- Effective
- May 1, 1967
- Models
- M20, M20A
- Data sheet
- TCDS2A3
- Registered aircraft
- 81 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-370
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 | d9e817ad…cdc58df | FAA DRS (API key needed) |
On this page
The airworthiness directive
67-11-05 MOONEY: Amdt. 39-370, Part 39, Federal Register March 30, 1967. Applies to Model M20 Airplanes, Serial Numbers 1002 through 1200, and Model M20A Airplanes, Serial Numbers 1201 through 1534.
Compliance required within the next 100 hours' time in service after the effective date of this AD, unless replacement has already been accomplished in accordance with AD 65-22-03, as amended August 20, 1966.
To prevent failure of the tail truss due to internal corrosion for which inspection is impractical, remove and replace P/N 4009 with a new tail truss P/N 480007 or an equivalent approved by the Director, Southwest Region, FAA.
This directive effective May 1, 1967.
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