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Aviation History
1996
1996 - 3233.PDF
A1RUNERS OF THE WORLD Dimensions Span (m) Length (m) Height fm] Wing area (nfl Sweep!) Landing Accomodation Weights gear Track (m) Seats Wheelbase Iml Pitch Turn radius 1m) Abreast Hold vol (nfl Holds (kg) Ramp Takeoff Landing Zero-fuel Ops empty Press diff Ibarl Fuel (litres] Standard Optional FAR field lengths takeoff landing ISAsI ISAsI ISA+20Csl ISAtMCsl ISA ISA 5,000ft 5,000ft ISA+20C ISA+20C 5,00011 5,000ft Speeds Ml V2 VAT VN0 VMO VNE Imachl MNO Mmo MNE Cruise performance Max cruise long range speed Iktl speed [ktl Max alt (ft) at alt (ft) Fuel cons Fuel cons (kg/hi (kg/hi Payload Max (kg) Range/Mlkm) Full tank (kg) Range with F (km) II-62MK Classic 4 x 107.9kN Aviadvigatel O30KU turbofans 43.20 53.10 12.35 280 32.30 6.80 24.50 29.50 174 86cm 6 48 4 0.61 170,000 105,000 94,600 71,600 3,300 2,500 3,700 2,670 145 129 486 496 26,200 460 36,600 23,000 7,800 10,000 10,000 II-76MF 4 x 156.9kN Aviadvigatel PS-90AN turbofans 50.50 140 - 109,480 54.29 cm 190,000 14.76 151,50 300 25 1 K-76T Candid A 4 x 117.7kN Aviadvigatel D-30KP turbofans 50.50 46.59 - - 170,000 14.76 300 235.30 84,840 25 1 11-86 Camber 4 x 127kN Kuznetsov NK 86 turbofans 48.06 11.15 350 - 80,000 59.54 21.34 - 207,990 15.81 - 9 175,000 320 35 114 496" 432 39,000 52,000 5,200 1,830 850 450 130 405 405 29,500 405 40,000 3,650 20,000 3,700 26,000 23,000 140 486 1-96-300 4 x 156.9kN Aviadvigatel PS-90A turbofans 57.60 10.40 300 150,387 55.35 17.60 • - 350 30 H-96M&T 87cm 216,195 9 175,000 157,000 - 117,000 4 x 164.6kN Pratt & Whitney PW2337 turbofans 57.66 63.94 15.72 350 30 375 - 150,387 - 270,130 - 175,158 - 190,430 - 132,423 140 486 42,040 3,600 40,000 7,170 15,000 11,000 460 39,000 58,000 10,750 30,000 11,482 M is passenger modei, T is freighter. reduction in fuel consumption enabling range to be boosted by 20%. Ordered: 850+ Delivered: 850+ 11-86 The four-engined Kuznetsov NK-86-powered 11-86 was the first Russian widebody, and the first example was flown in December 197 6. It entered service with the then Aeroflot in December 1980. Some 104 aircraft had been built and delivered when production ceased in 1994. The planned CFM56-5C2 re-engineing programme for the 11-86 seems to have been delayed indefinitely. Ordered: 104 Delivered: 104 11-96-300 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 features a new wing, EFIS flightdeck and a fly- by-wire FCS. The first prototype was flown in September 1988, and the aircraftwas certificat ed in December 1992. Production—Final assembly of the 11-96-300 is undertaken at the Vorenezh factory in Russia. Ordered: 12 Delivered: 9 II-96M AND T The I1-96M (T is the freighter designation) is a stretched development of the 11-96-300, with Western-built P&W PW2337 engines, and Rockwell-Collins flightdeck avionics. The prototype I1-96M, created by modifying the prototype 11-96-3 00, was flown in April 1992, while the first production-standard aircraft (an I1-96T freighter) is to be flown in 1997. First flight of the production aircraft has been delayed. ARIA holds orders for 20 Il-96Ms and Ts, of which the first five aircraft will be the I1-96T cargo variant, and the other 15 will be the II- 96M passenger version. Amsterdam-based leas ing company Partnairs also holds five orders. The ARIA deal has received US Exim Bank financing to cover the US content of the aircraft. Production—See 11-96-300. Ordered: 25 Delivered: 0 and the Soviet military, all powered by the MKB (Soloviev) D-30KP engine. Many H-76s are now flown on commercial freight charters. A 6.6m stretched version, the I1-76MF, pow ered by the Perm PS-90A turbofan, was flown for the first time in August 1995. The new model features a 1.5t increase in payload, while the new engines are claimed to offer a 12% 11-98 The 11-98 is a proposed twin-engined version of the I1-96M, which would be powered by P&W PW4000s, GE GE90s or R-R Trent 800s. m PT Industri Pesawat Terbang Nusantara, PO Box 1562 Bd, lalan Pajajaran 154, Bandung 40174, Indonesia. Tel: +62 (22) 633900. Fax: +62 (22) 633912. N2130 Having flown its first indigenous regional air liner, the N250, in August 1995, Indonesian manufacturer IPTN announced plans to devel op a regional jet-powered airliner which will be offered in a family of models seating from 80 to 130 passengers, and with 3,700km range. The aircraft is expected to require an invest ment of some $2 billion, with income from the N250 put towards its development. IPTN has apparently already committed some $1.6 billion to the programme. Additional funds will be raised by a public share offering. IPTN intends to produce the first' aircraft by 2 002, and deliver the first customer aircraft by 2 004. Three variants are proposed, seating 80,100 and 130 passengers, and powered by two 81.9kN-class turbofans. FLIGHT INTERNATIONAL 4 -10 December 1996 61
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