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Airworthiness Directive

AD 2003-01-01 68 FR 997 Active

Federal Aviation Administration · 14 CFR part 39

FR document
03-148
Amendment
39-13012
Published
2003-01-08
Effective
2003-02-27
Models covered
2
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/2003-01-01 · 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

2003-01-01

FR doc 03-148 · 68 FR 997

AD 2003-01-01Published 2003-01-08Effective 2003-02-27

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.

1 correction to this AD FAA · 2003-01-27

Correction published 2003-01-27

Issued by
Federal Aviation Administration
Published
2003-01-27
Document
Federal Register 03-1674 · Final rule; correction
Corrects
the version published January 8, 2003 at 68 FR 997

This document makes a correction to Airworthiness Directive (AD) 2003-01-01, which was published in the Federal Register on January 8, 2003 (68 FR 997), and applies to certain Raytheon Aircraft Company (Raytheon) Beech Models 36, A36, A36TC, B36TC, 58, and 58A airplanes. We inadvertently omitted certain regulatory text to remove AD 2000-26- 16, Amendment 39-12066, from 14 CFR part 39. This action corrects the regulatory text.

A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.

Source: Federal Register document 03-1674, retrieved 2026-08-16

Read this correction on Federal Register (opens in a new tab)
Full official abstract

This amendment supersedes Airworthiness Directive (AD) 2000- 26-16, which applies to certain Raytheon Aircraft Company (Raytheon) Beech Models A36, B36TC, and 58 airplanes. AD 2000-26-16 requires you to inspect for missing rivets on the right hand side of the fuselage and, if necessary, install rivets. AD 2000-26-16 resulted from Raytheon identifying several instances of missing rivets on these airplanes. AD 2000-26-16 incorporated an incorrect listing of serial numbers for the affected model airplanes and omitted certain airplane models from the applicability section of AD 2000-26-16. This AD retains the actions required in AD 2000-26-16 and corrects the applicability section. The actions specified by this AD are intended to detect and correct 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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View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 2 models in our index