Standard: EASA - AD 2008-0084

AIRBORNE AUXILIARY POWER - APU TURBINE WHEEL LIFE LIMIT - REDUCTION (APPLICABLE TO MICROTURBO SAPHIR 20 MODEL 095 AUXILIARY POWER UNIT) [CORRECTED: 26 FEBRUARY 2009]

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Organization: European Aviation Safety Agency
Document Number: ad 2008-0084
Publish Date: 2008-05-06
Page Count: 2
Change Type: NEW ADDITION
Available Languages: EN
DOD Adopted: NO
ANSI Approved: NO
Most Recent Revision: YES
Current Version: YES
Status: Inactive

This Standard References

Showing 5 of 5.

AD 2010-0079
EASA.EC.216.2008
EASA.IR.21
EASA.IR.M
PAD-08-045

Standards That Reference This Standard

Showing 2 of 2.

AD 2010-0079
AD 2010-13-01

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