Fokker F.VII

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Fokker F.VII
Type Passenger & military transport
Manufacturer Fokker
Maiden flight 1924
Introduced 1925
Primary users SABENA
KLM
Polish Air Force
Polskie Linie Lotnicze LOT
Produced 1925-1932
Developed from Fokker F.V

The Fokker F.VII was an airliner produced in the 1920s by the Dutch aircraft manufacturer Fokker, Fokker's American subsidiary Atlantic Aircraft Corporation, and other companies under licence. The original Walter Rethel design of 1924 was a single-engined high-winged monoplane. Anthony Fokker modified the design with two additional engines to enter the inaugural Ford Reliability Tour in 1925, which it won. Consequently the production versions F.VIIa/3m, F.VIIb/3m and F.10 all had three engines, and the aircraft became popularly known as the Fokker Trimotor.[1]

Contents

[edit] Operational history

The Josephine Ford at The Henry Ford.
The Josephine Ford at The Henry Ford.
The Southern Cross in 1943.
The Southern Cross in 1943.

The 8- to 12-passenger F.VII was the aircraft of choice for many early airlines, both in Europe and the Americas. Along with the similar Ford Trimotor, it dominated the American market in the late 1920s. However, the popularity of the Fokker quickly came to an end after the 1931 death of Notre Dame football coach Knute Rockne in the crash of TWA Flight 599. The subsequent investigation, which revealed problems with the Fokker's plywood-laminate construction, resulted in the banning of the aircraft on commercial flights, and the rise of all-metal aircraft such as the Boeing 247 and Douglas DC-2.[2]

[edit] Pioneers and Explorers

The F.VII was used by many explorers and aviation pioneers, including:

  • Amelia Earhart became the first woman to fly across the Atlantic on June 17, 1928, as a passenger aboard the Fokker F.VIIb/3m Friendship.[3]

[edit] Variants

F.VII
Single-engined transport aircraft, five built.
F.VIIa (F.VIIa/1m)
Single-engined transport aircraft, slightly larger than F.VII with new undercarriage and wing. Flown on 12 March 1925. First aircraft had 420 hp inline Packard Liberty engine but remaining 39 F.VIIa had mostly radial Bristol Jupiter or Pratt Whitney Wasp engines.
F.VIIa/3m
Version with two additional underwing engines, flown on 4 September 1925. The first two aircraft were identical to the F.VIIa. From the third aircraft, the fuselage was 80cm longer and was powered by with 200 hp (147 kW) Wright J4 Whirlwind radial engines. Probably only 18 were built while many F.VIIas were upgraded to the F.VIIa/3m standard.

First two Fokker F.VIIAs were converted into three-engined transport aircraft.

F.VIIb/3m
Main production version with greater span, 154 built including built under licence.

[edit] Licenced copies

[edit] Operators

[edit] Civilian operators

Flag of Belgium Belgium
  • SABENA operated 28 aircraft.
Flag of Denmark Denmark
Flag of France France
  • CIDNA operated seven F.VIIa aircraft.
  • STAR operated one F.VIIa aircraft.
Flag of Hungary Hungary
  • Malert operated two F.VIIa aircraft.
Flag of the Netherlands Netherlands
  • KLM received all five F.VII aircraft and 15 F.VIIas.
Flag of Poland Poland
  • Aero operated six F.VIIa aircraft for a short period in 1928. Since 1 January, 1929 all aircraft were handed over to PLL LOT airline.
  • Polskie Linie Lotnicze LOT operated six F.VIIas and 13 F.VIIb/3ms between 1929 and 1939.
Flag of Switzerland Switzerland
  • Swissair operated one F.VIIa and eight F.VIIb-3m aircraft.
Flag of the United States United States

[edit] Military operators

Flag of Czechoslovakia Czechoslovakia
Flag of Finland Finland
Flag of the Netherlands Netherlands
Flag of Poland Poland
  • Polish Air Force operated 21 F.VIIb/3m (20 of them were licence-built) aircraft as bombers and transports between 1929 and 1939.
    • 1 Pułk Lotniczy
      • 211 Eskadra Bombowa
      • 212 Eskadra Bombowa
      • 213 Eskadra Bombowa
Flag of Spain Spain
Flag of the United States United States
Flag of the Kingdom of Yugoslavia Kingdom of Yugoslavia

[edit] Specifications

[edit] Fokker F.VIIb/3m; Atlantic-Fokker C-2A

Data from [8]

General characteristics

  • Crew: 2
  • Capacity: 8 passengers
  • Length: 47 ft 11in (14.60m)
  • Wingspan: 71 ft 2in (21.70 m)
  • Height: 12 ft 8 in (3.90 m)
  • Empty weight: 6,725 lb (3,050 kg)
  • Loaded weight: 11,570 lb (5,200 kg)
  • Powerplant:Wright J-5 Whirlwind radial engines, 220 hp (164 kW) each

Performance


[edit] F.10

Data from [8]

General characteristics

  • Crew: 2
  • Capacity: 12 passengers
  • Length: 50 ft 7 in (15.41 m)
  • Wingspan: 79 ft 1 in (24.10 m)
  • Height: 12 ft 8 in (3.86 m)
  • Empty weight: 7,716 lb (3,500 kg)
  • Loaded weight: 13,007 lb (5,900 kg)
  • Powerplant:Pratt & Whitney Wasp radial engines, 420 hp (313 kW) each

Performance


[edit] References

[edit] See also

Related development

Comparable aircraft

Related lists