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Aviation History
1997
1997 - 2155.PDF
COMMERCIAL AIRCRAFT Model Dimensions Span(m) Length (m) Height lm) wing area W notes Engines Landing Accomodation Max gear Track (m) Seats Wheelbase (m) Pitch Turn radius (m) Abreast Cabin width Fokker F28 Fellowship Mk4O0O weights Ikg Take-off Landing Zero fuel Operating empty Fuel (litres) Standard Optional 2 x 44kN Rolls-Royce RB183 Spey Mk555-15P turbofan 25.07 29.61 8.47 79 5.04 85 10.35 73 5 3.1 No longer in production Fokker 70 (standard) 33.110 31.525 20.125 2 x 62kN Rolls-Royce Tay 620 turbofan 28.08 30.91 8.51 93.5 5.04 80 11.54 79 17.78 5 3.1 Fokker 70 (high weight option) 36.740 34,015 31.975 22.784 2 x 62kN Rolls-Royce Tay 620 turbofan 28.08 30.91 8.51 93.5 5.04 80 11.54 79 5 3.1 No longer in production Fokker 100 (High weight option) 39.915 36.740 33.565 2 x 67kN Rolls-Royce Tay 650 turbofan 28.08 35.53 8.51 93.5 5.04 109 14.01 81 20.07 5 3.1 No longer in production 45.850 39,915 36.740 24,747 9,740 9.640 13.365 13,365 FAR field lengths take-off ISA sea-level ISA+20'c sea-level ISA 5,000ft ISA +20 c 5,000fl 1.678 2.037 2.535 2.902 1.296 1,434 1,639 1,965 1,583 1,756 2,010 2,510 1.821 2.012 2.830 3.4337 landing ISA sea-level ISA+20'c sea-level ISA 5,000ft ISA+20'c 5,000ft 1.036 1,036 1.091 1,091 1.210 1.210 1.335 1,335 1,275 1.275 1.417 1,417 1,348 1.348 1.497 1.497 Speeds (Ml Vno Vino Vne 330 330 390 320 320 380 320 320 380 320 320 380 (niachl Mno Mmo Mne 0.75 0.75 0.83 0.77 0.77 0.84 0.77 0.77 0.84 0.77 0.77 0.84 Cruise performance Max cruise speed (kt) Max alt (ft) Max cruise fuel cons (kg/h) 449 35.000 2.478 462 35.000 2.330 462 35.000 2.330 462 35.000 2.650 Long range speed (kt) At aft (ft) Long range fuel cons Ikg/h) 358 29.000 1,553 401 35.000 1,425 401 35.000 1.425 408 26,000 1,683 Payload details Max Ikg) Range with max p/1 (km) Payloail wrtli max fuel (kg) r.in;;e with max fuel 10,560 1.600 9.191 2.010 10.890 3,410 11.993 2.871 FOKKER 50/60 Developed from the F27 Mk500, the P&WC PW125B-powered, 46- to 58-seat Fokker 50 had its first flight in December 1985, and deliv eries began in August 1987. The aircraft fea tures improvements which include an all-new flightdeck with an EFIS, a twin-wheel nose- gear unit and all-composite, six-bladed, Dowry Rotol propellers. The turboprop formed the basis of Fokker's PropJetLine family of passenger, utility and special-mission aircraft. The most recent vari ant was the Fokker 50 High Performance, pro duced in both passenger and utility versions. This type, designed for improved hot-and- high operations, is powered by two P&WC PW127Bs, offering 10% more power than that of the standard Fokker 50's PW125Bs. A utility version of die Fokker 50, the Fokker 60, but with a 1.62m fuselage stretch, was launched in February 1994 for die Royal Netherlands Air Force, which placed orders for four for use as military transports. Delivered 212 Model Dimensions Span(m) Length (ml Height (m) wing area tofl Y-12-11 jii;Wii,w;i'iMiiiiiii;ii*i,'iiirJ Engines Landing Accomodation Max Fuel gear weights (kg) (litres) Track (m) Seats Take-off Standard Wheelbase (ml Pitch Landing Optional Turn Zero radius (m) Abreast fuel Cabin Operating width empty 2 x 460kW Pratt & Whitney Canada PT6A 27 turboprop 17.24 14.86 5.68 34.27 3.6 17 5.300 1.616 4.7 79 5.300 14.8 3 4.900 1.46 3.000 FAR field lengths take-off ISA sea-level ISA+20c sea-level ISA 5,000ft ISA +20 c 5,000ft 425 480 525 560 landing ISA sea-level ISA+20'c sea-level ISA 5,000ft ISA +20c 5,000ft 620 640 700 730 Speeds (kt) Vno Vmo Vne 140 162 (machl Mno Mmo Mne Cruise performance Max cruise speed (kt) Max alt (ft) Max cruise fuel cons (kg/hi 177 1,000 298 Long range speed (kt) At alt (ft) Long range fuel cons (kg/h) 144 1,000 213 Payload details Max Ikg) Range with max p/l (km) Payload with max fuel (kg) range with max fuel 1,700 757 1,100 1,540 F28 The 65-to 85-seat F28 twinjet was first flown in May 1967, and entered service in 1969. Production ceased in 1987 after 241 aircraft had been delivered. Four basic versions were pro duced (Mks 1000, 2000, 3000 and 4000), all powered by the R-R Spey Mk555. Fokker Aviation is studying an R-R Tay 620 re-engineing programme for the F28. The engine was been chosen over the BMW R-R BR710 and GE CF34-8C, and requires a small fuselage plug forward of the wing, to offset die extra weight. The programme is not yet launched, but, if a go-ahead is given soon, the first example could be available for delivery from early 1999. An ICAO Chapter 3-compliant hushkit for die F28 was proposed by a Fokker/TAT joint venture in 1992, but was shelved because of a lack of orders - die aircraft is exempt from US Stage 3 noise regulations as its MTOW falls below 34,050kg, a limitation which does not apply in Europe. Delivered 241 FOKKER 70/100 An advanced-technology, R-R Tay 620-pow- ered, development of the F28, the 107-seat Fokker 100 had its maiden flight in November 1986, and Swissair introduced the type into rev enue service in March 1988. The aircraft was progressively developed, with the more powerful Tay 650 being adopted, along widi higher weights, and additional fuel capacity. The 79-seat Fokker 70, which is 4.6m short er, was first flown in April 1993, and Indonesia's Sempati Air became the first airline to operate the aircraft, in March 1995. The two models were jointly marketed as the Fokker JetLine. The development of a stretched, 130-seat, derivative with a new wing and engines, dubbed the Fokker 130, had been proposed. This air craft was central to any take-over talks following the Dutch manufacturer's collapse. Delivered 226 (including46 Fokker 70s and 280 Fokker 100s) mm Harbin Aircraft Manufacturing, No 15 Youxie Street, PO Box 201, Harbin, Heilongjiang 150066, China; tel: +86 (451) 650 2122, or +86 (451) 650 2061; fax: +86 (451) 650 2061; telex: 87082 HAF CN. Y-12 The first Y-12 I was flown in 1982, after which the more-powerful Y-12 II, with 462 kW P&WC PT6A-27s, flew 1984 and won domes tic certification in 1985. Three models are available: the Y-12 I (Chinese utility interior), the Y-12 II (with a range of Western avionics options), and the updated Y-12-IV with winglets, strengthened undercarriage, and PT6A-2 7 engines. US certi fication of tlie latter was achieved in April 1995. FLIGHT INTERNATIONAL 27 August - 2 September 1997 63
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