AD Amdt-39-10843
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | Aircraft Company Models A200CT | Airworthiness Directives; Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C Airplanes |
Unsafe Condition
Fatigue cracking of the original design part in the main landing gear actuator clevis assembly could result in failure of the actuator clevis assembly, potentially leading to loss of control during landing operations.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the main landing gear left and right actuator clevis assembly.
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
Raytheon Aircraft Company Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C 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.