AD 2014-21-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | Aircraft Company | Airworthiness Directives; Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) Airplanes |
| aircraft | Beechcraft | Corporation | Airworthiness Directives; Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) Airplanes |
Unsafe Condition
Failure of the Acme nut threads in a pitch trim actuator (PTA).
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect to determine if PTAs with specific serial number and part number are installed. Replace PTAs if installed. Perform repetitive replacements of PTAs with new PTAs or certain overhauled PTAs.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 200 flight hours or 6 months after the effective date, whichever occurs first.
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Affected Aircraft
Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) Model 400, 400A, 400T, and MU-300 airplanes, with specific serial number ranges.
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
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