Airworthiness Directives (ADs)
CAA-2010-04-009
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
- 2010/04/22
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Applicability
- All BR700-710C4-11 model engines which have hardware configuration
standard 710C4-11/10 engraved on the engine data plate (Service Bulletin SB-BR700-72-101466 standard incorporated) and if equipped with HP Turbine Discs stage 1 or 2 listed in Table 1 or Table 2 of this AD. These engines are known to be installed on, but not limited to Gulfstream GV-SP (G500, G550) aeroplanes.
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Model Number
- Rolls-Royce Deutschland Ltd & Co KG BR700-710 engines
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CAA AD Number
- CAA-2010-04-009
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2010-0076
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Effective Date
- 2010/05/04
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Subject
- Engine – High Pressure (HP) Turbine Discs Stage 1 and 2
Assembly Life Limits – Modification
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Reference Publications (Revision/ATA/SB)
- ATA 72
Ref: Supplementary Time Limits Manual (TLM) T-710-5BR, Rolls-Royce Deutschland Alert NMSB-BR700-72-A900492 initial issue.
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Remarks
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Download
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