AD 2014-21-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; Pacific Aerospace Limited Airplanes |
Unsafe Condition
Cracking of the control column at the wiring access hole, which could lead to loss of control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the control column part number (P/N) 08-45031/32 for cracks within the next 50 hours time-in-service (TIS) after November 28, 2014. If any mechanical damage, deformation, or cracks are found, replace the control column with an airworthy one before further flight. If no issues are found, replace the control column at the next scheduled maintenance inspection or within the next 150 hours TIS, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 hours time-in-service (TIS) after November 28, 2014, for the initial inspection. Replacement actions have varying deadlines based on inspection results.
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Affected Aircraft
Pacific Aerospace Limited Models FU24-954 and FU24A-954 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 4, 2026
Rights: U.S. Government Public Domain
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