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Airworthiness Directive

AD 2000-26-16 66 FR 1253 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-183
Amendment
39-12066
Published
2001-01-08
Effective
2001-02-16
Models covered
2
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/2000-26-16 · 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

2000-26-16

FR doc 01-183 · 66 FR 1253

AD 2000-26-16Published 2001-01-08Effective 2001-02-16

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 for missing rivets on the right hand side of the fuselage and, if necessary, install rivets.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Beech Models A36, B36TC, and 58 airplanes. This AD requires you to inspect for missing rivets on the right hand side of the fuselage and, if necessary, install rivets. Raytheon has identified several instances of missing rivets on these airplanes. The actions specified by this AD are intended to install missing rivets in the right hand fuselage panel assembly in the area above the right wing and below the cabin door threshold. These rivets must be present for the fuselage to carry the ultimate load and prevent critical structural failure with loss of airplane control.

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Applies to 2 models in our index