- Model
- T-28A
- Data sheet
- TCDSAR-30
- Registered aircraft
- 2 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 | 18 KB | 216703f2…e6c50fc | FAA DRS (API key needed) |
On this page
The airworthiness directive
58-22-02 NORTH AMERICAN: Applies to all Model T-28A Aircraft Certificated in the Restricted Category.
Inspect the main landing gear trunnion shaft every 200 hours with a borescope or by an equivalent method for fatigue cracks emanating from the bolt holes. Replace all defective shafts.
(USAF T.O. 1T-28A-6 Page 39, Item 11, covers this same subject.)
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 2
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.