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Double click to editTHE FOKKER 100

( F100 - TAY Mk 620-15 , F100 - TAY Mk 650-15 , F100 QC )

Type: 100 seat regional jet airliner.

Country of origin: Netherlands.

Power plants:
                     Two 61.6kN ROLLSROYCE TAY Mk 620-15 or 67.2kN Mk 650-15 turbofans.

Electrical power:
                              Supply frequency is 400 hz , three phase, and voltage is 115 - 200 V each generator
                              90 kva and supply 28 v dc power.
Performance:

              Max cruising speed 462 kt (M 0.79), long range cruising speed 453kt (M0.77)
              APP speed 130 kt (cat app C),stall speed 105 kt. total fuel capacity 10294 - 13365 Lit.
Range:
              with 107 passengers and TAY 620s (1323nm), or high gross weight version with Tay 650s (1680nm).

Weights: Medium (M)

                                   F100 Operating empty 24,727kg, max takeoff 44,450kg, Max landing 39915 kg.

Dimensions:
                     Wing span: 28.08 m          Length: 35.53 m          Height: 8.50 m       Wing area: 93.5 m²                            Outer main gear wheel span: 5.04 m                     Fuselage max diameter: 3.30 m

Aeroplane classification code number and letter: 3C

Service ceiling: 35000 ft.

Aeroplane classification by airport category: CAT 6

Take off field length at max Take off weight: 1825 m

Landing field length at max Landing weight: 1350 m

Distance between engine center lines: 536 cm

Wheel base: 14.01 m

Engine ground clearance: 234 cm

Wing aspect ratio: 8.43

History:
             First flight (PHMKH) occurred on November 30 1986, certification was awarded in November
            1987 and the first customer delivery, to Swissair, occurred in February 1988.

Capacity:        Flight crew of two. Max single class high density seating for 122. Standard single class
                         seating for 107 at five abreast. Fokker 100QC Quick Change max payload of 11,500kg .
Production:               Almost 300 Fokker 100s had been ordered before Fokker's collapse in March 1996. 283 had been built when production ceased in early 1997. in august 2006 a total of 229 F100 Aircraft remain in airliner service with some 47 airliners around the world. Fokker announced it was developing the Fokker 100 simultaneously with the Fokker 50 turboprop in November 1983. The Fokker 100 is based on the basic F-28 airframe , with the most important and obvious change being the stretched fuselage, increasing maximum seating to 122, compared with 85 in the F-28-4000. Other changes include more economical ROLLSROYCE TAY turbofans, revised wing design with greater span and aerodynamic efficiency ( Fokker claimed it to be 30% more efficient than the F-28's ), a modern EFIS glass flight deck , redesigned cabin interior plus other systems and numerous equipment changes.

irk: epasu, EPIDG.

ira: EPIDA, EPIDB, EPIDD, EPIDF, EPIDR , EPCFC,EPCFD, EPCFE, EPCFH, EPCFI, EPCFJ, EPCFK, EPCFL, EPCFM, EPCFN, EPCFO ,EPCFP, EPCFQ, EPCFR.

irc: EPASF, EPASG, EPASH, EPASI, EPASJ, EPASK, EPASL, EPASM, EPASO, EPASP, EPASQ, EPASR, EPAST, EPASX, EPASZ, EPATB.




Sources:

Aerodrome design manual.

Jane^’s all the world^’s aircraft 1974 - 2002.

www. airliners.net.

airport services manual part 1 (aircraft data for rescue and fire fighting personnel).

aircraft type designators ( doc 8643/25).