AD 2005-17-19
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cirrus | Design Corporation Models SR20 and SR22 | Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes |
Unsafe Condition
The crew seats, under emergency landing dynamic loads, may fold forward at less than the 26 g required by 14 CFR Section 23.562(b)(2).
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Measure and adjust the crew seat break-over bolts and replace the crew seat recline locks on both crew seats. Follow Cirrus Design Corporation Alert Service Bulletin SB A2X-25-08, dated June 22, 2004, for Models SR20 (serial numbers 1005 through 1423) and SR22 (serial numbers 0002 through 0972).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 hours time-in-service (TIS) or within 180 days, whichever occurs first after October 13, 2005.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cirrus Design Corporation Models SR20 (serial numbers 1005 through 1455) and SR22 (serial numbers 0002 through 1044).
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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