Airworthiness Directives (ADs)
CAA-2012-11-004(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
- 2012/11/14
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Applicability
- RB211-524-524G2-T-19, RB211-524G3-T-19, RB211-524H-T-36 and RB211-524H2-T-19 engines, all serial numbers, except those incorporating Modification (Mod) 72-AG706.
RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, all serial numbers, except those incorporating Mod. 72-AG707.
RB211 Trent 875-17, 877-17, 884-17, 884B-17, 892-17, 892B-17 and 895-17 engines, all serial numbers, except those incorporating Mod. 72-AG705.
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Model Number
- ROLLS-ROYCE RB211-524, RB211 Trent 700 and RB211 Trent 800 Engines
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CAA AD Number
- CAA-2012-11-004(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2009-0243R3
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Effective Date
- 2012/11/27
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Subject
- Engine – Front Combustion Liner Inner Wall – Inspection
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Reference Publications (Revision/ATA/SB)
- (i) This AD revises EASA AD 2009-0243R2 dated18 February 2011, including the Correction dated 22 February 2011. (ii) Rolls-Royce NMSB RB.211-72-AF458 Revision 4 dated 09 March 2009, or Revision 5 dated 20 April 2011. Rolls-Royce SB 72-AG705 dated 13 July 2012.
Rolls-Royce SB 72-AG706 dated 21 June 2012. Rolls-Royce SB 72-AG707 dated 21 June 2012. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
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Remarks
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