Airworthiness Directives (ADs)
CAA-2010-03-010
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
- 2010/03/22
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Applicability
- Pratt & Whitney (PW) JT8D-209, -217, -217C, and -219 turbofan engines
with front compressor front hub (fan hub), part number (P/N) 5000501-01, installed. These engines
are installed on, but not limited to, McDonnell Douglas MD-80 series airplanes.
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Model Number
- Pratt & Whitney JT8D-209, -217, -217C, and -219 Turbofan Engines
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CAA AD Number
- CAA-2010-03-010
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 97-17-04R1
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Effective Date
- 2010/04/22
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Subject
- To prevent fan hub
failure due to tierod, counterweight, or bushed hole cracking, which could result in an uncontained
engine failure and damage to the airplane.
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Reference Publications (Revision/ATA/SB)
- This AD revises AD 97-17-04(CAA AD No.:86-JT8-042A). Ref:PW Alert Service Bulletin (ASB) No. A6272 and Non-Destruct Inspection Procedure No. NDIP-892。
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Remarks
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