AD Amdt-39-9380
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300-600 | Airworthiness Directives; Airbus Model A300-600 Series Airplanes |
Unsafe Condition
Cracks emanating from bolt holes in the rear spar where the main landing gear (MLG) is attached were found during full-scale fatigue testing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for cracks in bolt holes of the rear spar attached to the main landing gear (MLG), repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300-600 series airplanes
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.