Pratt & Whitney Canada PT7 / PW100 / PW115 / PW118 / PW119 / PW120 / PW123 / PW124 / PW126 / PW126 / PW127 / PW150
PW120
PW127 Maintenance Manual chapter 72-00. Click the start the download. Report this file. Description Pratt&Whitney CanadaTurboprop engine PW-127H maintenance manual chapter 72-00 Description&Operation Account 207.46.13.232. Pratt Whitney Pw100 Maintenance Manual For Atr72 The PW127M is a derivative of the PW127F and PW127E engines that today power the ATR 42-500 and ATR 72-500 regional turboprop aircraft. The PW127M will be offered on these aircraft going forward. Pratt & Whitney Canada PW127M Engine Certified to Power. ATR 72 Engine PW127 PCE-127089. Pratt&Whitney CanadaTurboprop engine PW-127H maintenance manual chapter 72-00 Description&Operation Account 207.46.13.51. Access interactive maintenance manuals and illustrated parts catalogs. Download a copy of your manual to your device. Save your shopping cart and transfer it to another user. Quickly access your preferred publications by clicking on the. and activating the publications widget on your dashboard. Our interactive electronic technical publications. Access interactive maintenance manuals and illustrated parts catalogs. Download a copy of your manual to your device. Save your shopping cart and transfer it to another user. Quickly access your preferred publications by clicking on the. and activating the publications widget on your dashboard. Our interactive electronic technical publications.
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
Pw127m Manual 2017
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.
Pw127m Manual Free
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)
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
The PW127M is a derivative of the PW127F and PW127E engines that today power the ATR 42-500 and ATR 72-500 regional turboprop aircraft.
LONGUEUIL, Que., March 10, 2008 – Pratt & Whitney Canada has received type certification from Transport Canada and the European Aviation Safety Agency for the PW127M engine, the newest member in the PW100 regional turboprop family. The PW127M offers 5 percent more power than its predecessor, the PW127F engine. Pratt & Whitney Canada (P&WC) is a United Technologies (NYSE: UTX) company.
The PW127M is a derivative of the PW127F and PW127E engines that today power the ATR 42-500 and ATR 72-500 regional turboprop aircraft. The PW127M will be offered on these aircraft going forward and will also be the standard engine on the newest versions of ATR’s aircraft, the ATR 42-600 and the ATR 72-600.
'The new PW127M turboprop engine is designed to deliver even better performance in both hot and high conditions,' said Keyvan Fard, senior vice president, Sales & Marketing. 'It is the most recent example of our clear commitment to the regional turboprop market.'
Worldwide orders for regional turboprop-powered aircraft have surged in recent years, due largely to the advantages they offer in lower fuel consumption and emissions within the short-haul regional airline sector. The PW100 family is a leader in this market with over 4,000 engines flying in 121 countries and more than 100 million operating hours accumulated to date.
Pw127m Manual Pdf
Pratt & Whitney Canada, based in Longueuil, Quebec, is a world leader in the design, manufacture and service of aircraft engines powering business, general aviation and regional aircraft, and helicopters. The company also offers auxiliary power units and industrial gas turbines. United Technologies, based in Hartford, Conn., USA, is a diversified company providing high technology products and services to the global aerospace and building industries.