Airworthiness Directive

AD 96-21-05 61 FR 54538 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-26705
Amendment
39-9782
Published
1996-10-21
Effective
1996-11-29
Models covered
1
Last live check
2026-10-03
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AD

96-21-05

FR doc 96-26705 · 61 FR 54538

AD 96-21-05Published 1996-10-21Effective 1996-11-29

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 drilling inspection access holes in the elevator torque tube arm, inspecting the elevator torque tube for corrosion, replacing any corroded elevator torque tube, and applying a corrosion preventive compound.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Fairchild Aircraft SA226 and SA227 series airplanes that do not have a certain elevator torque tube installed. This action requires drilling inspection access holes in the elevator torque tube arm, inspecting the elevator torque tube for corrosion, replacing any corroded elevator torque tube, and applying a corrosion preventive compound. Several reports of corrosion found in the elevator torque tube area on the affected airplanes prompted this action. The actions specified by this AD are intended to prevent failure of the flight control system caused by a corroded elevator torque tube, which could result in loss of control of the airplane.

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All Fairchild SA226/SA227 Metro directives

Applies to 1 model in our index