AD 2025-20-11

final rule
Data completeness: 80%

Airworthiness Directives; Textron Aviation Inc. Airplanes

AD Number
2025-20-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2025-3424
FR Citation
90 FR 47536

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc Airworthiness Directives; Textron Aviation Inc. Airplanes
aircraft Aviat Various Airworthiness Directives; Textron Aviation Inc. Airplanes

Unsafe Condition

Incorrect rivets used during installation of the rudder control pushrod do not meet the strength requirements of the type design. Failure of a rudder control pushrod may result in a rudder jam or loss of rudder control.

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

Required Actions

A visual inspection of the attaching rivets of the pilot and copilot rudder control pushrods for incorrect rivets and replacement if necessary.

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

Compliance Time

Within 20 hours time-in-service or 30 days, whichever occurs first.

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

Affected Aircraft

Textron Model B200GT, B200CGT, B300, and B300C airplanes.

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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