| AD Number | 71-19-01 | Status | Active |
| Effective Date | September 07, 1971 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-1283 |
| Product Type | ["Aircraft"] | Product Subtype | ["Glider"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Alexander Schleicher GmbH & Co. |
| Model(s) | K 8 K 8 B |
71-19-01 SCHLEICHER: Amendment 39-1283. Applies to Model K8 Gliders.
Compliance is required within the next 25 hours' time in service after the effective date of this AD unless already accomplished.
To prevent failure of the airbrake bellcrank inboard bearing bracket to main fuselage attachment welds, modify the bracket attachment in accordance with Schleicher Modification No. 10, dated October 25, 1962 or an FAA-approved equivalent.
This amendment becomes effective September 7, 1971.