| AD Number | 75-22-15 | Status | Active |
| Effective Date | November 04, 1975 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2405 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | SOCATA |
| Model(s) | MS 880B MS 885 MS 892A-150 MS 893A MS 894A |
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.