Piaggio P.136
Amphibious Utility Aircraft
The Piaggio P.136 is a twin-engined five-seat amphibious utility aircraft produced by the Italian manufacturer Rinaldo Piaggio S.p.A. (today Piaggio Aero Industries S.p.A.).
The Piaggio P.136-L1 and P.136-L2 were marketed, assembled and later also license-built in the USA by Kearney and Trecker Corporation as the Royal Gull.
| Propulsion | 2 Piston Engines |
| Engine Model | Lycoming GO-480-B |
| Engine Power (each) | 254 kW | 340 hp |
| Speed | 335 km/h | 181 kts
208 mph |
| Service Ceiling | 7.800 m | 25.590 ft |
| Range | 1.450 km | 783 NM
901 mi. |
| Empty Weight | 2.110 kg | 4.652 lbs |
| max. Takeoff Weight | 2.995 kg | 6.603 lbs |
| Wing Span | 13,53 m | 44 ft 5 in |
| Wing Area | 25,1 m² | 270 ft² |
| Length | 10,80 m | 35 ft 5 in |
| Height | 3,83 m | 12 ft 7 in |
| First Flight | 1948 |
| Production Status | out of production |
| Total Production | 65 |
| ICAO Code | P136 |
| Data for (Version) | Piaggio P.136-L-2 |
| Variants | P.136-L, P.136F, P.136-L1, P.136-L2, Kearney and Trecker Royal Gull (P.136-L1 / -L2) |
