Airworthiness Directive

AD 97-07-10 62 FR 15373 Active

Federal Aviation Administration · 14 CFR part 39

FR document
97-8249
Amendment
39-9984
Published
1997-04-01
Effective
1997-05-23
Models covered
1
Last live check
2026-09-30
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AD

97-07-10

FR doc 97-8249 · 62 FR 15373

AD 97-07-10Published 1997-04-01Effective 1997-05-23

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 wing struts for cracks or damage (chafing, etc.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to de Havilland DHC-6 series airplanes that do not have a certain wing strut modification (Modification 6/1581) incorporated. This action requires inspecting the wing struts for cracks or damage (chafing, etc.), replacing wing struts that are found damaged beyond certain limits or are found cracked, and incorporating Modification No. 6/1581 to prevent future chafing damage. This AD results from several reports of wing strut damage caused by the upper fairing rubbing against the wing strut. The actions specified by this AD are intended to prevent failure of the wing struts, which could result in loss of control of the airplane.

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All de Havilland DHC-6 Twin Otter directives

Applies to 1 model in our index