AD 2000-24-23
Unsafe Condition
Cracks could occur in the welded parts of airbrake arms, potentially preventing the pilot from using the airbrake system.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the airbrake control system for cracks within 60 calendar days after January 27, 2001, and then every 12 calendar months. If cracks are detected, replace the airbrake control system before further flight. Install specific parts (S.N. CENTRAIR part numbers $YO57D or $Y818E, or FAA-approved equivalents) depending on the glider configuration.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 60 calendar days after January 27, 2001, and then every 12 calendar months for repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
S.N. CENTRAIR Models 101, 101A, 101P, and 101AP gliders, all serial numbers up to but not including 101A0628, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.