- Effective
- August 17, 1965
- Models
- Bee Dee M-4, M-4, M-4-210
- Data sheet
- TCDS3A23
- Registered aircraft
- 63 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-115
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 | a0afe77c…20289d8 | FAA DRS (API key needed) |
On this page
The airworthiness directive
65-18-01 MAULE: Amdt. 39-115 Part 39 Federal Register August 19, 1965. Applies to Models Be Dee M-4, Serial Numbers 3 through 14; M-4, Serial Numbers 15 through 86; and M- 4-210, Serial Numbers 1001 through 1028 Airplanes.
Compliance required within the next 50 hours' time in service after the effective date of this AD unless already accomplished.
To prevent further failures of the attachment of the fuselage fabric to the windshield channel, install a metal reinforcement strip in accordance with Maule Service Letter No. 8, dated July 26, 1965, or later FAA-approved revision, or an FAA-approved equivalent.
This directive effective August 17, 1965.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 63
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1962 | 2 |
|---|---|
| 1963 | 16 |
| 1964 | 15 |
| 1965 | 13 |
| 1966 | 2 |
15 with no year recorded