F 28crash

This aircraft was owned by Fokker as PH-SIX and leased to NLM Cityhopper. Shown here the aircraft still has the slats (movable wing edge).

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The first design of the F.28 called for 65 passengers but eventually was built to carry 70 passengers. A later extended version could carry 85 passengers. The model itself was not revolutionary, as there were already three aircraft types flying of the same T tail configuration: the French Caravelle from 1959, the American DC-9 from 1965 and the English BAC-111 from 1963. It was courageous of Fokker that they dared to compete with these three competitors who had the same passenger capacity.

A Mark 1000 with an extended fuselage of 57 inches (1.4 m) in front of the wing and 30 inches (0.76 m) behind the wing, capacity of maximum of 79 passengers, made its first test flight on April 28th, 1971 and obtained the Certificate of Airworthiness on August 30th, 1972.

F 28engine

The letters 'WEV' behind the PH stood for Wevers, the surname of Frans Wevers, projection leader of the F.28 (proto)program

This was the first of two produced aircraft in the Mark.6000 version with wing slats. Meanwhile, the 5T-CLF of Air Mauritania had the fixed leading edge section of the wing again. This aircraft has been in use at Linjeflyg, Stockholm / Sweden, , Libyan Arab Airlines / Libya and Iran Asseman Airlines / Iran, NLM Cityhopper before going to Air Mauritanië

The wing flaps of the PH_JHG are clearly visible and are a significant part of the takeoff and landing process. When the airplane is taking off, the flaps help to produce more lift.

The last built F.28 went to the Swedish Linjeflyg as SE-DGU. Linjeflyg. Linjeflyg was formed in 1957 as a Swedish domestic airline by Scandinavian Airlines System.

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The traded in Garuda F.28s were refurbished at Fokker Woensdrecht for the American company Piedmont. Shown here the N280N for Piedmont.

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Part Number, F-802020.TR4-H122BR. Cage, sheet steel cages. Bearing Mass - m, 314 kg | 692.244 lb. Series, F series (F-80..TR4).

At the moment (April 2020) there are still 40 fellowships in active service with a number of airlines, Air Forces and heads of state.

After a crash in 1975 of an Itavia F.28, the cockpit went to the Canadian CAE to be converted to a flight simulator for Fokker. The Itavia aircraft in question was the I-TIDA

The VH-ATG calibration aircraft for the Australian Department of Transport. It was used to calibrate the ILS (Instrument Landing System) among other things.

f-28 tomcat

The PH-JHG during take-off in a new color scheme as a test aircraft for the avionics of the soon to be build Fokker 100.

A version with an enlarged cargo door, as well as one with a modified wing, with slats and larger wingspan were in development at Fokker-VFW.

Fokker built the nose section, the Germans built the front and rear fuselage section and tail. While Shorts in Ireland took care of the wings.

F-29

Mk 2000/4000 with the extended wing and front wing slats. Received its Airworthiness on October 30th, 1975. Two were built, after which the project was abandoned. .

After its period as a prototype, the PH-MOL has been leased dozens of times to various operators, here for the British Air Anglia.

There are 243 Fellowships built in a number of versions for airlines, air forces and heads of state. There are a total of 10 different F28 types designed of which 7 were produced and three that did not go beyond the drawing board and were therefore never built.

F 28cockpit

The financing was facilitated by the Dutch government which accounted for 50% of the Dutch part and the German government which accounted for 65% of the German part. The rest came from Fokker's own capital and the partners.

The typical air brakes in the tail ensure a stable, slow approach flight. The aircraft is particularly economical on the shorter distances.

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The intention was to combine the short fuselage of the Mk 3000 with a larger wing with leading edge slats together with the more powerful Rolls-Royce RB183 Mk555-15H motor. Although it was expected to perform well on short runways due to its superior engine power, the project was abandoned.

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A maximum capacity of 70 passengers. Proof of Airworthiness obtained on February 24th, 1969. The cargo version 1000C had a large loading door on the main deck.

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enstrom f-28

Airlines and governments in Norway, The Netherlands, Sweden, Australia, Nigeria, Indonesia, Columbia, Argentina and in the United States already have F.28s in use, while many operators showed great interest in this type.

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In recognition of the work of chief designer J.H. Greidanus, the first prototype was named PH-JHG and made its first flight on May 9th, 1967. The crew consisted of the test pilots Andreas ("Jas") Moll (captain), Abe van der Schraaf and flight engineer Cees Dik. The flight took place from Schiphol and lasted 1 hour and 25 minutes.

f-28 sap

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In the early 60's Fokker realized that the time had come for a new aircraft. After the successful F 27 Friendship, Fokker had carried out extensive market research and invested a lot of time in the development of a new type of commuter aircraft. Eventually Fokker came up with the F.28, an aircraft that was slower than its competitors, but more maintenance-friendly and could use 85% of the airports served by the DC3 and F.27.

At Fokker it was the first passenger aircraft to be powered by two gas turbines (jet engines). It was a low-decker with the two Rolls Royce Spey engines mounted at the back of the fuselage. The horizontal stabilizer was mounted on top of the T tail.

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On April 28th, 1962, Fokker revealed the details of the F.28 Fellowship at the Hannover Air Show. A new aircraft, not as a successor to the F.27 but intended as an addition.  Both types therefore have had their own production line at Fokker, Schiphol for years. The F.28 was especially designed to operate from smaller regional airfields and fly short or medium distances. A special feature of this aircraft is the application of a "speedbrake" which was built into the tail. An application that was only common in military aviation and enabled the aircraft to descend effectively and quickly.

The F.28 Fellowship, which was developed by Fokker in the sixties, is one of the few jet aircraft that could be used at smaller, less equipped airports.

For the construction of the aircraft they worked together with Hamburger Flugzeugbau (formerly Blohm & Voss), Vereinigte Flugtechnische Werke (VFW) both from Germany and Short Brothers & Harland from Belfast (Northern Ireland).

The aircraft flew previously for various airlines. Air Ivoire Societe / République de Côte d'Ivoire, Delta Air Transport NV - DAT / Belgium, Trigana Air Service / Indonesia and finally, as shown, as S2-ACV for Biman from Bangladesh

F 28aircraft

A Mark 1000 with a 60 inch (1.5 m) extended wing. Certificate of Airworthiness on July 19th, 1978. The cargo version 3000C had a large cargo door on the main deck.

Obtained the certificate of Airworthiness on December 13th, 1976. Built as the model Mark 2000 with two over the wing exits on either side, the wings were extended by 60 inches (1,500 mm) with an increase capacity of 85 passengers.