- Effective
- June 4, 1963
- Models
- M20, M20A
- Data sheet
- TCDS2A3
- Registered aircraft
- 81 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 | 8b28280b…196b4ad | FAA DRS (API key needed) |
On this page
The airworthiness directive
63-10-05 MOONEY: Amdt. 561 Part 507 Federal Register May 4, 1963. Applies to M20 Airplanes Serial Numbers 1002 Through 1200, and M20A Airplanes Serial Numbers 1201 Through 1540, With Empennage Attach Brackets P/N 3009, Installed.
Compliance required within 25 hours' time in service after the effective date of this AD, unless already accomplished.
Replace empennage attach bracket P/N 3009 and bearing plate P/N 3449 with bracket P/N 3471.
(Mooney Service Letter No. 20-60 dated November 17, 1959, also covers this change.)
This supersedes AD 59-09-01.
This directive effective June 4, 1963.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 81
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1956 | 6 |
|---|---|
| 1957 | 6 |
| 1958 | 11 |
| 1959 | 16 |
| 1960 | 18 |
| 1962 | 2 |
| 1965 | 1 |
| 1966 | 1 |
| 1976 | 1 |
19 with no year recorded