- Effective
- January 13, 1966
- Model
- M-4-210
- Data sheet
- TCDS3A23
- Registered aircraft
- 17 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-166
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 | d4f79250…1014066 | FAA DRS (API key needed) |
On this page
The airworthiness directive
65-28-04 MAULE: Amdt. 39-166 Part 39 Federal Register December 14, 1965. Applies to Model M-4-210 Airplanes, Serial Number 1001 through 1035.
Compliance required within the next 100 hours' time in service after the effective date of this AD unless already accomplished.
To prevent loss of engine power due to fuel starvation, modify the fuel system in accordance with Maule Service Letter No. 7, dated June 15, 1965, or later FAA-approved revision, or an equivalent approved by the Chief, Engineering and Manufacturing Branch, FAA Central Region.
This directive effective January 13, 1966.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 17
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1964 | 2 |
|---|---|
| 1965 | 10 |
5 with no year recorded