Usage

Experimenta l

Wing Construction

Metal

Capacity

Pilot

Motor type

Two Franklin (0-540-7) engines

Power

2 x 375 HP

Length

17.79 ft (5.4 m)

Span

60 ft (18.3 m)

Fuel

100 gal

Ceiling

21,500 ft

Enduranc e

3.2 hours

Weight

Approx. 7000 lbs (3175 kg)

Wing Area

490 ft2 (45.5 m²)

Aspect Ratio

7.35

Pilot position

Seated