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Airworthiness Directive

AD 99-26-19 64 FR 72524 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires repetitively inspecting the wing lift struts for dents and corrosion and the wing lift strut forks for cracks; replacing any strut found with corrosion or dents, or forks with cracks; and repetitively replacing the wing…

Revised by AD 99-26-19 R1Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
99-33166
Amendment
39-11479
Published
1999-12-28
Effective
2000-02-14
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/99-26-19 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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AD

99-26-19

FR doc 99-33166 · 64 FR 72524

AD 99-26-19Published 1999-12-28Effective 2000-02-14

Revised by 99-26-19 R1

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 repetitively inspecting the wing lift struts for dents and corrosion and the wing lift strut forks for cracks; replacing any strut found with corrosion or dents, or forks with cracks; and repetitively replacing the wing lift strut forks.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain The New Piper Aircraft, Inc. (Piper) J-2 series airplanes equipped with wing lift struts. This AD requires repetitively inspecting the wing lift struts for dents and corrosion and the wing lift strut forks for cracks; replacing any strut found with corrosion or dents, or forks with cracks; and repetitively replacing the wing lift strut forks. This AD also requires incorporating a ``NO STEP'' placard on the lift strut. This AD is the result of the Federal Aviation Administration (FAA) inadvertently omitting the J-2 series airplanes from the applicability of AD 99-01-05. The actions specified by this AD are intended to prevent in-flight separation of the wing from the airplane caused by wing lift struts with dents or corrosion or wing lift forks with cracks, which could result in loss of control of the airplane.

More directives for Piper J-2 Cub

  1. AD 99-26-19 R1 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2014-01-21

All Piper J-2 Cub directives

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Applies to 1 model in our index