| AD Number | 71-15-03 | Status | Active |
| Effective Date | July 26, 1971 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-1247 |
| 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 894A |
71-15-03 SOCATA MORANE SAULNIER: Amdt. 39-1247. Applies to Morane Saulnier Model MS.880B and MS.894A airplanes.
Compliance is required within the next 50 hours' time in service after the effective date of this AD unless already accomplished.
To prevent short circuits in the cables of the generator system, rework the cables of the generator system in accordance with paragraph 2 degrees/, SOCATA Service Bulletin No. 79 (Gr. 24-01), dated October 1970, or an FAA-approved equivalent.
This amendment becomes effective 26 July 1971.