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Piaggio P.136
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Top speed
335 km/h
Length
11 m
Manufacturer
Piaggio Aerospace
Wingspan
14 m
First flight
1948
The Piaggio P.136 was an Italian twin-engine amphibian flying boat, with an all-metal hull, pusher propellers, a gull wing, and retractable landing gear.
The prototype first flew in late 1948, and completed certification tests in spring 1949. The Italian Air Force contracted for 14 P.136s for coastal patrol and air-sea rescue. The aircraft was marketed in the United States as the Royal Gull, by Kearney and Trecker. Trecker received three aircraft, and components for another 29, but they also built a few under license.
Variants
P.136F
Variant with Franklin engines, mainly produced for the Italian Air Force, 18 built.
P.136L
Variant with Lycoming GO-435 engines, two built and one P.136F converted.
P.136L-1
Five-seat amphibian flying boat, powered by two 201-kW (270-hp) Avco Lycoming GO-480-B engine, 18 built.
P.136L-2
Five-seat amphibian flying boat, powered by two 254-kW (340-hp) Avco Lycoming GSO-480 piston engines, 24-assembled in the United States from Italian supplied kits.
Royal Gull
Both the P.136-L1 and P.136-L2 were marketed in the United States by the Kearney and Trecker Corporation.
Military operators
Italy
Italian Air Force operated 22 aircraft (14 Piaggio P-136F and eight Piaggio P-136L-1s) from 1951 until 1961
Peru
Peruvian Air Force - four aircraft (one P.136 and three P.136L-2s)
Specifications (variant)
Data from Donald, David, ed. (1997). The Encyclopedia of World Aircraft. Prospero Books. p. 733. ISBN 1-85605-375-X.
General characteristics
Capacity: five
Length: 10.80 m (35 ft 5.25 in)
Wingspan: 13.53 m (44 ft 4.75 in)
Height: 3.83 m (12 ft 6.75 in)
Wing area: 25.10 m2 (270.18 ft2)
Empty weight: 2110 kg (4652 lb)
Gross weight: 2995 kg (6603 lb)
Powerplant: 2 × Avco Lycoming GSO-480 flat-six piston, 254 kW (340 hp) each each
