Airworthiness Directive

AD 97-06-11 62 FR 12533 Active

Federal Aviation Administration · 14 CFR part 39

FR document
97-6540
Amendment
39-9968
Published
1997-03-17
Effective
1997-05-16
Models covered
1
Last live check
2026-10-03
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AD

97-06-11

FR doc 97-6540 · 62 FR 12533

AD 97-06-11Published 1997-03-17Effective 1997-05-16

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires inspecting the ruddervator differential tail control rod assembly for corrosion or cracks, repairing or replacing any cracked or corroded part, and applying anti-corrosion sealant to the ruddervator control pushrods.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) 35 series airplanes (formerly referred to as Beech 35 series airplanes). This action requires inspecting the ruddervator differential tail control rod assembly for corrosion or cracks, repairing or replacing any cracked or corroded part, and applying anti-corrosion sealant to the ruddervator control pushrods. This action results from a report of a split in the ruddervator control push rod on an affected airplane that was found during a routine inspection. The split occurred when water froze in the internal area of the control push rod and then expanded. The actions specified by this AD are intended to prevent failure of the differential tail control rod assembly, which could result in loss of control of the airplane.

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Applies to 1 model in our index