| AD Number | 70-20-02 | Status | Active |
| Effective Date | October 26, 1970 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-1083 |
| 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 894A |
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.