Airworthiness Directives (ADs)
CAA-2012-08-014
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
- 2012/09/03
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Applicability
- BR700-710A1-10 and BR700-710A2-20 engines, all serial numbers (s/n).
BR700-710C4-11 engines, all s/n which (a) have hardware configuration standard 710C4-11 engraved on the engine data plate (RRD Service Bulletin (SB) SB-BR700-72-101466 standard not
incorporated), or (b) have hardware configuration standard 710C4-11/10 engraved on the
engine data plate (Service Bulletin SB-BR700-72-101466 standard incorporated).
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Model Number
- Rolls-Royce Deutschland Ltd & Co KG (RRD) BR700-710 serialengines.
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CAA AD Number
- CAA-2012-08-014
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2012-0166
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Effective Date
- 2012/09/13
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Subject
- Engine – High Pressure Turbine Rotor Disc Stage 1 and Stage 2
Life Limitation – Implementation.
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Reference Publications (Revision/ATA/SB)
- Rolls-Royce Deutschland Alert NMSB BR700-72-A900508 at initial issue.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
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Remarks
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