- Effective
- December 12, 1969
- Model
- Cirrus
- Data sheet
- TCDSG19EU
- Registered aircraft
- 15 matched by model
- Product
- Aircraft · Glider
- Amendment
- 39-926
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 | 21 KB | 77a127bb…851492c | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-02-10 SCHEMPP-HIRTH K.G.: Amdt. 39-926. Applies to Schempp-Hirth Cirrus sailplanes having serial numbers 19, 46, 47, 50, 53, 55, 57 through 69, 71 through 75, 77, and 79 through 82.
Compliance is required as indicated.
To prevent failure of elevator, aileron or airbrake flight control systems, before further flight after the effective date of this AD, unless already accomplished, accomplish the following:
Inspect askubal rod ends located in wings (4), fuselage (2), and fin (1) in accordance with Schempp-Hirth K.G. Technical Note No. 1/69 dated 20 October 1969, or an FAA-approved equivalent, to ensure that correct rod ends are installed in the elevator, aileron, and airbrake flight control systems. Incorrect rod ends may be recognized by thread of shanks going up to neck of bearing housing. If incorrect rod ends are installed, before further flight, replace them with correct rod ends in accordance with Schempp-Hirth K.G. Technical Note No. 1/69 dated 20 October 1969, or an FAA-approved equivalent.
This amendment is effective upon publication in the Federal Register as to all persons except those persons to whom it was made immediately effective by the telegram dated 12 December 1969, which contained this amendment.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 15
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1968 | 6 |
|---|---|
| 1969 | 7 |
| 1971 | 1 |
1 with no year recorded