Airworthiness Directives (ADs)
CAA-2011-11-004(已有後續修訂版)
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
- 2011/11/23
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Applicability
- Models RB211 Trent 553-61, 553A2-61, 556-61, 556A2-61, 556B-61, 556B2- 61, 560-61 and 560A2-61 engines, all serial numbers and These engines are known to be installed on, but not limited to, Airbus A340- 500 and A340-600 series aeroplanes.
Models RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, all serial numbers and These engines are known to be installed on, but not limited to, Airbus A330 series aeroplanes.
Models RB211 Trent 875-17, 877-17, 884-17, 884B-17, 892-17, 892B-17 and 895-17 engines, all serial numbers and These engines are known to be installed on, but not limited to, Boeing 777 series aeroplanes.
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Model Number
- ROLLS-ROYCE PLC RB211 Trent 500, 700 and 800 engines
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CAA AD Number
- CAA-2011-11-004(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2011-0221
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Effective Date
- 2011/11/28
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Subject
- Engine – Intermediate Pressure Compressor Rotor Shaft and
Balance Weights – Inspection / Modification
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Reference Publications (Revision/ATA/SB)
- ATA 72. This AD supersedes EASA AD 2010-0266R1 dated 06 January 2011.
Ref. Rolls-Royce NMSB RB211-72-AF260 Revision 5 dated 7 July 2011 and Rolls-Royce NMSB RB211-72-AG085 Revision 2 dated 7 July 2011 and Rolls-Royce NMSB RB211-72-AG264 Revision 5 dated 21 March 2011 and Rolls-Royce NMSB RB211-72-AG270 Revision 4 dated 21 March 2011 and Rolls-Royce NMSB RB211-72-G448 Revision 3 dated 7 July 2011 and Rolls-Royce SB RB211-72-AG401 Revision 2 dated 5 July 2011 and Rolls-Royce SB RB211-72-AG402 Revision 2 dated 7 July 2011. The reference number of the applicable Rolls-Royce NMSB/SB might change
to incorporate an “A” (indicating categorisation as “Alert”, within the Rolls- Royce system).
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Remarks
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