AD Amdt-39-17294
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; GA200 (Pty) Ltd Airplanes |
Unsafe Condition
Failure of the wing strut bolt through the main spar.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the inboard strut fitting within 10 hours time-in-service after September 14, 2012, following GippsAero Mandatory Service Bulletin SB-GA200-2012-08, Issue 2. Repeat inspections at intervals not to exceed 500 hours time-in-service following the same bulletin. If discrepancies are found, take corrective action as specified in the revised 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, for the initial inspection. Repetitive inspections due at intervals not to exceed 500 hours time-in-service.
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 6, 2026
Rights: U.S. Government Public Domain
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