PW-2 | |
---|---|
![]() | |
Role | Monoplane fighter
Type of aircraft
|
National origin | United States |
Manufacturer | Loening Aeronautical Engineering |
Designer | Grover Loening |
First flight | 1920 |
Primary user | United States Army Air Corps |
Number built | 7 |
Developed from | Loening M-8 |
The Loening PW-2 was a 1920s American single-seat monoplane fighter designed by Grover Loening and built by his Loening Aeronautical Engineering Company.
Based on the earlier two-seat braced-wing monoplane fighter, the M-8, the PW-2 was a single-seat variant for the United States Army Air Corps. It had a fixed tailskid landing gear and was powered by a nose-mounted Wright-Hispano H engine with a tractor propeller. The pilot had an open cockpit. The company built three prototypes designated the PW-2 and a production order for 10 aircraft designated the PW-2A followed. The PW-2As were similar to the PW-2 but had a revised tail unit. After four aircraft had been delivered, one aircraft crashed when the wings separated from the aircraft; the contract was canceled. One of the PW-2As was modified with shorter-span wings and a 350 hp (260 kW) Packard 1A-1237 engine as the PW-2B.
Data from Fighters of the United States Air Force [1]
General characteristics
Performance
Armament
Related development
Related lists
Loening aircraft
| |
---|---|
Company designations |
|
Fighters |
|
Air Ambulance |
|
Observation |
|
Racer |
|
Army Seaplane |
|
Submarine-based Scouts |
|
USAAS fighter (pursuit) designations 1919-1924
| |
---|---|
Pursuit, Air-cooled |
|
Pursuit, Ground-attack |
|
Pursuit, Night |
|
Pursuit, Special |
|
Two-seat Pursuit |
|
Pursuit, Water-cooled |
|