- Effective
- November 4, 1975
- Models
- MS 880B, MS 885, MS 892A-150, MS 893A, MS 894A
- Data sheet
- TCDS7A14
- Registered aircraft
- 33 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-2405
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 | 20 KB | c0f4bdb5…888d16c | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-22-15 MORANE SAULNIER (SOCATA) RALLYE: Amendment 39-2405. Applies to MS880B and MS885 airplanes, certificated in all categories, except serial numbers 1962 and subsequent; and MS892A150, MS893A, and MS894A airplanes, certificated in all categories, except serial numbers 11993 and subsequent.
Compliance is required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent possible interference between the control stick and floor hat section, accomplish the following:
Modify the floor adjacent to the control stick by increasing the clearance between the floor and control stick in accordance with the "Description" paragraph in Socata Service Bulletin No. 104 GR-27-09, dated September, 1972, or an FAA-approved equivalent.
This amendment becomes effective November 4, 1975.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 33
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 | 13 |
| 1974 | 1 |
7 with no year recorded