Standard: EASA - AD 2008-0099
ENGINE - HP COMPRESSOR STAGE 1- 4 SHAFT - LIFE LIMIT REDUCTION (APPLICABLE TO ROLLS-ROYCE PLC RB211 TRENT 800 ENGINES) [CORRECTED: 12 JUNE 2008]
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|Organization:||European Aviation Safety Agency|
|Document Number:||ad 2008-0099|
|Change Type:||NEW ADDITION|
|Most Recent Revision:||YES|
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