- Effective
- September 7, 1971
- Models
- K 8, K 8 B
- Data sheet
- TCDS7G4
- Registered aircraft
- 21 matched by model
- Product
- Aircraft · Glider
- Amendment
- 39-1283
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 | 18 KB | 5022b142…a4e1945 | FAA DRS (API key needed) |
On this page
The airworthiness directive
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.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 21
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1960 | 1 |
|---|---|
| 1962 | 2 |
| 1963 | 2 |
| 1964 | 3 |
| 1965 | 1 |
| 1966 | 1 |
| 1967 | 1 |
10 with no year recorded