AD 2002-21-02

final rule
Data completeness: 70%

Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 Airplanes

AD Number
2002-21-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-CE-41-AD
FR Citation
67 FR 63815

Applicability

TypeManufacturerModelDetails
aircraft Cirrus Design Corporation Model SR20 and SR22 Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 Airplanes

Unsafe Condition

Self-locking retaining nut on the roll and yaw trim cartridges could come off during flight, potentially jamming the corresponding flight control system and leading to loss of control of the airplane.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace the self-locking retaining nut on the roll and yaw trim cartridges with a new self-locking retaining nut that has a higher axial load capability.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Cirrus Design Corporation Model SR20 and SR22 airplanes.

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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