AD 82-17-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | DG Flugzeugbau GmbH | LS-3 | Airworthiness Directives; ROLLADEN SCHNEIDER Model LS1-f and LS3 Sailplanes |
| aircraft | DG Flugzeugbau GmbH | LS1-f | Airworthiness Directives; ROLLADEN SCHNEIDER Model LS1-f and LS3 Sailplanes |
Unsafe Condition
Potential sailplane structural failure or loss of control due to elevator flutter
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Apply red tape to the airspeed indicator and alter the airspeed limit placard restricting VNE to 124 MPH (200 km/h, 108 knots) within 15 hours time in service after the effective date. Modify the elevator control system by December 15, 1982, by replacing the spring assembly with a solid link.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 15 hours time in service after the effective date of this AD and by December 15, 1982
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
ROLLADEN SCHNEIDER Model LS1-f and LS3 sailplanes not incorporating Technical Bulletin No. 38/3013 dated June 18, 1979
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.