| AD Number | 58-22-02 | Status | Active |
| Effective Date | Not specified | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | N/A |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Thompson Aircraft Sales |
| Model(s) | T-28A |
58-22-02 NORTH AMERICAN: Applies to all Model T-28A Aircraft Certificated in the Restricted Category. \n\n\tInspect 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. \n\n\t(USAF T.O. 1T-28A-6 Page 39, Item 11, covers this same subject.)