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Fokker F28 Fellowship

  (Redirected from Fokker F28-4000)

The Fokker F28 Fellowship is a short range jet airliner designed and built by Dutch aircraft manufacturer Fokker.

F28 Fellowship
Piedmont F-28-1000.jpg
A Piedmont F28-1000 on approach
Role Regional jet
National origin Netherlands
Manufacturer Fokker
First flight 9 May 1967
Introduction 28 March 1969 with Braathens SAFE
Status In military service[1][2]
Primary user Garuda Indonesia (historical)
AirQuarius Aviation
Ansett Australia
Biman Bangladesh Airlines (historical)
Produced 1967–1987
Number built 241
Unit cost
Mk 1000: US$2.9M, Mk 2000: US$3M (1970)[3] US$19-19M today
Developed into Fairchild 228
Fokker 70
Fokker 100


Design and developmentEdit

five-abreast seating

Announced by Fokker in April 1962, production was a collaboration between a number of European companies, namely Fokker, MBB of West Germany, Fokker-VFW (also of Germany), and Short Brothers of Northern Ireland. There was also government money invested in the project, with the Dutch government providing 50% of Fokker's stake and the West German government having 60% of the 35% German stake.

Projected at first to transport 50 passengers to 1,650 km (1,025 mi), the plane was later designed to have 60–65 seats. On the design sheet, the F28 was originally to mount Bristol Siddeley BS.75 turbofans, but the prototype flew with the lighter Rolls-Royce "Spey Junior", a simplified version of the Rolls-Royce Spey.

The F28 was similar in design to the British Aircraft Corporation BAC One-Eleven and Douglas DC-9, as it had a T-tail and engines mounted at the rear of the fuselage. The aircraft had wings with a slight crescent angle of sweep with ailerons at the tip, simple flaps, and five-section liftdumper only operated after landing to dump the lift. These were employed rather than reverse thrust as the designers felt that doing so not only reduced weight, but maintenance also. Having no reversers also meant that on unpaved airstrips there was less chance of the engines ingesting debris. The leading edge was fixed (although one experimental model had leading edge slats and these were offered as an option) and was anti-iced by bleed air from the engines. The tail cone could split and be hydraulically opened to the sides to act as a variable air brake – also used on the contemporaneous Blackburn Buccaneer. This design was also used on the HS-146, which became the BAe-146. The design is unique in that it not only slows the aircraft down rapidly, it can aid in rapid descents from economic cruising altitudes and also allowed the engines to be set at higher RPM which helped eliminate 'lag time'. This means the engines respond faster if needed for sudden speed increases or go-arounds on the approach to landing. The Fellowship had a retractable tricycle landing gear which used large low pressure tyres enabling the use of unpaved airstrips. Large wheel brakes also helped in shortening the landing run.

In terms of responsibility for production, Fokker designed and built the nose section, centre fuselage and inner wing; MBB/Fokker-VFW constructed the forward fuselage, rear fuselage and tail assembly; and Shorts designed and built the outer wings.

Final assembly of the Fokker F28 was at Schiphol Airport in the Netherlands.[4]

Operational historyEdit

F28-2000 prototype (PH-JHG)
Third prototype leased to Air Anglia

The F28-1000 prototype, registered PH-JHG, first flew on 9 May 1967, flown by Chief Test Pilot Jas Moll, Test Pilot Abe van der Schraaf and Flight Engineer Cees Dik. German certification was achieved on 24 February 1969. The first order was from German airline LTU, but the first revenue-earning flight was by Braathens (who operated five F28s) on 28 March 1969.[4]

The F28 with an extended fuselage was named F28-2000 and could seat up to 79 passengers instead of the 65 seats on the F28-1000. The prototype for this model was a converted F28-1000 prototype, and first flew on 28 April 1971. The models F28-6000 and F28-5000 were modified F28-2000 and F28-1000 respectively, with slats, greater wingspan, and more powerful and quieter engines as the main features. The F28-6000 and F28-5000 were not a commercial success; only two F28-6000 and no F28-5000 were built. After being used by Fokker for a time, the F28-6000 were sold to Air Mauritanie, but not before they were converted to F28-2000s.[4]

The most successful[why?] F28 was the F28-4000, which debuted on 20 October 1976 with one of the world's largest Fokker operators, Linjeflyg. This version was powered by quieter Spey 555-15H engines, and had an increased seating capacity (up to 85 passengers), a larger wingspan with reinforced wings, a new cockpit and a new "wide-look" interior featuring enclosed overhead lockers and a less 'tubular' look. The F28-3000, the successor to the F28-1000, featured the same improvements as the F28-4000.[citation needed]

F28s of Ansett Transport Industries' Western Australian intrastate airline, MacRobertson Miller Airlines of Western Australia, flew the longest non-stop F28 route in the world, from Perth to Kununurra, in Western Australia – a distance of about 2,240 km (1,392 mi). This was also the world's longest twin-jet route at the time.[when?] MMA'a F28's also had the highest utilisation rates at the time, flying over 8 hours per day.[citation needed]

By the time production ended in 1987, 241 airframes had been built.[4]


The Mk 2000 has a 87 in (2.2 m) longer fuselage
The Mk 4000 has the Mk 2000 longer fuselage with double overwing exits and a 60 in (1.5 m) wider wing
The Mk 3000 has the Mk 4000 wider wing and the Mk 1000 shorter fuselage
F.28 Mk 1000
With a maximum capacity of 70 passengers, it was approved on 24 February 1969, the 1000C had a Main Deck Large Cargo Door.[5]
F.28 Mk 2000
Mark 1000 with a fuselage stretch of 57 in (1.4 m) in front of and 30 in (0.76 m) aft of the wing, 79 maximum passengers, approved on 30 August 1972.[5] Though it first flew on 28 April 1971 and successfully began revenue service with Nigeria Airways in October 1971, only ten were built.[4]
F.28 Mk 3000
Mark 1000 with a 60 in (1.5 m) wing span extension, approved on 19 July 1978, with a 3000C variant with a large main deck cargo door.[5] A successful variant, featuring greater structural strength and increased fuel capacity, it began revenue service with Garuda Indonesia.[4]
F.28 Mk 4000
Approved on 13 December 1976, it is built on the longer Mark 2000, with two overwing exits on both sides, a 60 in (1,500 mm) wing span extension, and capacity for 85 passengers.[5] The first prototype appeared on 20 October 1976 and it began service with Linjeflyg (Sweden) at the end of the year.[4]
F.28 Mk 5000
Was to combine the shorter fuselage of the Mk 3000 and an increased wingspan. Leading edge slats were to be added to the wings and more powerful Rolls-Royce RB183 Mk555-15H engines were to be used. Although expected to be an excellent plane to operate on short runways due to its superior power, the project was abandoned.[4]
F.28 Mk 6000
It first flew on 27 September 1973 and had the longer fuselage of the Mk 2000/4000 with an increased wingspan and leading edge slats. It was certified in the Netherlands on 30 October 1975. Two were built by 1976.[4][6]
F.28 Mk 6600
Proposed version. Not built.[4]
Fairchild 228
Proposed 50 seat American version to be assembled by Fairchild-Hiller with Rolls-Royce RB.203 Trent engines.[7] Project cancelled.


In August 2006 a total of 92 Fokker F28 aircraft remained in airline service. Major operators included: MacRobertson Miller Airlines, Ansett Group Australia (more than 15), Toumaï Air Tchad (1), AirQuarius Aviation (3), SkyLink Arabia (1), Satena (1), Gatari Air Service (2), LADE (1), AirQuarius Aviation (4) and Merpati Nusantara Airlines (1). Biman Bangladesh Airlines (8). Some 22 airlines operated smaller numbers of the type.[8] As of July 2018, Fly-SAX is the only airline operator of the F28 worldwide with 1 aircraft in service.[9]

Military operatorsEdit

Argentine Air Force F-28 T-03 of the Presidential Flight, Aeroparque Jorge Newbery, 2004
COAN (ARA) F-28 at Comandante Espora airbase
  • Philippine Air Force (1 – Used for domestic presidential Flights, The aircraft was named "Kalayaan")
  Togo (2)

Accidents and incidentsEdit

The following is a list of Fokker F28 accidents and incidents:

Aircraft on displayEdit


Variant -1000[18] -2000[18] -4000[19] -3000[19]
seating[a] 65 79 85 65
Hold 459 cu.ft / 13m³ 559 cu.ft / 15.9m³ 459 cu.ft / 13 m³
Length 89ft 10in /27.4m 97ft 2in / 29.6m 89ft 10.7in / 27.4m
Height 27ft 9.5in / 8.47m
Wingspan 77ft 4in / 23.6m 82ft 3in / 25.07m
Wing 822ft² / 76.4m², 16° sweep, 7.3:1 AR 850ft² / 79m², 16° sweep, 8:1 AR
Max takeoff weight 65,000lb / 29,480 kg 73,000lb / 33,110 kg
Empty weight 35,517lb / 16,144kg 36,953 / 16,707kg 38,825lb / 17,611 kg 37,139lb / 16,846kg
Max payload 18,983 / 8,629kg 17,547 / 7,976kg 23,317lb / 10,556kg 19,003lb / 8,620kg
Max Fuel 2,869 Imp Gal / 13,040 l
2× Turbofans Rolls-Royce Spey Mk 555-15 RB.183 Mk 555-15H
Unit thrust 9,850lbf / 43.9kN
Cruise 458kn / 848km/h Max, 359kn / 666 km/h LR 436kn / 808km/h Max, 354kn / 656 km/h LR
Fuel Consumption 6,180lb/h / 2,800kg/h Max, 3,260lb/h / 1,480kg/h LR 4,980lb/h / 2,260kg/h Max, 3,252lb/h / 1,475kg/h LR
Max PL Range 920nmi / 1,705km 900nmi / 1,668km 1,550nmi / 2,872 km
Takeoff (MTOW, ISA, SL) 5,500ft / 1,676m
Landing (MLW, SL) 3,540ft / 1,079m 3,495ft /1,065m 3,173ft / 967m
Service ceiling 35,000 ft (10,700 m)[5]
  1. ^ 5-abreast, 31in / 79cm pitch

See alsoEdit

Related development

Aircraft of comparable role, configuration and era

Related lists


  1. ^
  2. ^
  3. ^ "Fokker F.28 Series 2000". Flight International. 21 May 1970.
  4. ^ a b c d e f g h i j Antonio López Ortega (1999). Reactores Comerciales [Commercial Jetliners] (in Spanish). Agualarga Editores S.l. ISBN 978-84-95088-87-1.
  5. ^ a b c d e "Type Certificate Data Sheet No. A.037 for Fokker F28" (PDF). EASA. 3 September 2018.
  6. ^ Taylor 1976, p. 137
  7. ^ "What happened to the Fairchild 228?". AAHS Journal. Spring 1998.
  8. ^ Flight International, 3–9 October 2006
  9. ^ "World Airline Census 2018". Retrieved 2018-08-26.
  10. ^ "Trade Registers".
  11. ^ Air International May 1988, p. 233.
  12. ^ Ranter, Harro. "ASN Aircraft accident Fokker F-28 Fellowship 3000 PK-GFU Sorong-Jefman Airport (SOQ)".
  13. ^ "Fokker F 28 1000 Fellowship". Norwegian Aviation Museum. Archived from the original on 10 July 2018. Retrieved 9 July 2018.
  14. ^ "11 Unusual Preserved Airliners in the USA". Airport Spotting. 2017-07-03. Retrieved 9 July 2018.
  15. ^ a b "Fokker News". Stichting AIRnieuws Nederland. Retrieved 26 March 2019.
  16. ^ "Fokker F-28-4000, XY-AGH / 1114". ABPic. Retrieved 9 July 2018.
  17. ^ "REGISTRATION DETAILS FOR PK-MGJ". Planelogger. Retrieved 9 July 2018.
  18. ^ a b "Commercial aircraft survey". Flight International. 24 October 1974.
  19. ^ a b "Commuter airliner guide". Flight International. 21 March 1981.
  • "Andean Air Power...The Peruvian Air Force". Air International. Vol. 34 no. 5. May 1988. pp. 224–235, 240.
  • Taylor, John W. R., ed. (1976). Jane's All the World's Aircraft 1976–77. London: Jane's Yearbooks. ISBN 978-0-354-00538-8.

Further readingEdit