AD 2008-14-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cirrus | Design Corporation Model SR20 and SR22 | Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 Airplanes |
Unsafe Condition
The cabin door rod ends may fail, resulting in door separation from the airplane while in flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the cabin door rod ends with new parts, including a redesigned non-binding hinge pin, as specified in Cirrus Design Corporation Service Bulletin SB 2X-52-07 R4.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 hours time-in-service (TIS) after August 14, 2008, or within 180 days after August 14, 2008, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cirrus Design Corporation Models SR20 (serial numbers 1423 through 1906) and SR22 (serial numbers 0795 and 0820 through 2912).
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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