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Aviation History
1997
1997 - 2156.PDF
COMMERCIAL AIRCRAFT Industrie Pesawat Terbang Nusantara, PO Box 3752 JKT. 14th Floor. Buml Daya Plaza Building, Jalan Imam Bonjol 61. Jakarta 10310, Indonesia: tel: +62 (21) 310 3833; fax: +62 (21) 310 0081. Model Dimensions Span (ml Length (ml Height (ml wing area Engines Landing Accomodation Max gear weights [kg] Track (m) Seats rVheelbase (m) Pitch Tum radius (ml Abreast Cabin width ILYUSHIN Takeoff Landing Zero fuel Operating empty 11-114 2 x l,840kW Isotov TV7-117 turboprop 30 8.4 64 22.700 26.86 9.2 75 22.700 9.18 12.3 4 21.500 81.9 2.26 15.000 Fuel litres) Standard Optional 8.360 FAR field lengths take-off landing ISA sea-level ISA+20c sea-level ISA 5,000ft ISA+20 c 5,000ft 1,550 ISA sea-level ISA+20C sea-level ISA 5,000ft ISA +20 c 5,000ft 1.300 Speeds (kt) (machl MM Vmo Vne 270 Mno Mmo Mne Cruise performance Max cruise Long range speed (kt) speed (kt) Max alt At ait Iftl (ft) Max cruise Long range fuel cons fuel cons (kg/h) (kg/h) 270 26.500 Payload details Max (kg) Range with max p/1 (km) Payloadwith max fuel (kg) range with max fuel 5.760 1.000 1,500 4,800 aircraft has a range of 1,000km. The 11-114 is powered by two l,860kW Klimov TV7-117C turboprops, driving Stupino ultra-wide-chord low-noise CB-34 carbonfibre-composite propellers, giving a 2 70kt cruise speed. Ilyushin has also signed an MoU with P&WC to install PW127 engines on a new model, known as the II-114PC, which would be supported by a P&WC/Klimov joint ven- ture.The cockpit has electronic displays and the wing is fitted with double-slotted flaps. A range of 3,250km with half payload and 5,800km with no payload is claimed. Production aircraft will have composite tailplanes and wingboxes - the maker's first use of such material in primary structure. Composites are used for the dorsal fin, ailerons, spoilers, wing-root fairings, radome and cabin floor. The II-114 has no underfloor stowage, so baggage is stowed either side of the aisle near the front entrance or in a single bay by the rear door. Production Final assembly is undertaken by the Tashkent Aircraft Production Organisation in Tashkent, Uzbekistan. The production rate is intended to be 100 aircraft a year. ni , ; • HllMlttHW^.IWIiir:.™ HAL, P0 Box 5150, Bangalore, 560 001, India; tel: +91 (812) 268003; fax: +91 (812) 2688758 or 577533. Indian manufacturer Hindustan Aeronautics builds the Fairchild Dornier 228 under licence and has been in wide-ranging talks with other manufacturers, notably in China and Indonesia, about the possibilities of producing other types. Ihyushin Design Bureau, Leningradsky Prospekt 45G, Moscow, 125190, Russia; tel: +7 (095) 943 8121; fax: +7 (095) 212 2132; telex: 411956 S0K0L IL-112 Ilyushin has Russian Government approval to proceed with development of this new high- winged, twin-turboprop, 40-seater. It is intend ed as an An-38 replacement. Production Planned to be at KUiYIAPP at Kumertau. IL-114 The II-114 twin turboprop has been delayed repeatedly, but the passenger version was cer tificated in April. It must continue trials with Uzbekistan Airways, however, while the cargo version is heading for clearance by December and will also first enter service with the national carrier. This version has a rear cargo-door and an MTOW of 23.5t. With a 6.5t payload, the N250 The first N250 prototype had its maiden flight in August 1995. Powered by two 2,400kW Allison AE2100C turboprops, it features a fly- by-wire flight-control system. The prototype was produced to the original 50-seat specification, while subsequent aircraft are stretched, 64- to 68-seat, N2 50-100s, and die second prototype, which is the first full-size -100, had its maiden flight in December 1996, eight months behind schedule. It will be followed by a further two test air craft. IPTN plans eventually to re-introduce the 50-seat version.The FAA has refused to accept the second as a certification-validation vehicle, because of shortfalls in conformity doc umentation. IPTN and its US subsidiary, American Regional Aircraft Industries (AMRAI), which will market the aircraft in the USA, are trying to get the N250-100 and the planned follow-on 70-seat N250-200/N270 derivative programmes back on schedule. In the meantime, AJVIRAI does not now plan to begin construction of its US site in Mobile, Alabama, until 1998. The plant is to be used for N270 final assembly and after-sales support. IPTN has enlisted a team of European aero space consultants to try to help secure JAA type certification of die N250. They have decided to pool their efforts in getting French DGAC type certification in line with JAA and FAA required standards. The JAA, unlike its US counterpart, does not require a bilateral treaty with Indonesia. For this reason, JAR Part 25 certifi cation is now expected ahead of FAR Part 2 5 approval some time towards the end of 1998. It is understood that flight-test certification will begin with the PA3, now due to be flown later this year. Two more certification aircraft, Span (m) Track (m) Seats Take-off Length (in) Wheelbase (m) Pitch Landing Height Tum Zero (m) radius (m) Abreast fuel wing area Cabin Operating (m ] width empty K250-100 2 x 3.330kW Allison GMA2100 turboprop 28 3.9 64 22.000 5,267 1.220 26.23 6.9 76 20.650 8.2 18.9 4 18.565 59.1 2.7 13.665 the PA4 and, finally, the SA1, are due to follow at four-monthly intervals. Production Final assembly is undertaken at IPTN's plant in Bandung. Two aircraft have been completed to date. Ordered 26 Delivered 0 N2130 Twin-engined regional jet family See Part 2 of directoiy next 'week (ovei~ 100 seats) 1.220 300 6.000 20.000 1.482 2.038 HiaUij^H Model Engines Dimensions Landing Accomodation Max Fuel FAR field lengths Speeds Cruise performance Payload fear weights (kg) (litres) take-off landing (kt) Imach) details Fue S| (litres takeof ) ISA ISA Standard sea-level sea-level Vno ISA+20C ISA+20c Optional sea-level sea-level Vmo ISA ISA 5,000ft 5,000ft Vne ISA+20'c ISA+20C 5,000ft 5,000ft I Imach Max cruise Long range Mno speed (kt) speed (kt) Max (kg) Max aft At aft Range with Mmo (ft) (ft) maxp/Hkm) Max cruise Long range fuel cons fuel cons Payload with Mne (kg/h) (kg/h) max fuel (kg) range with max fuel 64 FLIGHT INTERNATIONAL 27 August - 2 September 1997
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