PW127M Certified in 2007 with a maximum continuous rating of 2619 eshp (1953 kW). PW150 Twin Pack A proposed powerplant for the Airbus A400M Atlas; two PW150-based engines would be used to drive a single propeller.
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The Pratt & Whitney Canada PW100 aero engine family is a series of 2,000 to 5,000 horsepower (1,500 to 3,700 kW) turboprops manufactured by Pratt and Whitney's Canadian subsidiary. The engine first entered service in 1984.
Originally called the PT7, the PW100 uses a relatively unusual three-shaft engine configuration. In the PW100, a centrifugal LP impeller (except for the PW150 which uses a 3-stage axial LP compressor), driven by a single stage LP turbine, supercharges a centrifugal HP impeller, driven by a single stage HP turbine. Power is delivered to the offset propeller reduction gearbox via a third shaft, connected to a 2-stage free (power) turbine.
Variants:
PW115
PW118 Certified in 1986 with a maximum continuous rating of 1892eshp (1411kW), can be converted to a PW118A.
PW118A Certified in 1987 with a maximum continuous rating of 1893eshp (1412kW), can be converted to a PW118B.
PW118B Certified in 1996 with a maximum continuous rating of 1892eshp (1412kW). PW119
PW119A Certified in 1992 with a maximum continuous rating of 1948eshp (1453kW), can be converted to a PW119B. PW119B Certified in 1993 with a maximum continuous rating of 1941eshp (1448kW), can be converted to a PW119C. PW119C Certified in 1995 with a maximum continuous rating of 1941eshp (1448kW), can be converted to a PW119B. PW120 Certified in 1983 with a maximum continuous rating of 1787eshp (1333kW), can be converted to a PW121. PW120A Certified in 1984 with a maximum continuous rating of 1892eshp (1411kW), can be converted to a PW121. PW121 Certified in 1987 with a maximum continuous rating of 2044eshp (1524kW), can be converted to a PW120. PW121A Certified in 1995 with a maximum continuous rating of 1992eshp (1465kW). PW123 Certified in 1987 with a maximum continuous rating of 2261eshp (1687kW), can be converted to a PW123B, C, D or E. PW123AF Certified in 1989 with a maximum continuous rating of 2261eshp (1686kW), can be converted to PW123. PW123B Certified in 1991 with a maximum continuous rating of 2262eshp (1687kW), can be converted to a PW123. PW123C Certified in 1994 with a maximum continuous rating of 2054eshp (1532kW), can be converted to a PW123 or D. PW123D Certified in 1994 with a maximum continuous rating of 2054eshp (1532kW), can be converted to a PW123 or C. PW123E Certified in 1995 with a maximum continuous rating of 2261eshp (1687kW), can be converted to a PW123. PW124
PW124A
PW124B Certified in 1988 with a maximum continuous rating of 2522eshp (1881kW), can be converted to a PW123 or PW127.
PW125
PW125A
PW125B Certified in 1987 with a maximum continuous rating of 2261eshp (1687kW). PW126 Certified in 1987 with a maximum continuous rating of 2323eshp (1732kW) can be converted to a PW123 or PW126A. PW126A Certified in 1989 with a maximum continuous rating of 2493eshp (1859kW), can be converted to a PW123 or PW127D. PW127 Certified in 1992 with a maximum continuous rating of 2619eshp (1953kW), can be converted to a PW127C,E or F. PW127A Certified in 1992 with a maximum continuous rating of 2620eshp (1954kW), can be converted to a PW127B. PW127B Certified in 1992 with a maximum continuous rating of 2619eshp (1953kW). PW127C Certified in 1992 with a maximum continuous rating of 2880eshp (2148kW). PW127D Certified in 1993 with a maximum continuous rating of 2880eshp (2148kW), can be converted to a PW127B. PW127E Certified in 1994 with a maximum continuous rating of 2516eshp (1876kW), can be converted to a PW127M. PW127F Certified in 1996 with a maximum continuous rating of 2619eshp (1953kW), can be converted to a PW127M. PW127G Certified in 1997 with a maximum continuous rating of 3058eshp (2281kW). PW127H Certified in 1998 with a maximum continuous rating of 2880eshp (2148kW). PW127J Certified in 1999 with a maximum continuous rating of 2880eshp (2148kW). PW127M Certified in 2007 with a maximum continuous rating of 2619eshp (1953kW). PW150A Certified in 1998-06-24 with a maximum continuous rating of 5071 SHP (3782kW), although capable of up to 7000 SHP. Has a 3 stage axial low pressure compressor instead of the centrifugal NL unit on other variants. Used on the Bombardier Q400.
ST18M marine application for PW100
ST40M marine application for PW150A
Applications ATR 42 (PW120 on -200, PW127E on -500, PW127M on -600) ATR 72 (PW124B on -100 -200, PW127F or M on -500, PW127M on -600) BAe ATP (PW126) Bombardier 415 (PW123AF) Bombardier CL-215T (PW123AF) Bombardier Q100 (PW121) Bombardier Q200/Q300 (PW123) Bombardier Q400 (PW150) Canadair CL-415 (PW123AF) Dornier 328 (PW119) EADS CASA C-295 (PW127G) Embraer EMB 120 Brasilia (PW115, latterly PW118A) Euromil Mi-38 (PW127TS) Fokker 50 (PW125B) Fokker 60 (PW127B) Ilyushin Il-114 (PW127H) Xian MA60 (PW127J)
Pw127m Manual 2017
Specifications: Type: Turboprop Length: Diameter: Dry weight: 929 pounds Weight with accessories and fluid 1064 pounds Compressor: LP and HP independent centrifugal compressors. PW150 LP compressor is three-stage axial. Combustors: Annular reverse flow combustion chamber Turbine: Axial flow: single-stage HP; single-stage LP; the power turbine has two stages on all PW100 variants, and three stages on the PW150. Fuel type: JET A Oil system: Self-contained system Maximum power output: PW120 - takeoff 1800shp - Rto 2000shp PW121 - takeoff 1900shp - Rto 2100shp PW124 - takeoff 2160shp - Rto 2400shp PW127 - takeoff 2475shp - Rto 2750shp Turbine inlet temperature: max ITT for Reserve takeoff power, 816c Start 950c 5 seconds