2012-01-11
FR doc 2012-1122 · 77 FR 3585AD 2012-01-11Published 2012-01-25Effective 2012-02-29
Requires inspection and modification of the air box flange welds and slots and installation of induction system air box seals as applicable.
Full official abstract
We are adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (Cirrus) Model SR22T airplanes. This AD was prompted by reports of partial loss of engine power due to a dislodged rubber gasket/seal being ingested into the turbocharger. This AD requires inspection and modification of the air box flange welds and slots and installation of induction system air box seals as applicable. We are issuing this AD to correct the unsafe condition on these products.
More directives for Cirrus SR22
- AD 2024-24-11 Airworthiness Directives; Cirrus Design Corporation Airplanes 2024-12-06
- AD 2009-26-01 Airworthiness Directives; Cirrus Design Corporation Model SR22 Airplanes 2009-12-14
- AD 2008-14-13 Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 ... 2008-07-10
- AD 2008-03-16 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... 2008-02-05
- AD 2007-24-13 Airworthiness Directives; Cirrus Design Corporation Model SR22 Airplanes 2007-11-29
