- Effective
- September 12, 1970
- Models
- MS 880B, MS 885, MS 894A
- Data sheet
- TCDS7A14
- Registered aircraft
- 31 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-1066
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 | 895ae064…94294c8 | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-17-04 MORANE SAULNIER: Amdt. 39-1066. Applies to Models MS. 880B, MS. 885, and MS. 894A airplanes.
To prevent possible fires resulting from leaks in the fuel system, within the next 50 hours' time in service after the effective date of this AD, unless already accomplished, modify the fuel system by installing flexible fuel lines between the engine pump and the carburetor and in the fuel pressure system in accordance with Parts 2 and 3 of SOCATA Service Bulletin No. 56, dated December 1968, or later SGAC-approved issue or an FAA-approved equivalent.
This amendment becomes effective September 12, 1970.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 31
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1961 | 1 |
|---|---|
| 1968 | 1 |
| 1969 | 2 |
| 1970 | 2 |
| 1971 | 6 |
| 1972 | 11 |
| 1974 | 1 |
7 with no year recorded