Airworthiness Directives (ADs)
CAA-2010-03-009
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
- International Aero Engines (IAE) V2500-A1, V2522-A5, V2524-A5,
V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan
engines with high-pressure (HP) compressor stage 3-8 drums, part numbers (P/Ns) 6A4900, 6A5467,
6A6473, 6A7383, 6A7384, 6A7385, and 6A7401, installed. These engines are installed on, but not
limited to, Airbus A319, A320, and A321 series airplanes and Boeing MD-90 airplanes.
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Model Number
- International Aero Engines (IAE) V2500-A1, V2522-A5, V2524-A5,
V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 Turbofan
Engines
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CAA AD Number
- CAA-2010-03-009
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2010-06-18
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Effective Date
- 2010/04/22
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Subject
- To inspect for cracks in the vortex reducer. Cracks in the vortex reducer
could result in an uncontained failure of the high-pressure (HP) compressor stage 3-8 drum and
subsequent damage to the airplane.
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Reference Publications (Revision/ATA/SB)
- None.
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Remarks
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Download
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