2014-17-08 R1
FR doc 2015-10075 · 80 FR 24791AD 2014-17-08 R1Published 2015-05-01Effective 2015-06-05
Revises 2014-17-08
Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.
Prompted by P&WC development of an additional single crystal CT blade that corrects the unsafe condition.
Full official abstract
We are revising airworthiness directive (AD) 2014-17-08 for all Pratt & Whitney Canada Corp. (P&WC) PT6A-114 and PT6A-114A turboprop engines. AD 2014-17-08 required initial and repetitive borescope inspections (BSIs) of compressor turbine (CT) blades, and the removal from service of blades that fail inspection. This new AD adds an additional single crystal CT blade, reduces the affected population, and corrects the Credit for Previous Action paragraph. This AD was prompted by P&WC development of an additional single crystal CT blade that corrects the unsafe condition. We are issuing this AD to prevent failure of CT blades, which could result in damage to the engine and damage to the airplane.
More directives for Pratt & Whitney Canada PT6A
- AD 2024-04-51 Airworthiness Directives; Pratt & Whitney Canada Corp. Engines Effective 2024-03-28
- AD 2022-08-13 Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop Engines Effective 2022-05-27
- AD 2016-05-13 Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop Engines Effective 2016-04-22
- AD 2014-17-08 Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop Engines Effective 2014-10-08
- AD 2012-09-10 Airworthiness Directives; Pratt & Whitney Canada Turboprop Engines Effective 2012-05-23
