Fokker F.IV / T-2

The Fokker F.IV was designed in the Netherlands in the early 1920s, only two were built for the United States Army Air Service, designated as T-2.

Specifications

Crew

One pilot

Capacity

12 passengers

Length

15.00 m (49 ft 3 in)

Wingspan

24.80 m (81 ft 4 in)

Height

3.34 m (11 ft 0 in)

Wing area

34.6 m2 (372 sq ft)

Empty weight

2,250 kg (4,960 lb)

Gross weight

3,460 kg (7,630 lb)

Powerplant

1 × Packard-built Liberty L12 piston engine , 298 kW (400 hp)

Performance

Maximum speed

150 km/h (93 mph, 81 kn)

Range

4,100 km (2,550 mi, 2,220 nmi)

Service ceiling

3,200 m (10,500 ft).