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Aviation History
1997
1997 - 2231.PDF
COMMERCIAL AIRCRAFT M\vm\\\it>WMiimm Leningradsky Prospekt 45G, Moscow 125190,Russia; te): +7 (095) 943 8509 or +7 (095) 943 8121; fax: +7 (095) 212 2132; telex: 411956 SOKOL IL-62M/MK Three versions of the four-engined 170- to 195- seat 11-62 were built between 1963 and 1985, before it was superseded by the re-engined I1-62M. All versions were dimensionally identi cal, 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. Delivered 285 IL-76 The 11-76 was conceived to meet die Soviet air force's requirement for a heavy transport air craft. The first example of the four-engined high-winged freighter was flown in March 1971, and the type entered service in 1974. Different versions were produced for Aerofiot and the Soviet military, all powered by MKB (Soloviev) D-30KP engines. Many Il-76s are now flown on commercial freight charters. A 6.6m-stretched version, the II-76MF, pow ered by the Perm PS-90A turbofan, was flown for the first time in August 1995. The new model has a 1.5t increase in payload, while the new engines are claimed to offer a 12% reduc tion in fuel consumption, enabling range to be boosted by 20%. CFMI has been examining a possible re- engineing programme for the 11-76, with the CI \ 156-5. Production Final assembly of die 11-76 is under- ILYUSHIN Model Dimensions Span(m) Length (m) Height (m) wing area Inf) Engines Landing Accomodation Max Fuel gear weights (kg) (litres) Track (m) Seats Wheelbase(m) Pitch Turn radius (m) Abreast Cabin width Take-off Standard Landing Optional Zero fuel Operating empty FAR field lengths take-off landing ISA sea-level ISA+20c sea-level ISA 5,000ft ISA +20 c 5,000ft ISA sea-level ISA+20'c sea-level ISA 5,000ft ISA-f 20 c 5,000ft Speeds (Ml (mach) Vno Vmo Vne Mno Mmo Mne Cruise performance Max cruise Long range speed (kt) speed (kt) Max alt At aft (ft) (ft) Max cruise Long range fuel cons fuel cons (kg/h) (kg/hi Payload details Max (kg) Range with max p/l (km) Payload with max fuel (kg) range with max fuel notes II-62MK Classic 4 x 108kN Aviadvigatel D 30KU turbofan 43.2 6.8 174 170,000 105.300 3.300 2,500 53.1 24.5 86 105,000 12.35 29.5 6 94,600 3,700 2,670 280 - 71,600 II-76MF 4 x 157kN Aviadvigatel PS 90AN turbofan 50.5 - 140 190,000 109.480 54.29 - - 151,500 14.76 300 - 151,500 II-76T Candid A 4 x 118kN Aviadvigatel D 30KP turbofan 496 26,200 432 39.000 36.600 23,000 7,800 10,000 52,000 5.200 50.5 46.59 14.76 300 170,000 81,830 850 84.840 450 405 405 29,500 405 40,000 3,650 20,000 11-86 Camber 4 x 127kN Kuznetsov NK 86 turbofan 48.06 11.15 350 207,990 80.000 59.54 21.34 - 175.000 15.81 - 9 320 n-96-300 4 x 157kN Aviadvigatel PS 90A turbofan 57.6 10.4 300 216.195 150.387 55.35 - 87 175,000 17.6 - 9 157,000 350 117.00 II-96M&T 4 x 164.6kN Pratt & Whitney PW2337 turbofan 57.66 375 270,130 150,387 63.94 - - 175.158 15.72 • 190.430 350 - 132,423 M is passenger model, T is freighter. 26,000 23,000 2.760 1,980 42,040 3,600 40,000 7,170 15.000 0.86 460 39,000 58.000 10,750 30,000 taken by the Tashkent Aircraft Production Association (TAPO), in Tashkent, Uzbekistan. Delivered 850 plus IL-86 The four-engined Kuznetsov XK-86-powered 11-86 was the first Russian widebody, and the initial example was flown in December 1976. It entered service with Aerofiot in December 1980. Some 104 aircraft had been built and delivered when production ceased in 1994. The planned CFM56-5C2 re-engineing programme for Aerofiot Russian International Airlines' Il-86s has been delayed indefinitely, and according to CFMI, foundered on the inability to arrange funding. Delivered 104 IL-96-300 The 11-96-300 is a short-fuselage, long-range, advanced-technology development of the 11-86, equipped with new engines (Perm PS-90A), but has a new wing, EFIS flightdeck and a fly-by- wire FCS. The first prototype was flown in September 1988, and the aircraft was certificated in December 1992. Production Final assembly of the 11-96-300 is undertaken at the VASO Voronezh production plant in Russia. Delivered 9 IL-96M AND T The II-96M (T is the freighter designation) is a stretched development of the 11-96-300, with Western-built P&W PVV2337 engines, and Rockwell-Collins flightdeck avionics. The prototype II-96M, created by modifying the prototype 11-96-300, was flown in April 1992, while the first production-standard air craft (an I1-96T freighter) had its first flight in May 1997. Certification is scheduled to be gained by the end of 1997, to enable Aerofiot Russian International Airlines (ARIA) to take deliver)' of its first aircraft this year. The first production U-96M will be completed in mid- 1998, and is to be delivered by earlv 1999. ARIA holds orders for 20 Il-96Ms and fs. The ARIA deal has received US Exim Bank financing to cover the US content of the aircraft. In August 1997, Ilyushin signed an agree ment with Russian cargo carrier Volga-Dnepr covering the sale of four Il-96Ts, with two options, for delivery from 1999. Ilyushin is also negotiating a further order for 26 aircraft from another, unnamed, customer. Production See 11-96-300. Ordered 29 Delivered 0 IL-98 The 11-98 is a proposed twin-engined version of the I1-96M, which would be powered bv P&W P\\ 4000s, GE GE90s or R-R Trent 800s. FLIGHT INTERNATIONAL 3 - 9 September 1997 47
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