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Aviation History
1997
1997 - 2159.PDF
•Mihim^iW'ii'ii^'Wi Model Engines Dimensions Landing Accomodation Max gear weights (kg] Span (m) Track (ml Seats Take-off Length |m] Wheelbase(m) Pitch Landing Height Tarn Zero (m) radius (m) Abreast fuel wing area Cabin Operating (rrr) width empty notes AntonovAn-2Antek 1 x 746kW PZL-Rzeszow Kalis* ASz€2IR piston 18.18 3.36 12 5.500 12.74 8.19 - 5,250 6.1 3 4,800 Ceased production in 1991 Antonov An-28 2 x 705kW PZLAzeszow TWD-lOB turboprop 22.06 3.41 17 6,500 13.1 4.35 72 6,500 4.9 - 3 5,884 39.72 1.87 Ceased production in 1991 Fuel (litres) Standard Optional 1,200 1,960 FAR held lengths take-off landing ISA sea-level ISA+20c ISA 5,000ft ISA+20'c 5,000ft 150 260 ISA sea-level BA+20c sea-level ISA 5,000ft ISA+20 c 5,000ft 170 315 Antonov An-28PT 2 x 820kW Pratt & Whitney Canada PT6A 65B turboprop 22.06 3.4 17 6.500 1,960 280 465 13.1 4.4 72 6,500 325 4.9 - 3 4,980 340 39.7 1.87 - 39 This aircraft was only ever a prototype and never entered series production. Speeds Ikt) (mach) VIM Vino Vne 115 145 190 210 185 210 Mno Mmo Mne Cruise performance Max cruise speed (kt) Max alt (ft) Max cruise fuel cons (kg/h) 139 5.740 170 189 9.850 210 9.840 520 Long range speed (kt) At alt IN Long range fuel cons (kg/h) 90 5.740 120 75 185 9,840 340 Payload details Max (kg) Range with maxp/1 (km) Paytoadwith max fuel (kg) range with max fuel 2,170 750 1.750 560 871 1,950 700 850 COMMERCIAL AIRCRAFT tSBMSSSM Esnzmmm Raytheon Aircraft, 10511 E Central, PO Box 85, Wichita, Kansas 67201-0085, USA; tel: +1 (316) 676 7111; fax: +1 (316) 676 8286. • VII^.].1.-^^——— Model Engines Dimensions Landing Accomodation Max Fuel FAR field lengths gear weights (kg) (litres) take-off landing ISA ISA Span (m) Track (m) Seats Take-off Standard sea-level sea-level Length ISA+20'c ISA+20c (m| Wheelbase(m) PHch Landing Optional sea-level sea-level Speeds Cruise performance Ikt) Imach) Payload details Max cruise Long range Vno Mno speed (kt) speed (kt) Max (kg) Max art At aft Range with Vmo Mmo (ft) (ft) max p/l (km) Height Tum |m) radius (m) Zero Abreast fuel wing area Cabin Operating (m2) width empty Beech King Air 350 2 x Pratt & Whitney Canada PT6A 60A turboprop 17.65 14.22 4.37 28.8 5.23 4.95 12.67 15 124 2 1.37 6.818 6,818 5.670 4.336 2.040 Beech King Air B200 2 x 635kW Pratt & Whitney Canada PT6A 42 turboprop 16.61 5.23 14 5,682 2,059 13.36 4.56 132 5.682 4.52 12.14 2 4,990 28.1 1.37 3,892 Beech 1900C Airliner 2 x 820kW Pratt & Whitney Canada PT6A 65B turboprop 16.61 5.23 19 7,530 2,525 17.65 7.26 4.54 11.99 28.15 Beech 19000 Airliner 2 x 954kW Pratt & Whitney Canada PT6A 67D turboprop 17.65 5.23 19 7.688 2.518 17.62 7.25 76 7.530 4.72 12.55 2 6.804 28.8 1.37 4.831 19 76 2 1.37 7,530 7.303 6.804 4,604 ISA ISA 5,000ft 5,000ft ISA+20 c ISA+20C 5,000ft 5,000ft 1.006 802 1.235 829 1,303 869 1.639 911 786 884 884 945 1.006 1.021 1,758 1.092 1.158 736 1,269 776 1.549 829 1.802 874 1,139 844 1.249 876 1.401 918 1.560 956 Vne 315 263 294 259 247 247 248 248 Mne 0.58 0.52 Max cruise fuel cons (kg/h) 315 24.000 350 294 22.000 - 318 268 14.000 283 16.000 460 Long range fuel cons (kg/h) 230 29.000 172 226 29.000 167 231 25.000 245 236 25,000 278 Payload with max fuel (kg range with max fuel 1.334 2.126 875 3.065 1,098 1,327 166 3,371 2.200 1,069 948 3.291 1.973 1.298 2.022 3.098 PZL-Mietec Aircraft, ul Wojska Pobkiego 3, Mielec, PL39300, Poland; tefc +48 (17) 788 7902; fax: +48 (17) 788 7226. AN-2 The Antonov An-2 single-piston-engined util ity biplane, with capacity for up to 12 passen gers, is still produced under licence at PZL. Some 12,000 examples have been built for use worldwide, but most have gone to the former Eastern bloc countries. AN-28 Antonov has considered resuming production of the An-28 (which has been the responsibility of Poland's PZL), re-engined with AlliedSignal TPE331s, although tiie manufacturer is look ing more to the larger An-38 in the short term. An-28 plans centre around a straight resump tion of manufacture, but with two 750kW TPE331-10/1 Is in place of the 720kW WSK- PZL Rzeszow TWD-lOBs used in the Polish WSK-PZL Mielec version. The first Polish An-28 was flown in July 1984 and the type received certification in February 1986. The aircraft has a rear-loading ramp, entered tJirough clamshell doors, fixed tricycle landing gear and is unpressurised. It also has short-take-off-and-landing performance, with automatically deployed leading-edge slats. BEECH KING AIR B200 AND 350 Although it is designed primarily as a business aircraft, the King Air's range and speed make it attractive for use as an airliner on low-density, long-distance, routes. Introduced in 1981, the B200 replaced the earlier 200 model. The B200 is powered by P&WC PT6A-42s, offering improved cruise and altitude performance, greater maximum zero-fuel weight and increased cabin-pressure differentials. All King Air models can be fitted witii optional cargo doors. Top of the range is the Beech King Air 3 50. Four extra windows are provided in the fuselage, which is 860mm longer, with wingspan 1.06m greater. In late 1995, the King Air 350 became the first Western turboprop to be certificated in Russia. US company Stevens Aviation has a supple mental type certificate to fit Lord's NVX acth e noise system to the King Air series. Commuter Air Technology of Scottsdalc, Arizona, has developed a streamlined exhaust- gas extractor for the King Air 200/B200 series, which it says eliminates "cracking problems'' associated with the original design. Production Final assembly is undertaken at the Raytheon plant in Wichita, Kansas. Delivered >2,000 (including military versions) BEECH 99 The Beech 99 is a 15-seat airliner development of the Beech Queen Air general-aviation air- FLIGHT INTERNATIONAL 27 August - 2 September 1997 67
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