# AD 47-30-02: Brake Pedal Links

- Type: Airworthiness directive
- Status: Current
- Products: Cessna T-50
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Small airplane
- Registered aircraft: 37 may be affected, by airframe or engine model (OpenAirDocs)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FC00F9C934053A6A86256A3400606F06.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/47-30-02

## The airworthiness directive

47-30-02 CESSNA: (Was Mandatory Note 12 of AD-722-5.) Applies to T-50 Aircraft.

Compliance required no later than next 100 hour inspection.

Inspect the ends of the brake pedal links, P/N 53046, for reinforcing doubler plates around the fitting holes. If the doubler is not in evidence, 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 of each link using two 1/8-inch A17ST rivets through both doublers and the link on the far side of the joggle from the fitting holes.

## Affected data sheets (1) (OpenAirDocs)

The type certificate data sheets whose models the AD names.

- [TCDS A-722](https://openairdocs.org/tcds/A-722): Cessna Aircraft Company; names 1 of 1 models: T-50 (Army AT-17 and UC-78 series; Navy JRC-1)

## Registered aircraft it may apply to (OpenAirDocs)

Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment.

- Aircraft: 37 (37 by airframe model, 0 by engine model)
- Makers: Cessna 37

Models with the most aircraft:

- [Cessna T-50](https://openairdocs.org/model/cessna-t-50): 37 aircraft (airframe model)

All 1 models: https://openairdocs.org/ad/47-30-02/models.md
Every aircraft: https://openairdocs.org/ad/47-30-02/aircraft.md

Its text cites no advisory circulars or STCs.

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