This is the final and user friendly variant of the P-75 Eagle.
It's easy to controll and very manuverable.

AG1: Bombs
AG2: Ejection Seat
AG3: Parachute

Take-off with 40% throttle

General characteristics

- Crew: One
- Length: 40 ft 5 in (12.32 m)
- Wingspan: 49 ft 4 in (15.04 m)
- Height: 15 ft 6 in (4.72 m)
- Wing area: 347 ft² (32.24 m²)
- Empty weight: 11,495 lb (5,214 kg)
- Loaded weight: 19,420 lb[7] (8808 kg)
- Max. takeoff weight: 18,210 lb (8,260 kg)
- Powerplant: 1 × Allison V-3420-23 liquid-cooled 24-cylinder double-Vee, 2,885 hp (2,150 kW)

Armament

6x .50 caliber (12.7 mm) wing mounted machine guns
4x .50 caliber (12.7 mm) fuselage mounted machine guns
2x 500 lb (227 kg) bombs

The General Motors/Fisher P-75 Eagle was a fighter aircraft designed by the Fisher Body Division of General Motors. Development started in September 1942 in response to United States Army Air Forces requirement for a fighter possessing an extremely high rate of climb, using the most powerful liquid-cooled engine then available, the Allison V-3420. The program was cancelled after only a small number of prototypes and production aircraft had been completed, as it was no longer required in its original role, could not be quickly deployed, and possessed no significant advantages over aircraft already in production.