AD 2013-06-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; REIMS AVIATION S.A. Airplanes |
Unsafe Condition
Fretting (wear and/or chafing) found between the elevator pushrod assembly and the horizontal tail structure, which could cause the elevator pushrod to jam and could result in loss of control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the elevator pushrod assemblies, part number 6015034-1, and the horizontal tail structure. If fretting is found, or if clearance is insufficient or looseness at riveted end fittings is detected, contact REIMS AVIATION INDUSTRIES for a repair scheme and incorporate it. If bending or eccentricity of an elevator pushrod exceeds allowable limits, replace each affected elevator pushrod with a serviceable part.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 4 months after May 3, 2013
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
REIMS AVIATION S.A. Model F406 airplanes, serial numbers F406-0001 through F406-0096, 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 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.