- Effective
- April 16, 1966
- Models
- M.S. 760 (Paris I), M.S. 760.A (Paris IA), M.S. 760B (Paris II)
- Data sheet
- TCDS7A3
- Registered aircraft
- 7 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-211
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 | 86ebaad8…d3ed231 | FAA DRS (API key needed) |
On this page
The airworthiness directive
66-08-05 MORANE-SAULNIER: Amdt. 39-211 Part 39 Federal Register March 17, 1966. Applies to Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes. Compliance required within the next 300 hours' time in service after the effective date of this AD unless already accomplished. Replace aluminum alloy rudder control system rod, P/N 0176-27.1.191, located between Stations 5 and 10, with steel rod, P/N 0176-27.1.218. (Morane-Saulnier Service Bulletin No. 45 pertains to this subject.) This directive effective April 16, 1966.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 7
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1959 | 1 |
|---|---|
| 1966 | 1 |
5 with no year recorded