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Aviation History
1996
1996 - 3232.PDF
AIRLINERS OF THE WORLD resulting from hushkitting. The F2 8 was intro duced in 1969. Production ceased in 1987. Ordered: 241 Delivered: 241 FOKKER 70/100 The Fokker 70/100 assembly line should remain open until April 1997, despite the Dutch manufacturer's entry into administrative receivership in March, following cash purchas es of an additional nine Fokker 70s by KLM Cityhopper and Vietnam Airlines. Samsung has proposed a rescue plan for Fokker, although this still awaits approval by the South Korean Government. If Samsung is successful in taking over Fokker, it is understood that the South Korean company will push ahead with development of a 130-seat derivative of the Fokker 100, with a new wing and engines. The upgraded wing would later be used on the Fokker 70/100 as part of a mid-life update. The Fokker 100 had its maiden flight in November 1986, and Swissair introduced the type into revenue service in March 1988. In March 1995, Indonesia's Sempati Air became the first airline to operate the Fokker 70, which is 4.6m shorter than the Fokker 100. Production — Fokker assembly is undertaken at Schiphol, Amsterdam. A handful of Fokker 70s is in final assembly, although Samsung is proposing to build a further batch if the South Korean Government approves its take-over plan. These would be built for cash buyers which have already signed memoranda of understanding for additional aircraft. In the long term, Samsung envisages a production rate of up to 46 aircraft per year, rising from an ini tial rate of 20. Ordered: 362 Delivered: 315 Dimensions Landing Accomodation Weights gear (kg) Span (ml Track Im) Seals Ramp Length |ml Wheelbase (ml Pitch Take-off Height tm) Turn radius Im) Abreast Landing FAR field lengths take-off Fuel (litres) Standard ISA si ISAsI Optional ISA+20 C si ISA+20 C s ISA 5,000ft ISA 5,000ft Ml V2 VAT VNO Speeds Cruise performance Payioad Imach) Maxcniise longrange speed Ml speed Ml Max (kg) Maxatimi ataltlft) Range/M (km) Fuel cons Fuel cons Ikg/hl kg/n] Wing area Inr] Sweep C) HoMvol Zero-fuet (nf) Holds Opsempty Press drff (bar! ISA+20C ISA+20 C 5,000ft 5,000ft Fultank (kg) Range wittiF Fokker 70 Ihigh optional) 2 x 62kN Rolls-Royce Tay Mk620 turbofans 28.08 30.91 8.51 93.50 17.40 5.04 11.54 17.78 40,140 39,915 36,740 33,565 22,784 13,365 1,583 1,756 2,010 2,510 1,275 1,275 1,417 1,417 126 119 320 320 0.77 0.77 0.84 462 35,000 2,330 401 35,000 1,425 10,890 3,410 80 79/81cm 5 12.78 2 0.51 Range with a typical two class load of 79 passengers is 3469km. Optional weights: Ramp 41,955kg, MTOW 41,730kg, increases range with 79 pax to 3774km. Fokker 100 llstandard) 2 x 62kN Rollsfloyce Tay Mk620 turbofans 28.08 35.53 8.50 93.50 17.40 5.04 14.01 20.07 109 81cm 5 16.72 2 0.51 43,320 13,365 43.090 38,780 35,835 24,593 1,856 1,321 136 456 414 11,242 2,307 1,321 128 35,000 35,000 2,390 2,613 1,467 320 0.77 2,565 1,716 3,033 1.458 320 0.77 0.84 Takeoff ISA +20T 5,000ft at MTOW of 41,730kg. Range with a typical two class load of 107 passengers is 2,387km. Fokker 100 l2optkmall 2 x 67kN Rolls-Royce Tay Mk650 turbofans 28.08 35.53 8.50 93.50 17.40 5.04 14.01 20.07 109 81cm 5 16.72 2 0.51 44,680 44,450 39,915 36,740 24,727 13,365 1,715 1,891 2,652 2,970 1,348 1,348 1,497 1,497 138 130 320 320 0.77 0.77 0.84 462 35,000 2,650 408 35,000 1,683 12,013 2,871 Range with a typical two class load of 107 passengers is 2,867km. Fokker 100 (high optional) 2 x 67kN Rolls-Royce Tay Mk650 turbofans 28.08 35.53 8.50 93.50 17.40 5.04 14.01 20.07 109 81cm 5 16.72 2 0.51 46,040 45,850 39,915 36,740 24,747 13,365 1,821 2,012 2,830 3,433 1,348 1,348 1,497 1,497 138 130 320 320 0.77 0.77 0.84 462 26,000 2,650 408 35,000 1,683 11,993 3,113 Range with a typical twodass load of 107 passengers is 3,108km. ILYUSHIN llyushin Design Bureau, Leningradsky Prospekt 45G, Moscow 125190, Russia. Tel: +710951943 8509 or +7 1095) 943 8121 Fan +7 1095) 212 2132. Telex: 411956 S0K0L II-62M/MK Three versions of the four-engined 170-to 195- seat 11-62 were built between 1963 and 1985, before it was superseded by the re-engined II- 62M. All versions were dimensionallyidentical, with the main differences being in engine type, weight and performance. While the initial production version was equipped with the Kuznetsov Nk8 engines, the later I1-62M and MK were equipped with the SolovievD-30KU. Ordered: 285 Delivered: 285 11-76 The 11-76 was conceived to meet the Soviet air force's requirement for a heavy transport air craft. The first example of the four-engined high-winged freighter flew in March 1971, and the type entered service in 1974. Different versions were produced for Aeroflot The 11-9 6M prototype is still the only flying example of the PW2000-powered model 60 FLIGHT INTERNATIONAL 4 - 10 December 1996
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