AD Amdt-39-10446
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A340 | Airworthiness Directives; Airbus Model A340 Series Airplanes |
Unsafe Condition
Fatigue cracking of the vertical support beam at the upper first fastener row of the actuator attachment fitting of the center landing gear (CLG).
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct a rototest inspection for fatigue cracking of the vertical support beam. Perform follow-on actions as specified.
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 A340 series airplanes as specified in the AD.
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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