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.