Airworthiness Directives (ADs)
CAA-2013-08-001A
The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.
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Issue Date
- 2013/11/04
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Applicability
- Pratt & Whitney Canada model PT6A-114 and PT6A-114A engines, with Pre-SB1669 or Pre-SB 1727 Configuration CT Blades Installation.
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Model Number
- Pratt & Whitney Canada model PT6A-114 and PT6A-114A engines.
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CAA AD Number
- CAA-2013-08-001A
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Aeronautics Authority of Original AD
- Transport Canada Civil Aviation
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Original AD Number
- CF-2013-21R1
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Effective Date
- 2013/11/13
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Subject
- Compressor Turbine (CT) Blade Failures
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Reference Publications (Revision/ATA/SB)
- This AD supersedes TCCA AD CF-2013-21 (CAA-2013-08-001). (ii) P&WC SB 1669R9 dated 28 June 2013 or the Accomplishment Instructions in SB 1727 dated 23 August 2013, or later revisions of either SB approved by the Chief Continuing Airworthiness, Transport Canada.
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Remarks
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Download
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