pratt & whitney canada, inc. Airworthiness Directives

11 ADs indexed for pratt & whitney canada, inc. aircraft.

Recent ADs

2016-05-13

final rule

Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop Engines

Unsafe Condition: incidents of corrosion and perforation of the two-ply Cu-Be bellows in Woodward fuel control units (FCUs)

Effective: Apr 22, 2016 Category: engine Compliance: within 500 flight hours or one year after the effective date of this AD, whichever occurs first

Why matched: Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop Engines

2012-09-10

final rule

Airworthiness Directives; Pratt & Whitney Canada Turboprop Engines

Unsafe Condition: Failures of certain first stage sun gears, manufactured by TAATI, leading to potential failure of the sun gear and planet gears in the propeller reduction gearbox assembly.

Effective: May 23, 2012 Category: engine Compliance: Within 40 operating hours after the effective date of the AD.

Why matched: Airworthiness Directives; Pratt & Whitney Canada Turboprop Engines

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2010-18-09

final rule

Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW530A, PW545A, and PW545B Turbofan Engines

Unsafe Condition: Engine intercompressor bleed valve/servo valve malfunction causing engine surge, lack of response to Power Lever input, and crew commanded engine shutdown.

Effective: Sep 10, 2010 Category: aircraft Compliance: Within the defined compliance time specified in the AD.

Why matched: Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW530A, PW545A, and PW545B Turbofan Engines

2006-24-08

final rule

Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW535A Turbofan Engines; Correction

Unsafe Condition: The FAA is correcting airworthiness directive (AD) 2006-24-08. That AD applies to Pratt & Whitney Canada (P&WC) PW535A turbofan engines. We published that AD in the Federal Register on December 4, ...

Effective: May 22, 2007 Category: aircraft

Why matched: Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW535A Turbofan Engines

2006-08-13

final rule

Airworthiness Directives; Pratt & Whitney Canada (PWC) PW535A Turboshaft Engines

Unsafe Condition: PW535A turboshaft engines experiencing lack of response to the power lever input during engine acceleration, due to an incorrect adjustment of the HFC ratio unit setscrew.

Effective: May 8, 2006 Category: engine Compliance: Within 50 flight hours time-in-service after the effective date of this AD.

Why matched: Airworthiness Directives; Pratt & Whitney Canada (PWC) PW535A Turboshaft Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2003-03-21

final rule

Airworthiness Directives; Pratt & Whitney Canada PW500 Series Turbofan Engines

Unsafe Condition: Reports of fuel dripping from engine nacelles caused by leaking flexible fuel tubes.

Effective: Feb 20, 2003 Category: engine Compliance: Not specified in the provided text.

Why matched: Airworthiness Directives; Pratt & Whitney Canada PW500 Series Turbofan Engines

98-17-10

final rule

Airworthiness Directives; Pratt & Whitney Canada PW530A Series Turbofan Engines

Unsafe Condition: Rubbing of the second stage stator vanes on the compressor rotor due to insufficient original type design clearance, which can result in inflight engine shutdowns and significant compressor rotor d...

Effective: Oct 21, 1998 Category: engine Compliance: within 200 hours time in service (TIS) after the effective date of this AD, or prior to December ...

Why matched: Airworthiness Directives; Pratt & Whitney Canada PW530A Series Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

97-04-12

final rule

Airworthiness Directives; Pratt & Whitney Canada PT6 Series Turboprop Engines

Unsafe Condition: Malfunctions of the compressor bleed-off valve (BOV) due to broken cotter pins and improperly installed guide shaft pins, which can result in engine power reduction and forced landing.

Effective: Mar 14, 1997 Category: engine Compliance: Within 100 hours time in service after the effective date of this AD, but no later than April 2, ...

Why matched: Airworthiness Directives; Pratt & Whitney Canada PT6 Series Turboprop Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

95-13-08

final rule

Airworthiness Directives; Pratt & Whitney Canada Model PT6A-67D Turboprop Engines

Unsafe Condition: Cracking and irregularities in the compressor turbine (CT) disk and blades due to high cycle fatigue (HCF) fractures in the fir tree area of the blade while exposed to normal engine vibrations.

Effective: Jun 15, 1994 Category: engine Compliance: Within specified intervals based on time-in-service (TIS) since last inspection or by the next sh...

Why matched: Airworthiness Directives; Pratt & Whitney Canada Model PT6A-67D Turboprop Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

91-15-02

final rule

PRATT & WHITNEY CANADA, INC. Model JT15D-4B Engines

Unsafe Condition: Rupture of the gas generator case (GGC) which could result in an inflight shutdown, aborted takeoff, and/or damage to the aircraft.

Effective: Aug 22, 1991 Category: engine Compliance: within 10 days after the effective date of this AD, unless already accomplished within the previo...

Why matched: PRATT & WHITNEY CANADA, INC. Model JT15D-4B Engines

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

91-01-03

final rule

PRATT & WHITNEY CANADA Model PW118, PW118A, PW120, PW120A, PW121, and JT15D- 5 Engines

Unsafe Condition: Fuel leakage from Hamilton-Standard Model JFC118 hydromechanical fuel control units (HMU) excluding those marked 'MS090-001' poses a fire hazard in the engine nacelle.

Effective: Jan 7, 1991 Category: engine Compliance: Required as indicated, unless already accomplished.

Why matched: PRATT & WHITNEY CANADA Model PW118, PW118A, PW120, PW120A, PW121, and JT15D- 5 Engines

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