- Effective
- October 26, 1970
- Models
- MS 880B, MS 885, MS 894A
- Data sheet
- TCDS7A14
- Registered aircraft
- 31 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-1083
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 | 5acabda0…4f51a55 | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-20-02 MORANE SAULNIER: Amdt. 39-1083. Applies to Moels MS. 880B, MS.885, and MS.894A airplanes.
To maintain correct alignment of the airspeed limit markings on the cover glass of the airspeed indicator with the face of the dial, within the next 50 hours' time in service after the effective date of this AD, unless already accomplished, align the cover glass and mark its correct position in accordance with Socata Service Bulletin No. 73 dated March 1970, or later SGAC- approved issue or an FAA-approved equivalent.
This amendment becomes effective October 26, 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