AD 2001-25-03

final rule
Data completeness: 70%

Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes

AD Number
2001-25-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-CE-46-AD
FR Citation
66 FR 63913

Applicability

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

Unsafe Condition

Understrength rivets on the elevator torque tube and rudder hinge, which could result in failure of the control surfaces.

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

Required Actions

Inspect one time for understrength rivets on the elevator torque tube and rudder hinge. Replace any understrength rivets with new rivets, part number MS20470AD4, or FAA-approved equivalent part number.

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 after December 17, 2001 (the effective date of this AD).

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

Affected Aircraft

Cirrus Design Corporation Models SR20 (serial numbers 1134 through 1159) and SR22 (serial numbers 0003 through 0119).

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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