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Aviation History
1995
1995 - 3579.PDF
AIRLINERS OF IWC MfOltLO U.^drHI^Mi. PO Box 12222, Amstefdam-Zuidoost, 1100 AE, Netherlands. Tel: +31 (20) 605 6666; Fax: +31 (20) 605 7022; Telex: 11526 FMHS NL F28 The F28 was introduced in 1969, with pro duction lasting until 1987, and has since been succeeded by its derivatives, the Fokker 100 and 70. Fokker has defined an inspection and modification programme which extends the life of the aircraft to 100,000 flight cycles. Each F28 approaching 90,000 cycles (a limit itself extended from the initial 60,000 cycles) will be treated individually. Operators apply directly to Fokker for a dedicated programme of inspections, structural modifications and retirement-life replacements. The fleet- leader F28 passed its modification pro gramme in 1993. Ordered: 232 Delivered:232 FOKKER 70/100 Indonesia's Sempati Air became the first air line to operate the Fokker 70 in March 1995, when it received the first two of the ten air craft which t will eventually operate. The first Fokker 70 was delivered to Ford Motor Corporation of the USA in October 1994. In October 1995, the Fokker 70 became only the second jet type approved for opera tion at London City Airport in the UK, start ing operations there in November 1995. This broke Avro International Aerospace's monop oly with the RJ Avroliner family. The Dutch manufacturer has indicated that it plans to gain a similar approval for the larger Fokker 100. This will require various modifi cations to the aircraft, including a reduction in the pre-charged pressure in the main-landing- gear struts. Software changes to reconfigure the avionics systems, to cope with the steeper, 5.5°, glideslope, will also be introduced. Earlier in 1995, Fokker announced that Rockwell-Collins' AVSAT-900 FMS/GPS would be fitted to the JetLine family as stan dard from 1997, replacing the existing Honeywell FMS. Also available is the Fokker 100QC (quick change). This would be manufactured as a standard aircraft and then modified by a sub contractor. The QC would carry a maximum payload of 11.5t, or up to 11 LD3 containers. The Fokker 100 was launched in November 1983, superseding the F28-4000 from which it is derived. The first flight was in November 1986 and the type entered ser vice with Swissair in March 1988. The Fokker 70's fuselage is 4.62 m shorter than that of the Fokker 100, achieved by removing fuselage plugs forward and aft of the wing. The Fokker 70 programme was launched in November 1992 and the first air craft flown in April 1993. Ordered: 357 Delivered: 295 Dimensions Landing fcto-odrtlon WM|Mi fie." IKR] Span (m) Track (m) Seats Ramp Length (m) Wheefcase (ml Pitch Take-off Height (m) Tum radius (m) Abreast Landing Wing area (nfl SweepC) HoMml Zero-fuel (•*) HoWs Ops empty Press M (bar) Fuel INtres) Standard Optional FAR field lengths takeoff landing ISAsi ISA si BA»20Csl ISA.20CsJ ISA ISA 5.000ft 5,000ft BA+arc ISA.2OC 5,000ft 5,000ft Speeds (kt) Imach) V2 VAT VN0 VMO MNO Mmo Cruise performance Max cruise long range speedlkt) speed (kt) a* (ft) a*(ft) Fuel cons Fuel cons (kg/Til (kg/h| Payload Max (kg) Range/* (km Fiitaafc (kg) Range with F (km) Fokker F28 Fetowship MMOO0 2 x 244kN Rolls-Royce RB.183 Mk555-15P turbofans 25.07 5.04 85 33.335 9,740 29.61 10.35 73cm 33.110 13,040 8.47 16.96 5 31.525 79.00 13.50 20.125 16.00 2 17.565 0.51 Takeoff ISA +20_C 5,000ft at MTOW of 31.750kg Fokker 70 (standard) 2 x 261.6kN Rollsfloyce Tay Mk620 turbofans 28.08 30.91 8.51 93.50 17.40 5.04 80 11.54 79/81cm 17.78 5 12.78 2 0.51 36.965 36.740 34.015 31.975 22.784 9.640 Fokker 70 (optional) 2 x 261.6kN Rollsfloyce Tay Mk620 turbofans 28.08 30.91 8.51 93.50 17.40 5.04 80 11.54 79/81cm 17.78 5 12.78 2 0.51 38,325 9.640 38.100 13.365 35,830 32,655 22,784 Fokker 70 (high optional) 2 x 261.6kN Rollsfloyce Tay Mk620 turbofans 28.08 5.04 80 40,140 13.365 30.91 11.54 79/81cm 39.915 _ 8.51 17.78 5 36,740 93.50 12.78 33,565 17.40 2 22,784 0.51 Optional wights: Ramp 41,955kg. MTOW 41.730kg Fokker F28 FefawNp Mk4000 2 x 244kN Rollsfloyce RB.183 Mk555-15P turbofans 25.07 5.04 85 29.61 10.35 73cm 8.47 16.96 5 79.00 13.50 16.00 2 0.51 Takeoff ISA +20_C 5.000ft at MTOW of 31.750kg Fokker 100 (standard) 2 x 261.6kN Rollsfloyce Tay Mk620 turbofans 28.08 5.04 109 43.320 13,365 35.53 14.01 81cm 8.50 20.07 93.50 16.72 17.40 2 0.51 Takeoff ISA +20_C 5,000ft at MTOW of 41.730kg Fokker 100 (optional) 2 x 267.2kN Rollsfloyce Tay Mk650 turbofans 28.08 5.04 109 44,680 13,365 35.53 14.01 81cm 44,450 8.50 20.07 5 39,915 93.50 16.72 36,740 17.40 2 24.727 0.51 Fokker 100 (high optional) 2 x 267.2kN Rollsfloyce Tay Mk650 turbofans 28.08 5.04 109 46.040 13,365 35.53 14.01 81cm 45.850 . 8.50 20.07 5 39,915 93.50 16.72 36,740 17.40 2 24.747 .0.51 33,335 9.740 33,110 13.040 31,525 20,125 17,565 43,090 _ 5 38,780 35,835 24.593 1,678 1.036 134 449 358 2,037 1.036 125.00 26,000 29.000 2.535 1,091 330 0.75 2,478 1.553 2,902 1.091 330 0.75 0.83 1.393 1,250 1.540 1,250 1.762 1.387 2.117 1,387 1.583 1.275 1.756 1,275 2.010 1,417 2.510 1,417 1.678 1.036 2.037 1,036 2.535 1,091 2.902 1,091 1.856 1,321 2.307 1,321 2,613 3.033 1,458 1.715 1.348 1.891 1,348 2.652 1,497 2.970 1,497 1.821 1,348 2.012 1.348 2.830 1,497 3,433 1,497 126 119.00 320 0.77 320 0.77 0.84 126 119.00 320 0.77 320 0.77 0.84 462 401 26,000 35,000 2,330 1,425 462 401 26,000 35,000 2,330 1,425 134 449 358 125.00 26,000 29.000 330 0.75 2.478 1,553 330 0.75 0.83 136 456 414 128.00 26,000 35,000 1.467 320 0.77 2.565 320 0.77 0.84 138 462 408 130.00 26.000 35,000 320 0.77 2.650 1,683 320 0.77 0.84 138 462 408 130.00 26,000 35,000 320 0.77 2.650 1.683 320 0.77 0.84 10.560 1.600 1.296 1.434 1,639 1,965 1.210 1.210 1,335 1,335 126 119.00 320 320 0.77 0.77 0.84 462 26,000 2,330 401 35.000 1.425 9,191 2,010 - 9.871 2,648 10.890 3,410 10.560 1,600 11,242 2.390 1,716 12,013 2,871 11,993 3,113 FLIGHT INTERNATIONAL 6 - 12 December 1995 73
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