Airworthiness Directives (ADs)
CAA-2002-11-017B
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
- 2006/10/25
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Applicability
- This AD applies to the following Pratt & Whitney (PW) JT8D- 1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, -17AR, -209, -217, -217A, -217C, and -219 turbofan engines, with 8th stage high pressure compressor (HPC) front hubs
These engines are installed on, but not limited to, Boeing DC-9, MD-80 series, 727 series, and 737 series airplanes.
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Model Number
- Pratt & Whitney JT8D-1, -1A, -1B, -7, - 7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, -17AR, -209, -217, - 217A, -217C, and -219 Turbofan Engines
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CAA AD Number
- CAA-2002-11-017B
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2006-17-07R1
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Effective Date
- 2006/11/02
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Subject
- To prevent a rupture of an HPC front hub or an HPC disk that could result in an uncontained engine failure and damage to the airplane.
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Reference Publications (Revision/ATA/SB)
- Revises AD 2006-17-07(CCAA AD 2002-11-017A)
Ref. Pratt & Whitney Alert Service Bulletin No.JT8D A6430R2 and JT8D A6468
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Remarks
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