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Aviation History
1996
1996 - 2718.PDF
ENGINE DIRECTORY l*l,WUii.Mlilldrf.WiHM.I?iii;ilb.ll PW4084 373.8 84,000 4.86 3.04 11 7 Boeing 777; PW4090 has 400.5kN thrust; PW4098 has 436.1kN thrust and will enter service in 1998 PW4152-4460 PW4168 PW6000 •I'linifiUVftin; Model F100-220 F100-229 F117-100 F119-100 231v4 -267 52,000 -60,000 3.37 302.5 68,000 4.14 67-107- 15,000-24,000- Max thrust dry kN lb 64.9 14,590 79.2 17,800 classified classified Max thrust (reheat) kN lb 105.7 23,770 129.4 29,100 157.5 35,000 PRATT & WHITNEY CANADA 2.46 2.71 - Length m 4.85 4.85 3.73 classified 9.94-10.47.348-0.370 Rotor/Fan SFC diameter (ml mg/Ns Ib/h/lb 1.18 1.81 2.15 classified 20.37 .72 22.64 .8 20.65 .73 classified classified I I fan 3 stage 3 stage 1 3 stage 4 11 5 11 6 Compressors LP HP 10 10 4 12 6 2 2 1 4' 5 Turbines LP HP 2 2 2 1 2 2 5 1 Airbus A300-600/600R, A310-200/300, MDC MD-11 Airbus A330 lApplicatiion Lockheed Martin F-16A/B, C/D, MDC F-15, F-15E. Offers a kit which upgrades earlier F100 engine models to equivalent of the F100-220. Lockheed Martin F-16C/D. MDC F-15E, MDC C-17 Military version of Pratt & Whitney's commercial PW2000 Lockheed Martin/Boeing F-22, basis of Joint Strike Fighter powerplants. Pratt & Whitney Canada, 1000 Marie-Victorin Boulevard,, Longueuil, Quebec J4G 1A1, Canada. Tel: +1 (514) 677 9411; Fax: +1 (514) 647 3620; Telex: 5267509 prattwhit mtl TWO NEW applications for Pratt & Whitney Canada's (P&WC) best-selling PT6 turbo- prop/turboshaft engine have been announced in 1996. The PT6B-37 turboshaft has been select ed by Agusta for its Al 19 Koala single-engined helicopter. Certification of the PT6B-37 is scheduled for late-1996, with production engine deliveries beginning during early 1997. The 745kW engine has an automatic fuel control with manual override, and a new, offset reduction gearboxrated at 670kW Initial and mature time-between-overhauls will be 3,000 and 3,500h, respectively, P&WC claims. The PT6C-65 turboshaft, a derivative of the PT6A- 65/67 turboprop, has been chosen by PZL- Swidnik to power the latest version of its W-3 Sokol twin-engined, multi-purpose helicopter. The PW150A turboprop, selected to power the Bombardier de Havilland Dash 8-400 Series 400, had its first test-cell run in June, and is on course for certification in June 1998. The latest version of the PW100 family, the PW150A is rated at 4,850-5,600kW, and has a new three-stage axial low-pressure compressor and a single-stage, centrifugal high-pressure compressor. Also included are a redesigned combustion system, additional turbine cooling and a high-power, low-speed reduction gearbox. Among other developments, the first PW206B turboshaft-powered Eurocopter EC135 was delivered in August. In June, Bell announced the selection of the PW206D as the powerplant for its new light twin-engined heli copter, the Model 427. The P WS 3 0 A turbofan, powering the Cessna Citation Bravo business jet, gained US Federal Aviation Administration certification in April, and the first production engines were delivered in June. The first flight of the PW545A-pow- ered Citation Excel took place in February, and engine certification is scheduled to take place in December. • Thrust Model kN lb JT15D4 JT15D-5 JT15D-5D 11.12 L2.9-14.19 13.54 PW305A/B 20.9-23.4 PW306A PW530A PW545A Model PT6A-114A PT6A-27 PT6A-42 PT6A-60A PT6A-67D PW118 PW119B PW120A 25.36 12.23 16.19 2,500 Length m 1.53 2,900-3,1901.53 3,045 1.53 4,678-5,2662.07 5,700 2,750 3,640 Power kW shp 502 506 633 782.2 908.9 1,342 1,624 1,491 675 680 850 1,050 1,220 1,800 2,180 2,000 1.92 1.52 1.72 Length (m) 1.57 1.57 1.7 1.77 1.93 2.06 2.06 2.06 Rotor/fan diameter (m] 0.52 Total SFC compressor ug/Ns Ib/h/lb Fan stages 15.92 .562 1 stage lcfgl* 0.52 15.61 -16.23.551 -0.5731 stage axl 1 cfgl* 0.69 0.78 0.8 0.58 0.69 Rotor/fan diameter (ml 0.48 0.48 0.48 0.48 0.48 0.63 0.63 0.63 15.84 10.99- 11.09 11.16 13.44 12.31 .56 1 stage axl lcfgl* 0.388- 1 4 axl +1 ofgl 0.391 .394 1 4axl + lcfgl .475 1 stage axl2 axl +1 cfgl .435 1 stage axil axl2 axl + Total SFC compressor ug/J Ih/h/shp stages 108.2 101.8 101.5 92.6 89.6 84.14 82.79 81.95 0.64 3 axl+ 1 cfgl 0.602 3 axl + 1 cfgl 0.601 3 axl + 1 cfgl 0.548 3 axl + 1 cfgl 0.53 4 axl + 1 cfgl 0.498 2 cfgl 0.49 2 cfgl 0.485 2 cfgl lcfg Turbines HP LP 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 Turbines HP LP 1 1 1 2 2 1 3 2 2 2 3 3 2 1 power turbine 2 2 2 Application 4B powers Cessna Citation II; -AC powers Agusta S.211; 4D powers Diamond IA * with axial booster stage -5 powers powers Cessna T47A, Diamond II, Beechjet 400A; -5A powers Citation V; -5B powers Beech T-1A Jayhawk; -5C powers Agusta S.211A * with axial booster stage Cessna Citation Ultra *with axial booster stage PW305A powers Learjet 60; PW305B powers Hawker 1000 Astra Galaxy; Cessna Citation Bravo Cessna Citation Excel Application Cessna Caravan 208B; -114 powers Caravan 1; -112 powers Cessna Conquest 1, Reims-Cessna F406 Caravan II Beechcraft 99 & 99A, DHC-6 Twin Otter 300, Harbin Y-12 II, • Let L-410, Pilatus PC-6; -21 powers Beech King Air C90 Beech Super King Air B200 Beech Super King Air 300; -62 powers Pilatus PC-9, PZL Orlik Beech 1900D; -66 powers Myasishchev M-102, Piaggio Avanti; -67A powers Beech Starship 2000; -67B powers Pilatus PC-12; -68 powers Embraer IEMB-312H, JPATS Beech Mkll Embraer EMB-120 Dornier 328 Dash 8-100 42 FLIGHT INTERNATIONAL 9 - 15 October 1996
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