AD 2002-24-08
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 rocket cone's internal diameter variance at the threaded end may cause the retaining nut to not be fully secured, leading to the CAPS activation cable not pulling the igniter pin free to release the parachute in an emergency situation.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the CAPS handle access cover, replace the CAPS activation handle bracket, and replace the CAPS activation cable.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 days after the effective date of this AD, unless already accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cirrus Design Corporation Models SR20 and SR22 airplanes with the affected Cirrus Airplane Parachute System (CAPS).
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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