AD 2012-18-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; GA200 (Pty) Ltd Airplanes |
Unsafe Condition
Failure of the strut bolt through the main spar.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 10 hours time-in-service after September 14, 2012, and repetitively thereafter at intervals not to exceed every 100 hours TIS, inspect as required by GippsAero Mandatory Service Bulletin SB-GA200-2012-08. If any discrepancy is found, take corrective actions before further flight following the same service bulletin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 10 hours time-in-service after September 14, 2012, and repetitively thereafter at intervals not to exceed every 100 hours TIS.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
GA200 (Pty) Ltd Models GA200 and GA200C airplanes, all serial numbers, 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 4, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.