Airworthiness Directive

AD 97-10-13 Amendment 39-10025

Federal Aviation Administration · 14 CFR part 39

FR document
97-12517
Amendment
39-10025
Published
1997-05-13
Models covered
1
Last live check
Not yet re-verified
AD

97-10-13

FR doc 97-12517

AD 97-10-13Published 1997-05-13Effective 1997-07-08

Supersedes 96-21-05

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

Requires the following on certain Fairchild Aircraft, Inc.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 96-21- 05, which currently requires the following on certain Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes that do not have a certain elevator torque tube installed: 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. AD 96-21-05 resulted from several reports of corrosion found in the elevator torque tube area on the affected airplanes. This AD retains the actions required by AD 96- 21-05, and adds certain Fairchild Model SA227-BC airplanes to the Applicability section of that AD. 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.

Applies to 1 model in our index