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Airworthiness Directive

AD 94-18-04 R1 60 FR 13624 Superseded

Federal Aviation Administration · 14 CFR part 39

Superseded by AD 2003-21-01Federal Register (opens in a new tab)

FR document
95-6058
Amendment
39-9173
Published
1995-03-14
Effective
1995-03-24
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/94-18-04%20R1 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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AD

94-18-04 R1

FR doc 95-6058 · 60 FR 13624

AD 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Superseded by 2003-21-01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.

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 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.

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.

More directives for ERCO/Forney/Alon Ercoupe 415

  1. AD 2012-08-06 Airworthiness Directives; Univair Aircraft Corporation Airplanes Effective 2012-10-03
  2. AD 2003-21-01 Airworthiness Directives; Univair Aircraft Corporation Models Alon A-2 a... Effective 2003-12-01
  3. AD 2002-26-02 Airworthiness Directives; Univair Aircraft Corporation Models Alon A-2 a... Effective 2003-02-14
  4. AD 2002-16-04 Airworthiness Directives; Univair Aircraft Corporation Models (ERCO) 415... Effective 2002-09-13

All ERCO/Forney/Alon Ercoupe 415 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 94-18-04 R1 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index