Fokker F.IV

Specifications

1st Flight 1921

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)

Variants

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

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