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Airworthiness Directive

AD 2001-23-10 66 FR 58366 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-29019
Amendment
39-12507
Published
2001-11-21
Effective
2001-12-13
Models covered
3
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/2001-23-10 · 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

2001-23-10

FR doc 01-29019 · 66 FR 58366

AD 2001-23-10Published 2001-11-21Effective 2001-12-13

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 you to inspect the left-hand and right-hand flap flex shaft assemblies to determine the manufacture date.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) 33, T-34, 35, 36, 55, 56, 58, and 95 Series airplanes. This AD requires you to inspect the left-hand and right-hand flap flex shaft assemblies to determine the manufacture date. This AD also requires you to replace any flap flex shaft assemblies manufactured from January 2000 through April 2001. This AD is the result four separate reports of flap drive cable separation. The actions specified by this AD are intended to prevent separation of the flap flex shaft assembly caused by improper heat treatment. Such a condition could lead to an asymmetric flap condition, resulting in uncommanded roll of the airplane.

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Applies to 3 models in our index