Airworthiness Directives (ADs)
CAA-2010-04-008
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 BR700-710A1-10 model engines if equipped with HP Turbine Discs
stage 1 or 2 listed in Table 1 or Table 2 of this AD, and All BR700-710A2-20 model engines if equipped with HP Turbine Discs stage 1 or 2 listed in Table 1 or Table 2 of this AD, and All BR700-710C4-11 model engines which have hardware configuration standard 710C4-11 engraved on the engine data plate (Service Bulletin SB-BR700-72-101466 standard not 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, GV-SP (G500, G550) and Bombardier BD-700-1A10, BD-700-1A11
series aeroplanes.
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Model Number
- Rolls-Royce Deutschland Ltd & Co KG BR700-710 engines
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CAA AD Number
- CAA-2010-04-008
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2010-0075
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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
Reference: Time Limits Manual (TLM) T-710-1BR (BR700-710A1-10), Time Limits Manual (TLM) T-710-2BR (BR700-710A2-20), Time Limits Manual (TLM) T-710-4BR (BR700-710C4-11) and Rolls-Royce Deutschland Alert NMSB-BR700-72-A900497 initial issue.
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Remarks
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