94-18-04 R1
FR doc 95-6058 · 60 FR 13624AD 94-18-04 R1Published 1995-03-14Effective 1995-03-24
Superseded by 2003-21-01
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 Univair Aircraft Corporation (Univair) Models Ercoupe 415-C, 415-CD, 415-D, 415-E, and 415-G, Forney F-1 and F-1A, Alon A-2 and A-2A, and Mooney M10 airplanes: installing inspection openings in the outer…
Full official abstract
This amendment revises Airworthiness Directive (AD) 94-18-04, which currently requires the following on Univair Aircraft Corporation (Univair) Models Ercoupe 415-C, 415-CD, 415-D, 415-E, and 415-G, Forney F-1 and F-1A, Alon A-2 and A-2A, and Mooney M10 airplanes: installing inspection openings in the outer wing panels, inspecting (one-time) the wing outer panel structural components for corrosion, and repairing any corroded wing outer panel structural component. Several reports of corrosion in the outer wing panels of the affected airplanes prompted that AD. This action incorporates a revision to the service information to include procedures that the Federal Aviation Administration (FAA) has determined are necessary for installing future outer wing panel inspection openings. The actions [[Page 13625]] specified by this AD are intended to prevent wing damage caused by a corroded wing outer panel structural component, which, if not detected and corrected, could progress to the point of structural failure.