AD 47-30-02

final rule
Data completeness: 60%

Airworthiness Directives; CESSNA Model T-50 Airplanes

AD Number
47-30-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company T-50 Airworthiness Directives; CESSNA Model T-50 Airplanes

Unsafe Condition

The absence of reinforcing doubler plates on the ends of brake pedal links, P/N 53046, could result in failure of the brake pedal links due to overstress at the fitting holes.

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

Required Actions

Inspect the ends of brake pedal links, P/N 53046, for reinforcing doubler plates. If doubler plates are missing, remove the links and rivet two 0.040 inch x 1/2-inch x approximately 2-inch length 24ST aluminum alloy reinforcing doubler plates to each end using two 1/8-inch A17ST rivets through both doublers and the link.

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

Compliance Time

no later than next 100 hour inspection

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

Affected Aircraft

Cessna Model T-50 Aircraft

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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