Airworthiness Directive

AD 2012-04-10 77 FR 14681 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2012-5864
Amendment
39-16966
Published
2012-03-13
Effective
2012-04-17
Models covered
1
Last live check
2026-10-03
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AD

2012-04-10

FR doc 2012-5864 · 77 FR 14681

AD 2012-04-10Published 2012-03-13Effective 2012-04-17

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 repetitive inspections of the upper and lower main wing spar cap angles for cracks and/or corrosion and installing inspection access panels.

Full official abstract

We are adopting a new airworthiness directive (AD) for all Burl A. Rogers (type certificate previously held by William Brad Mitchell and Aeronca, Inc.) Models 15AC and S15AC airplanes. This AD was prompted by reports of intergranular exfoliation and corrosion of the upper and/or lower wing main spar cap angles found on the affected airplanes. This AD requires repetitive inspections of the upper and lower main wing spar cap angles for cracks and/or corrosion and installing inspection access panels. This AD also requires replacing the wing spar cap angles if moderate or severe corrosion is found and applying corrosion inhibitor. We are issuing this AD to correct the unsafe condition on these products.

Applies to 1 model in our index