295:
274:
287:
222:, Pratt & Whitney Canada introduced the PW127XT (extended-time-on-wing) series. The PW127XT, which is intended to replace the PW127M variant, reduces the number of engine overhauls within 10 years to two from three. The engine maintenance interval (time-on-wing) is increased from 14,000 hours to 20,000 hours and would use three percent less fuel than the PW127M. The engine series will premiere as the standard powerplant on all new
1768:
1022:
40:
957:. Two PW150-based engines would be used to drive a single propeller. The powerplant was eliminated from contention by Airbus in early June 1999, since it was short of providing the 9,000 shp (6,700 kW) required to drive the eight-bladed propeller at the time, and its specific fuel consumption (SFC) was excessive.
2155:
215:, and the turbine modified to have improved cooling. The power rating was increased from 2,750 shaft horsepower (2,050 kilowatts) in the PW127 to 4,920 shp (3,670 kW) in the PW150, although the engine was thermodynamically capable of 6,500–7,500 shp (4,800–5,600 kW).
861:
Is capable of up to 7,000 shp (5,200 kW). Has a 3 stage axial low pressure compressor instead of the centrifugal NL unit on other variants. On the Q400, it sports a larger, six-bladed 13.5 ft (4.1 m) Dowty R408 propeller that spins at slower rates of 1,020
981:, and optimized low-pressure compressor. Has higher thrust, higher speed, and extended range compared to the PW150A. Blocked from an export license by the Canadian government in 2020, because of the Chinese government's retaliatory detention of Canadian citizens (the "
2122:
206:
selected the engine for the launch of its de
Havilland Dash 8-400 regional turboprop. The PW150 was a higher-power version of the PW100 series, with the low-pressure compressor changed from a single-stage
234:
using the PW127XT-M engine model. The PW127XT-N variant, which is designed for the ATR 72-600, has the same mechanical power rating as the PW127XT-M but has a higher thermodynamic power rating.
3110:
3030:
2977:
2838:
1999:
277:
Pratt & Whitney Canada PW123, from right to left: propeller mount, gearbox, air intake below, accessories surrounding the compressor, combustor, turbine and exhaust
967:
F-600. Abandoned in
December 2008 when the United States government barred a U.S.-based subcontractor from exporting the engine control software for the PW150B.
2628:
181:
The engine was first introduced as a technology demonstrator in 1977. The PW100 was first tested in March 1981, made its initial flight in
February 1982 on a
2588:
3164:
2970:
2567:
2955:
1977:
17:
242:
Originally called the PT7, the PW100 uses a relatively unusual three-shaft engine configuration. In the PW100, a centrifugal low-pressure (LP)
2963:
2528:
2428:
2608:
2845:
2694:
1957:
1881:
2790:
2262:
1835:
2870:
3140:
2814:
2763:
2948:
2729:
2297:
254:
centrifugal high-pressure (HP) impeller, driven by a single-stage HP turbine. Power is delivered to the offset propeller
2370:
2342:
2460:"European powerhouse: BMW Rolls-Royce is poised for new growth as it enters the commercial engine world with the BR715"
2985:
2220:
2922:
2244:
2052:
1903:
302:
The last two digits of each variant model number represent the nominal power at takeoff, in hundreds of horsepower.
3159:
2393:
3092:
3050:
3045:
3040:
3035:
3025:
1292:
2546:
3077:
294:
3072:
2318:
2033:
Hosking, E.; Kenny, D. P.; McCormick, R. I.; Moustapha, S. H.; Sampath, P.; Smailys, A. A. (11–15 May 1998).
2658:
2252:
1968:
2900:
2532:
2171:
1585:
1459:
1410:
1161:
1150:
1139:
108:
262:. The gearbox has two stages, yielding a reduction ratio between 15.4 and 17.16. The first stage uses
2986:
1831:
158:
80:
2043:
3126:
2912:
1808:
1357:
1192:
116:
1927:
3007:
2459:
259:
2365:
2337:
2038:
1725:
208:
170:
48:
2747:
2230:
1913:
1836:"Pratt & Whitney Canada celebrates the 30th anniversary of the PW100 turboprop powerhouse"
246:(except for the PW150, which uses a 3-stage axial LP compressor), driven by a single-stage LP
2755:
2199:
1796:
1746:
1257:
912:
2,500 shp (1,900 kW) turboshaft version that powered the first 2 prototypes of the
2657:
2627:
2458:
2427:
2282:
1998:
1926:
1880:
3102:
2699:
2465:
2434:
2404:
2176:
2005:
1933:
1887:
1791:
273:
8:
1854:
998:
346:
150:
2104:
2037:. Design principles and methods for aircraft gas turbine engines. pp. 4–1 to 4–9.
161:. Pratt & Whitney Canada dominates the turboprops market with 89% of the turboprop
2928:
2918:
2820:
2810:
2769:
2759:
2704:
2669:
2639:
2509:
2501:
2478:
2470:
2439:
2408:
2375:
2347:
2209:
2204:
2181:
2096:
2058:
2048:
2010:
1938:
1892:
978:
923:
255:
192:
162:
2802:
2664:
2088:
212:
185:
182:
2000:"ATR re-engines with new PW127XT series and secures launch order from Air Corsica"
286:
2990:
1773:
1468:
1464:
1213:
1182:
1129:
1118:
840:
251:
203:
146:
112:
2551:
1882:"Return of the power turboprop: Turboprop engine duel strikes up for 90-seater"
1786:
1516:
1051:
1040:
844:
219:
2794:
2773:
3153:
2932:
2824:
2708:
2673:
2643:
2513:
2505:
2482:
2474:
2443:
2412:
2379:
2351:
2213:
2185:
2100:
2062:
2014:
1942:
1896:
1689:
Single-stage low pressure and high pressure turbines, Two-stage power turbine
977:. Includes a third-stage power turbine, larger-diameter propellers, modified
2634:
2137:
2125:(Report). Vol. E-19 (51st ed.). Transport Canada. 28 August 2023.
982:
954:
2158:(Report). Vol. E-29 (3rd ed.). Transport Canada. 28 August 2000.
1742:
6.70, 8.49, and 14.44 kg/s (14.8, 18.7, and 31.8 lb/s)
263:
1172:
1001:, which was proposed for use in high-speed train travel in North America.
964:
231:
166:
2629:"Beyond C919 certification euphoria, COMAC confronts sobering realities"
2108:
3064:
1529:
974:
940:
2496:
Cook, Nick (9 June 1999). "Airbus to select A400M engine next month".
3060:
2593:
2572:
1675:
1537:
1223:
1202:
944:
936:
913:
267:
196:
154:
124:
120:
58:
2748:"Table 7-9. Typical T-O power and SFC of selected turboprop engines"
3017:
2999:
2806:
2092:
1252:
1233:
243:
2799:
Improving the efficiency of engines for large nonfighter aircraft
1684:
1108:
926:
247:
2914:
The
History of North American Small Gas Turbine Aircraft Engines
2752:
General aviation aircraft design: Applied methods and procedures
1021:
2589:"Pratt Canada seals deals to power Chinese, Russian turboprops"
2429:"CASA chosen for final assembly of Airbus Military transporter"
2338:"Douglas may offer three MD-90 versions with V2500 powerplants"
1698:
Kerosene Jet A, A-1/JP8; Wide Cut Jet B/JP4; High Flash JP5/JP1
1533:
1524:
1520:
1405:
1097:
1086:
1072:
1061:
794:
Developed for use on STOL (short takeoff and landing) aircraft
227:
223:
189:
104:
100:
70:
2035:
The PW100 engine: 20 years of gas turbine technology evolution
2032:
1978:"ATR Upgrades Turboprops with New Pratt & Whitney Engine"
298:
PW127G engine on a CASA C-295 aircraft at Paris Air Show 2013
1721:
3,415 kW (4,580 hp) + 3.412 kN (767 lbf)
2795:"Table 3-1. Comparison of candidate engine characteristics"
2609:"China's MA700 in jeopardy as Canada blocks PW150C exports"
2568:"Chinese LCC takes its first ARJ21, MA700 set for assembly"
2886:
ATR 42 72 Aircraft
Maintenance Training Manual, chapter 71
2695:"Xian signs Y-7 deals with five Chinese domestic airlines"
1830:
2789:
2319:"Deutsche Aircraft upgrades to P&W PW127XT-S engines"
863:
2785:
2783:
2260:
39:
202:
The PW150 engine was introduced on 24 April 1995, when
1076:
2780:
916:
helicopter and was to be used on the Mi-38-1 variant.
888:
2,400 shp (1,800 kW), no longer in service.
882:
1,815 shp (1,353 kW), no longer in service.
2083:. General Aviation Aircraft Meeting and Exposition.
1763:
2529:"China, Russia still at odds over Il-76 sales deal"
2911:Leyes II, Richard A.; Fleming, William A. (1999).
2741:
2739:
2469:. No. 4679. Berlin, Germany. pp. 38–40.
2310:
2087:. Vol. 94, no. 4. pp. 4.740–4.746.
188:, and then entered service in December 1984 on a
3151:
1958:"ATR upgrades turboprops with new Pratt engines"
258:through a third shaft, connected to a two-stage
2910:
2736:
2261:Thierry Dubois; Mark Huber (February 1, 2014).
2226:
2028:
2026:
2024:
1909:
1879:Trimble, Stephen (28 February – 5 March 2012).
2386:
2290:Take-off: Russia's National Aerospace Magazine
2275:
2243:Dubois, Thierry; Huber, Mark (February 2014).
1826:
1824:
1667:Two-spool, two-stage centrifugal compressors,
2971:
2148:
1751:3.44–3.83 kW/kg (2.09–2.33 hp/lb);
2993:and United Aircraft of Canada (UAC) aircraft
2801:. The National Academies Press. p. 29.
2724:
2722:
2720:
2718:
2192:
2074:
2072:
2021:
1855:"Pratt & Whitney Canada – The Dominator"
1671:Two-spool, 3-stage axial, single centrifugal
3165:Pratt & Whitney Canada aircraft engines
2917:. Washington, DC: Smithsonian Institution.
2745:
2601:
2580:
2559:
2539:
2520:
2489:
2242:
2138:"Civil Turboshaft/Turboprop Specifications"
1975:
1821:
1717:1,342–1,846 kW (1,800–2,476 hp);
1025:A PW120A fitted to a Canadian Forces CT-142
266:, followed by a second stage with straight
2978:
2964:
2650:
2619:
2450:
2419:
2358:
2329:
2163:
2130:
2127:Canadian type certificate for PW118–PW127.
2081:Development of the PW100 turboprop engines
1949:
1615:
490:Can be converted to a PW123B, C, D, or E.
2901:"Pratt & Whitney Canada PW100 Series"
2863:
2831:
2715:
2316:
2236:
2069:
2042:
1990:
1919:
1872:
1852:
1650:390.5–481.7 kg (861–1,062 lb);
1630:2,046–2,130 mm (80.6–83.9 in);
2906:. Forecast International. November 2010.
2565:
2500:. Vol. 31, no. 23. p. 1.
2403:. Vol. 37, no. 287. AEROPERS.
1020:
293:
285:
272:
2335:
2169:
2115:
1878:
629:Can be converted to a PW127C, E, or F.
615:Can be converted to a PW123 or PW127D.
601:Can be converted to a PW123 or PW126A.
14:
3152:
2659:"Pratt-built engine to power JetTrain"
2566:Meszaros, Jennifer (20 January 2020).
2456:
574:Can be converted to a PW123 or PW127.
2959:
2586:
2526:
2425:
1996:
1955:
1640:635–679 mm (25.0–26.7 in);
1245:
149:family is a series of 1,800 to 5,000
3141:Pratt & Whitney aircraft engines
2625:
2495:
2371:Aviation Week & Space Technology
2343:Aviation Week & Space Technology
2170:Warwick, Graham (9 September 1998).
2160:Canadian type certificate for PW150.
2078:
2880:
2871:"PW150 Type certificate data sheet"
2844:. EASA. 4 June 2014. Archived from
2839:"PW100 Type certificate data sheet"
2547:"PWC pulls out of military Y8-F600"
2317:Schuurman, Richard (17 June 2022).
2079:Cook, David L. (16–19 April 1985).
1997:Perry, Dominic (15 November 2021).
943:aircraft. Proposed for the unbuilt
290:A PW127E installed on an ATR 72-500
230:aircraft, with a launch order from
24:
2336:Shifrin, Carole A. (3 July 1989).
1853:Schonland, Addison (25 Apr 2017).
1007:Marine application for the PW150A.
546:Can be converted to a PW123 or C.
532:Can be converted to a PW123 or D.
25:
3176:
2940:
2687:
2527:Chang, Andrei (3 December 2008).
1976:Cathy Buyck (November 15, 2021).
1956:Buyck, Cathy (16 November 2021).
1755:4.76 kW/kg (2.90 hp/lb)
1263:
997:PW150 derivative adapted for the
991:Marine application for the PW100.
873:
866:at takeoff and 850 rpm at cruise.
18:Pratt & Whitney Canada PW150B
2438:. Toulouse, France. p. 22.
2407:. July–August 1990. p. 38.
1891:. No. 728. pp. 32–33.
1766:
165:installed base in 2016, leading
144:Pratt & Whitney Canada PW100
38:
2893:
2626:Chua, Alfred (3 October 2022).
2587:Polek, Gregory (20 June 2017).
2426:Moxon, Julian (17 March 1999).
1596:
1011:
935:Unsuccessfully offered for the
855:
823:2,621 eshp (1,954 kW)
807:2,621 eshp (1,954 kW)
791:2,619 eshp (1,953 kW)
776:2,619 eshp (1,953 kW)
762:2,619 eshp (1,953 kW)
749:2,880 eshp (2,148 kW)
736:2,880 eshp (2,148 kW)
722:3,058 eshp (2,281 kW)
708:2,619 eshp (1,953 kW)
694:2,516 eshp (1,876 kW)
680:2,880 eshp (2,148 kW)
667:2,880 eshp (2,148 kW)
654:2,619 eshp (1,953 kW)
640:2,620 eshp (1,954 kW)
626:2,619 eshp (1,953 kW)
612:2,493 eshp (1,859 kW)
598:2,323 eshp (1,732 kW)
585:2,261 eshp (1,687 kW)
571:2,522 eshp (1,881 kW)
557:2,261 eshp (1,687 kW)
543:2,054 eshp (1,532 kW)
529:2,054 eshp (1,532 kW)
515:2,262 eshp (1,687 kW)
501:2,261 eshp (1,686 kW)
487:2,261 eshp (1,687 kW)
474:1,992 eshp (1,465 kW)
460:2,044 eshp (1,524 kW)
446:1,892 eshp (1,411 kW)
432:1,787 eshp (1,333 kW)
418:1,941 eshp (1,448 kW)
404:1,941 eshp (1,448 kW)
390:1,948 eshp (1,453 kW)
377:1,892 eshp (1,412 kW)
363:1,893 eshp (1,412 kW)
2394:"Launch target for new Fokker"
2298:"Fourth Mi-38 commences tests"
2283:"Fourth Mi-38 commences tests"
2208:. September 1991. p. 26.
1846:
1708:
711:Can be converted to a PW127M.
697:Can be converted to a PW127M.
683:Can be converted to a PW127B.
643:Can be converted to a PW127B.
421:Can be converted to a PW119B.
407:Can be converted to a PW119C.
393:Can be converted to a PW119B.
366:Can be converted to a PW118B.
352:Can be converted to a PW118A.
331:1,500 shp (1,100 kW)
176:
13:
1:
2732:. Pratt & Whitney Canada.
2172:"Turboprop - and proud of it"
1814:
1658:
1654:716.9 kg (1,580 lb)
560:Can be converted to a PW123.
518:Can be converted to a PW123.
463:Can be converted to a PW120.
449:Can be converted to a PW121.
435:Can be converted to a PW121.
2746:Gudmundsson, Snorri (2022).
2374:. 30 July 1990. p. 11.
2292:. November 2014. p. 30.
973:Proposed powerplant for the
963:Proposed powerplant for the
953:Proposed powerplant for the
7:
2457:Norris, Guy (2 June 1999).
2399:. From other publications.
2366:"Allison GMA 2100 selected"
2267:Aviation International News
2253:Aviation International News
2227:Leyes II & Fleming 1999
2156:Type certificate data sheet
2123:Type certificate data sheet
1982:Aviation International News
1969:Aviation International News
1910:Leyes II & Fleming 1999
1759:
1016:
504:Can be converted to PW123.
281:
10:
3181:
2987:Pratt & Whitney Canada
2533:United Press International
2340:. Report from Le Bourget.
1832:Pratt & Whitney Canada
1634:2,420 mm (95 in)
1162:De Havilland Canada Dash 8
1151:De Havilland Canada Dash 8
1140:De Havilland Canada Dash 8
836:5,492 eshp (4,095 kW)
159:Pratt & Whitney Canada
109:De Havilland Canada Dash 8
81:Pratt & Whitney Canada
3135:
3119:
3101:
3059:
3016:
2998:
2876:. EASA. 19 November 2014.
2791:National Research Council
2200:"Dornier lands big order"
810:Used in the ATR 72-600s.
765:Used in the ATR 72-600s.
237:
153:(1,300 to 3,700 kW)
46:
37:
32:
1809:List of aircraft engines
1740:PW120, PW127, and PW150:
1731:PW120, PW127, and PW150:
1644:790 mm (31 in)
1193:Embraer EMB 120 Brasilia
117:Embraer EMB 120 Brasilia
3160:1980s turboprop engines
1733:12.14, 15.77, and 17.97
1616:General characteristics
136:>8,000 (as of 2014)
2730:"PW100/150 Turboprops"
1928:"PW150 for Dash 8-400"
1726:Overall pressure ratio
1680:Reverse flow combustor
1026:
922:Selected to power the
334:No longer in service.
299:
291:
278:
209:centrifugal compressor
171:Allison Engine Company
49:Canada Aviation Museum
27:Aircraft engine family
3103:Auxiliary power units
2756:Butterworth-Heinemann
2498:Jane's Defence Weekly
2368:. Industry observer.
2263:"New Rotorcraft 2014"
2245:"New rotorcraft 2014"
1797:General Electric GE38
1747:Power-to-weight ratio
1715:Maximum power output:
1704:Self-contained system
1624:Three-shaft turboprop
1602:At sea-level take-off
1258:Skjold-class corvette
1024:
906:No longer in service.
900:No longer in service.
894:No longer in service.
297:
289:
276:
2700:Flight International
2615:. 28 September 2021.
2466:Flight International
2435:Flight International
2405:Flight International
2177:Flight International
2006:Flight International
1934:Flight International
1888:Flight International
1792:General Electric CT7
1560:0.433 lb/(hp⋅h)
1491:0.459 lb/(hp⋅h)
1434:0.470 lb/(hp⋅h)
1380:0.485 lb/(hp⋅h)
1332:0.498 lb/(hp⋅h)
985:") starting in 2018.
264:double helical gears
260:free (power) turbine
2668:. 16 October 2002.
2555:. 22 December 2008.
2288:. Industry – News.
1270:
999:Bombardier JetTrain
725:Used in CASA C295.
307:
306:Certified variants
2851:on 31 January 2017
2346:. pp. 56–57.
2142:www.jet-engine.net
1965:Dubai Airshow News
1781:Comparable engines
1268:
1246:Other applications
1027:
305:
300:
292:
279:
96:Major applications
3147:
3146:
2816:978-0-309-10399-2
2765:978-0-12-818465-3
2256:. pp. 48–51.
1859:Air Insight Group
1592:
1591:
1269:PW100/150 Series
1243:
1242:
1081:PW127E/XT-M/XT-L
979:reduction gearbox
924:Deutsche Aircraft
851:
850:
256:reduction gearbox
250:, supercharges a
211:to a three-stage
193:regional aircraft
163:regional airliner
140:
139:
16:(Redirected from
3172:
2991:aircraft engines
2980:
2973:
2966:
2957:
2956:
2952:
2951:
2949:Official website
2936:
2907:
2905:
2887:
2884:
2878:
2877:
2875:
2867:
2861:
2860:
2858:
2856:
2850:
2843:
2835:
2829:
2828:
2787:
2778:
2777:
2754:(2nd ed.).
2743:
2734:
2733:
2726:
2713:
2712:
2703:. 16 June 1998.
2691:
2685:
2684:
2682:
2680:
2665:Hartford Courant
2661:
2654:
2648:
2647:
2631:
2623:
2617:
2616:
2605:
2599:
2598:
2584:
2578:
2577:
2563:
2557:
2556:
2543:
2537:
2536:
2524:
2518:
2517:
2493:
2487:
2486:
2462:
2454:
2448:
2447:
2431:
2423:
2417:
2416:
2398:
2390:
2384:
2383:
2362:
2356:
2355:
2333:
2327:
2326:
2314:
2308:
2305:
2293:
2287:
2279:
2273:
2270:
2257:
2249:
2240:
2234:
2224:
2218:
2217:
2196:
2190:
2189:
2167:
2161:
2159:
2152:
2146:
2145:
2134:
2128:
2126:
2119:
2113:
2112:
2085:SAE Transactions
2076:
2067:
2066:
2046:
2030:
2019:
2018:
2002:
1994:
1988:
1985:
1972:
1962:
1953:
1947:
1946:
1930:
1923:
1917:
1907:
1901:
1900:
1884:
1876:
1870:
1869:
1867:
1865:
1850:
1844:
1843:
1842:(Press release).
1828:
1776:
1771:
1770:
1769:
1603:
1600:
1465:Canadair CL-215T
1271:
1267:
1197:PW118/118A/118B
1078:
1029:
1028:
867:
859:
817:
801:
785:
308:
304:
213:axial compressor
186:testbed aircraft
183:Vickers Viscount
157:manufactured by
151:shaft horsepower
133:
97:
67:
42:
30:
29:
21:
3180:
3179:
3175:
3174:
3173:
3171:
3170:
3169:
3150:
3149:
3148:
3143:
3131:
3127:CH-124 Sea King
3115:
3097:
3055:
3012:
2994:
2984:
2947:
2946:
2943:
2925:
2903:
2899:
2896:
2891:
2890:
2885:
2881:
2873:
2869:
2868:
2864:
2854:
2852:
2848:
2841:
2837:
2836:
2832:
2817:
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349:(1,411 kW)
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2552:Air Cargo News
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2003:. Dubai 2021.
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1840:Skies Magazine
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1787:Allison AE2100
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1558:
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1523:-400/500/600,
1514:
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1382:295 g/kWh
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1334:303 g/kWh
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1803:Related lists
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1565:1,583 lb
1564:
1559:
1556:
1554:3,700 kW
1552:5,000 hp
1551:
1549:4,600 kW
1547:6,200 hp
1546:
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1542:
1539:
1535:
1531:
1526:
1522:
1518:
1515:
1510:
1505:
1500:
1496:1,060 lb
1495:
1490:
1487:
1485:2,050 kW
1483:2,750 hp
1482:
1480:2,400 kW
1478:3,200 hp
1477:
1474:
1473:
1470:
1466:
1461:
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1453:
1448:
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1438:
1433:
1430:
1428:1,800 kW
1426:2,400 hp
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1423:2,200 kW
1421:3,000 hp
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1417:
1416:
1412:
1407:
1404:
1399:
1394:
1389:
1384:
1379:
1376:
1374:1,600 kW
1372:2,100 hp
1371:
1369:1,800 kW
1367:2,400 hp
1366:
1363:
1362:
1359:
1356:
1351:
1346:
1341:
1336:
1331:
1328:
1326:1,300 kW
1324:1,800 hp
1323:
1321:1,630 kW
1319:2,180 hp
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77:Manufacturer
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31:
19:
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2913:
2894:Bibliography
2882:
2865:
2853:. Retrieved
2846:the original
2833:
2798:
2751:
2698:
2689:
2677:. Retrieved
2663:
2652:
2635:FlightGlobal
2633:
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2612:
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2571:
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2080:
2034:
2004:
1992:
1981:
1971:. p. 6.
1964:
1951:
1932:
1921:
1905:
1886:
1874:
1862:. Retrieved
1858:
1848:
1839:
1802:
1801:
1780:
1779:
1752:
1745:
1739:
1736:
1730:
1724:
1718:
1714:
1701:
1695:
1692:
1683:
1674:
1668:
1664:
1651:
1647:
1641:
1637:
1631:
1627:
1621:
1612:PW100, PW150
1609:
1608:
1598:
1582:240 cm
1527:-210/500/600
1513:210 cm
1456:210 cm
1402:210 cm
1354:210 cm
1311:Application
1208:PW125B/127B
1145:PW120/PW121
1103:PW127F/XT-M
1075:-500/600/600
1067:PW120/PW121
1064:-300/320/400
1012:Applications
983:two Michaels
955:Airbus A400M
857:
301:
241:
218:At the 2021
217:
201:
180:
143:
141:
132:Number built
3065:Turboshafts
2855:14 February
2613:ch-aviation
2302:Fantasy Lab
1709:Performance
1702:Oil system:
1665:Compressor:
1648:Dry weight:
1572:110 cm
1567:718 kg
1498:480 kg
1441:450 kg
1439:992 lb
1387:418 kg
1385:921 lb
1339:391 kg
1337:861 lb
1251:Bombardier
1173:Dornier 328
1032:Application
965:Shaanxi Y-8
345:1,892
342:1986-03-11
232:Air Corsica
190:Dash 8
177:Development
167:GE Aviation
90:March 1981
3154:Categories
3061:Turboprops
2774:1272887697
2679:20 October
2229:, p.
1912:, p.
1815:References
1693:Fuel type:
1676:Combustors
1659:Components
1580:95 in
1577:76 cm
1575:30 in
1570:44 in
1530:CASA C-295
1511:84 in
1508:66 cm
1506:26 in
1503:84 cm
1501:33 in
1454:84 in
1451:66 cm
1449:26 in
1446:84 cm
1444:33 in
1418:PW123/124
1400:84 in
1397:64 cm
1395:25 in
1392:79 cm
1390:31 in
1352:81 in
1349:64 cm
1347:25 in
1344:79 cm
1342:31 in
975:Xian MA700
941:IPTN N-250
833:1998-06-24
820:2023-06-22
804:2022-08-25
788:2023-08-28
773:2014-05-05
759:2007-12-07
746:1999-01-04
733:1998-10-23
719:1997-09-19
705:1996-08-30
691:1994-12-16
677:1993-03-31
664:1992-10-06
651:1992-11-05
637:1992-02-10
623:1992-02-04
609:1989-06-14
595:1987-05-01
582:1987-05-01
568:1988-05-25
554:1995-02-13
540:1994-05-13
526:1994-05-13
512:1991-12-20
498:1989-06-14
484:1987-06-30
471:1995-03-24
457:1987-02-18
443:1984-09-18
429:1983-12-16
415:1995-04-21
401:1993-04-05
387:1992-03-04
374:1996-02-29
360:1987-06-30
268:spur gears
204:Bombardier
155:turboprops
87:First run
3138:See also:
3018:Turbofans
3000:Turbojets
2933:247550535
2825:567827788
2709:0015-3710
2674:1047-4153
2644:0015-3710
2594:AINonline
2573:AINonline
2514:207398309
2506:0265-3818
2483:207200939
2475:0015-3710
2444:0015-3710
2413:173866706
2401:Rundschau
2380:0005-2175
2352:0005-2175
2214:0015-4806
2186:0015-3710
2101:0096-736X
2063:300373932
2039:CiteSeerX
2015:0015-3710
1943:0015-3710
1897:0015-3710
1638:Diameter:
1610:Data from
1538:Xian MA60
1224:Xian MA60
1203:Fokker 50
945:Fokker 50
937:Saab 2000
919:PW127XT-S
914:Mil Mi-38
816:PW127XT-N
800:PW127XT-M
784:PW127XT-L
197:NorOntair
125:Xian MA60
121:Fokker 50
59:Turboprop
47:PW120 in
3120:Aircraft
3008:J60/JT12
2793:(2007).
2109:44729718
1760:See also
1462:-200/300
1408:-300/320
1289:max. RPM
1253:JetTrain
1234:Xian Y-7
1153:-200/300
1134:PW123AF
1124:PW123AF
1100:-500/600
1089:-100/200
1035:Variant
1017:Aircraft
839:For the
495:PW123AF
328:1983-12
282:Variants
244:impeller
1864:12 July
1685:Turbine
1628:Length:
1277:Thermo.
1239:PW127C
1228:PW127J
1218:PW127H
1187:PW127G
1109:BAe ATP
1092:PW124B
1056:PW127A
1046:PW150A
927:D328eco
909:PW127TS
830:PW150A
770:PW127N
756:PW127M
743:PW127J
730:PW127H
716:PW127G
702:PW127F
688:PW127E
674:PW127D
661:PW127C
648:PW127B
634:PW127A
606:PW126A
579:PW125B
565:PW124B
551:PW123E
537:PW123D
523:PW123C
509:PW123B
468:PW121A
440:PW120A
412:PW119C
398:PW119B
384:PW119A
371:PW118B
357:PW118A
311:Variant
248:turbine
2989:(PWC)
2931:
2921:
2823:
2813:
2772:
2762:
2707:
2672:
2642:
2535:(UPI).
2512:
2504:
2481:
2473:
2442:
2411:
2378:
2350:
2212:
2205:Flying
2184:
2107:
2099:
2061:
2051:
2041:
2013:
1941:
1895:
1753:PW150:
1719:PW150:
1696:PW150:
1669:PW150:
1652:PW150:
1642:PW150:
1632:PW150:
1586:Dash 8
1544:PW150
1536:-100,
1534:Il-114
1525:ATR 72
1521:ATR 42
1517:An-140
1475:PW127
1469:CL-415
1460:Dash 8
1411:Dash 8
1406:ATR 42
1364:PW120
1316:PW118
1308:Length
1302:Height
1299:weight
1274:Series
1177:PW119
1167:PW150
1156:PW123
1113:PW126
1098:ATR 72
1087:ATR 72
1073:ATR 42
1062:ATR 42
970:PW150C
960:PW150B
903:PW125A
891:PW124A
845:An-132
620:PW127
592:PW126
481:PW123
454:PW121
426:PW120
339:PW118
325:PW115
320:Notes
317:Rating
238:Design
228:ATR 72
224:ATR 42
105:ATR 72
101:ATR 42
71:Canada
33:PW100
3111:PW900
3093:PW200
3088:PW150
3083:PW100
3051:PW800
3046:PW600
3041:PW500
3036:PW300
3031:JT25D
3026:JT15D
2904:(PDF)
2874:(PDF)
2849:(PDF)
2842:(PDF)
2397:(PDF)
2286:(PDF)
2248:(PDF)
2105:JSTOR
1961:(PDF)
1622:Type:
1588:-400
1557:1,020
1488:1,200
1431:1,200
1413:-100
1377:1,200
1329:1,300
1305:Width
1287:Prop.
1284:Power
1282:Mech.
1279:Power
1236:-200A
1004:ST40M
988:ST18M
932:PW130
897:PW125
885:PW124
879:PW119
55:Type
3078:PT6T
2929:OCLC
2919:ISBN
2857:2017
2821:OCLC
2811:ISBN
2770:OCLC
2760:ISBN
2705:ISSN
2681:2023
2670:ISSN
2640:ISSN
2510:OCLC
2502:ISSN
2479:OCLC
2471:ISSN
2440:ISSN
2409:OCLC
2376:ISSN
2348:ISSN
2210:ISSN
2182:ISSN
2097:ISSN
2059:OCLC
2049:ISBN
2011:ISSN
1939:ISSN
1893:ISSN
1866:2020
1293:BSFC
1164:-400
1142:-100
994:ST40
939:and
843:and
841:Q400
347:eshp
226:and
195:for
169:and
142:The
3073:PT6
2803:doi
2231:491
2089:doi
1914:489
1297:Dry
1205:/60
864:rpm
3156::
2927:.
2819:.
2809:.
2797:.
2782:^
2768:.
2750:.
2738:^
2717:^
2697:.
2662:.
2638:.
2632:.
2611:.
2591:.
2570:.
2549:.
2531:.
2508:.
2477:.
2463:.
2432:.
2321:.
2300:.
2265:.
2250:.
2202:.
2180:.
2174:.
2140:.
2103:.
2095:.
2071:^
2057:.
2047:.
2023:^
2009:.
1980:.
1967:.
1963:.
1931:.
1885:.
1857:.
1838:.
1823:^
1532:,
1519:,
847:.
270:.
199:.
173:.
3063:/
2979:e
2972:t
2965:v
2935:.
2859:.
2827:.
2805::
2776:.
2711:.
2683:.
2646:.
2597:.
2576:.
2516:.
2485:.
2446:.
2415:.
2382:.
2354:.
2325:.
2304:.
2269:.
2233:.
2216:.
2188:.
2144:.
2111:.
2091::
2065:.
2017:.
1984:.
1945:.
1916:.
1899:.
1868:.
1749::
1728::
1687::
1678::
1467:/
1121:T
1077:S
1043:D
103:/
20:)
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