Fokker 100: Difference between revisions
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== External Links == | == External Links == | ||
* [https://www.easa.europa.eu/sites/default/files/dfu/EASA-TCDS-A.037_Fokker_F28-04-22082013.pdf EASA Type Certificate Data Sheet (TCDS)] | * [https://www.easa.europa.eu/sites/default/files/dfu/EASA-TCDS-A.037_Fokker_F28-04-22082013.pdf EASA Type Certificate Data Sheet (TCDS)] | ||
* [https://www. | * [https://web.archive.org/web/20120330044557/http://www.flyfokker.com/Fokker-100 FlyFokker (archived at web.archive.org)] | ||
{{Fokker}} | {{Fokker}} |
Latest revision as of 11:09, 24 July 2020
Type | Airliner |
---|---|
Configuration | Low wing aircraft, Retractable gear aircraft |
Propulsion | Twinjet (Jet aircraft, Twin-engine aircraft) |
Manufacturer | Fokker |
Author(s) |
|
FDM | JSBSim |
--aircraft= | fokker100 |
Status | Beta |
FDM | |
Systems | |
Cockpit | |
Model | |
Development | |
Website | |
Repository | |
Download | |
License | GPLv2+ |
Wikipedia | Fokker 100 |
|
The Fokker 100, officially called Fokker F28 Mark 0100 is a twin-engine passenger jet that was built by the Dutch aircraft company Fokker until it went defunct in 1996. It features a narrow body, T-tail configuration and digital avionics. Although it was originally used by almost every major airline, only 128 aircraft remain in operation today, mostly with Australian and some Asian airlines.
In FlightGear, the Fokker100 package, available since version 0.9.8, also includes the Fokker 70 and Fokker 130.
Specifications [1]
Overall Length [2] | 32.5 m (107 ft) | |
Wing Span [3] | 28.08 m (92 ft) | |
Height [4] | 8.50 m (28 ft) | |
MTOW | Between 40,995 kg (90,375 lbs) and 44,450 kg (98,000 lbs) | |
Engines | 2x Rolls-Royce Tay 620-15 with 61,610 N (13,850 lb) takeoff thrust | 2x Rolls-Royce Tay 650-15 with 67,170 N (15,100 lb) takeoff thrust |
Range [5] | 2,450 km (1,323 nm) | 3,170 km (1,710 nm) |
External Links
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- ↑ EASA Type Certificate Data Sheet (TCDS)
- ↑ aer.ita.br (archived on web.archive.org)
- ↑ aer.ita.br (archived on web.archive.org)
- ↑ aer.ita.br (archived on web.archive.org)
- ↑ Wikipedia