AD 2012-01-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cirrus | Design Corporation | Airworthiness Directives; Cirrus Design Corporation Airplanes |
Unsafe Condition
Reports of partial loss of engine power due to a dislodged rubber gasket/seal being ingested into the turbocharger.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the air box flange welds and slots, make modifications as necessary, and replace the induction air box seals with reinforced silicone fiberglass seals part number 29486-001 for Group 1 airplanes. For Group 2 airplanes, inspect the air box flange welds and slots and make modifications as necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 10 hours time-in-service (TIS) after February 29, 2012.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cirrus Design Corporation Model SR22T airplanes, serial numbers 0001 through 0169, with specific exclusions and modifications for Group 1 and Group 2 airplanes as detailed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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