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Airworthiness Directive

AD 96-04-08 61 FR 6934 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-3886
Amendment
39-9520
Published
1996-02-23
Effective
1996-04-12
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/96-04-08 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

96-04-08

FR doc 96-3886 · 61 FR 6934

AD 96-04-08Published 1996-02-23Effective 1996-04-12

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 replacing the main landing gear legs.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to Air Tractor, Incorporated (Air Tractor) Models AT-802 and AT-802A airplanes. This action requires repetitively replacing the main landing gear legs. Failure of the main landing gear legs on an AT-802A prompted this action. The actions specified by this AD are intended to prevent possible failure of the main landing gear legs, which, if not detected and corrected, could result in loss of control of the airplane during landing operations.

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All Air Tractor AT-Series directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index