- Model
- T-50
- Data sheet
- TCDSA-722
- Registered aircraft
- 37 matched by model
- Product
- Aircraft · Small airplane
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 19 KB | d386d168…efbf3fd | FAA DRS (API key needed) |
On this page
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 TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 37
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1941 | 1 |
|---|---|
| 1942 | 7 |
| 1943 | 15 |
| 1944 | 5 |
| 1945 | 2 |
| 1949 | 1 |
6 with no year recorded