-purpose aircraft. The U.S. Navy had adopted the Consolidated P2Y and Martin P3M models for this role in 1931, but both aircraft were underpowered and hampered by inadequate range and limited payloads.

Consolidated and Douglas both delivered single prototypes of their new designs, the XP3Y-1 and XP3D-1, respectively. Consolidated's XP3Y-1 was an evolution of the XPY-1 design that had originally competed unsuccessfully for the P3M contract two years earlier and of the XP2Y design that the Navy had authorized for a limited production run. Although the Douglas aircraft was a good design, the Navy opted for Consolidated's because the projected cost was only $90,000 per aircraft.


PBY waist gunner mounting port side gun blister
Consolidated's XP3Y-1 design (company Model 28) had a parasol wing with external bracing struts, mounted on a pylon over the fuselage. Wingtip stabilizing floats were retractable in flight to form streamlined wingtips and had been licensed from the Saunders-Roe company. The two-step hull design was similar to that of the P2Y, but the Model 28 had a cantilever cruciform tail unit instead of a strut-braced twin tail. Cleaner aerodynamics gave the Model 28 better performance than earlier designs. Construction is all-metal, stressed-skin, of aluminum sheet, except the ailerons and wing trailing edge, which are fabric covered.

The prototype was powered by two 825 hp (615 kW) Pratt & Whitney R-1830-54 Twin Wasp radial engines mounted on the wing's leading edge. Armament comprised four .30 in (7.6 mm) Browning AN/M2 machine guns and up to 2,000 lb (910 kg) of bombs.

The XP3Y-1 had its maiden flight on 21 March 1935, after which it was transferred to the U.S. Navy for service trials. The XP3Y-1 was a significant performance improvement over previous patrol flying boats. The Navy requested further development in order to bring the aircraft into the category of patrol bomber, and in October 1935, the prototype was returned to Consolidated for further work, including installation of 900 hp (670 kW) R-1830-64 engines. For the redesignated XPBY-1, Consolidated introduced redesigned vertical tail surfaces which resolved a problem with the tail becoming submerged on takeoff, which had made lift-off impossible under some conditions.
General characteristics

Crew: 10 (pilot, co-pilot, bow turret gunner, flight engineer, radio operator, navigator, radar operator, two waist gunners and ventral gunner)
Length: 63 ft 10.875 in (19.47863 m)
Wingspan: 104 ft (32 m)
Height: 21 ft 1 in (6.43 m)
Wing area: 1,400 sq ft (130 m2)
Aspect ratio: 7.73
Empty weight: 20,910 lb (9,485 kg)
Max takeoff weight: 35,420 lb (16,066 kg)
Zero-lift drag coefficient: 0.0309
Drag area: 43.26 ft2 (4.02 m2)
Powerplant: 2 × Pratt & Whitney R-1830-92 Twin Wasp 14-cylinder air-cooled radial piston engines, 1,200 hp (890 kW) each
Propellers: 3-bladed constant-speed propellers
Performance

Maximum speed: 196 mph (315 km/h, 170 kn)
Cruise speed: 125 mph (201 km/h, 109 kn)
Range: 2,520 mi (4,060 km, 2,190 nmi)
Service ceiling: 15,800 ft (4,800 m)
Rate of climb: 1,000 ft/min (5.1 m/s)
Lift-to-drag: 11.9
Wing loading: 25.3 lb/sq ft (124 kg/m2)
Power/mass: 0.067 hp/lb (0.110 kW/kg)
Armament
Guns: 3 x .30 cal (7.62 mm) machine guns (two in nose turret, one in ventral hatch at tail)
2 x .50 cal (12.7 mm) machine guns (one in each waist blister)
Bombs: 4,000 lb (1,814 kg) of bombs or depth charges; torpedo racks were also available

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