P-26A Peashooter
| GENERAL DATA | |||
| Other Designation(s) | Boeing
266 |
||
| Type | Fighter |
Crew | 1 |
| Manufacturer(s) | Boeing |
||
| Production | 111 |
||
| First Flight | 20 March 1932 |
Introduction | ? |
| DIMENSIONS | |||
| Empty Weight | 996 kg |
Loaded Weight | 1524 kg |
| Max takeoff weight | ? kg |
Length | 7.18 m |
| Wingspan | 8.50 m |
Wing area | 13.89 m² |
| Height | 3.04 m |
Wing loading | 96 kg/m² |
| ARMAMENT | |||
| Main Guns | 2 × .30 in (7.62 mm) M1919
Browning MG* |
Ammunition Carried | ? |
| Secondary Guns | - |
Ammunition Carried | - |
| Other Armament | 2 × 45 kg GP bombs or 5 x
14 kg anti-personnel bombs |
||
(*) or one remplaced by a 1 x .50 (12.5mm) caliber machine guns.
| POWERPLANT | |||
| Engine | 1 × Pratt & Whitney R-1340-7
"Wasp" radial |
Type & Displacement | 9-cylinder air-cooled single-row,
22 L |
| Horsepower (maximum) | 600
hp |
Power/Weight Ratio | 394 hp / ton * |
| Fuel Capacity |
? L
|
||
(*) with loaded weight
| PERFORMANCES | |||
| Maximum Speed | 377 km/h
at 1800 m |
Cruise Speed | ? km/h |
| Stall Speed * | ? km/h |
Service Ceiling | 8350 m |
| Rate of Climb | 3.65 m/s |
Range | 580 km (1020 km w/external fuel tanks) |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | |||
Drawings |
File |
