- Models
- M-62A, M-62A-3, M-62A-4, M-62B, M-62C
- Data sheet
- TCDSA-724
- Registered aircraft
- 219 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 | e1057bf0…77ab56d | FAA DRS (API key needed) |
On this page
The airworthiness directive
47-07-02 FAIRCHILD: (Was Service Note 3 of AD-724-2.) Applies to M-62 Series Aircraft.
At each periodic inspection, determine if any looseness exists in elevator hinge attachments to rear spar of stabilizer. All loose hinges should be tightened. This will necessitate cutting oval shaped openings in the lower surface of the stabilizer just forward of the rear spar. After nuts are drawn up and safetied the openings should be covered with fabric patches.
(Fairchild Service Bulletin 44-2-C dated January 14, 1944, 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 · 219
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1940 | 4 |
|---|---|
| 1941 | 15 |
| 1942 | 29 |
| 1943 | 86 |
| 1944 | 11 |
| 1945 | 6 |
| 1946 | 5 |
| 1949 | 1 |
| 1954 | 1 |
| 1959 | 1 |
| 1965 | 4 |
56 with no year recorded