Airworthiness Directives (ADs)
CAA-2008-07-009
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
- 2008/07/21
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Applicability
- This AD applies to IAE V2500-A1, V2522-A5, V2524-A5, V2527- A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, and V2528-D5 turbofan engines with a part listed by part number (P/N) in this AD installed. These engines are installed on, but not limited to, Airbus A319, A320, A321, and McDonnell Douglas MD-90 airplanes.
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Model Number
- International Aero Engines AG (IAE) V2500 Series
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CAA AD Number
- CAA-2008-07-009
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2008-14-15
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Effective Date
- 2008/08/20
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Subject
- To prevent heat damage to high-pressure turbine (HPT) and low-pressure turbine (LPT) critical life limited hardware such as the HPT stage 1-2 airseal. Damage to the HPT stage 1-2 airseal could cause uncontained engine failure and damage to the airplane.
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Reference Publications (Revision/ATA/SB)
- International Aero Engines Service Bulletin No. V2500-ENG- 72-0541, Revision 4.
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Remarks
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