AD 2003-01-01

Airworthiness directive · Right hand fuselage panel assembly · Textron 36, 58, 58A and 3 more

Effective
February 27, 2003
Published
January 8, 2003 · 68 FR 997–999
Issued
December 30, 2002
Supersedes
AD2000-26-16
Models
36, 58, 58A, A36, A36TC, B36TC
Data sheets
TCDS3A15TCDS3A16
Registered aircraft
3,862 matched by model
Product
Aircraft · Small airplane
Amendment
39-13012
Docket
2002-CE-07-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document 03-148. Only the govinfo PDF is the legal edition. DRS record last changed January 21, 2026.

On this page

Summary

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.

The airworthiness directive

2003-01-01 Raytheon Aircraft Company: Amendment 39-13012; Docket No. 2002-CE-07-AD; Supersedes AD 2000-26-16, Amendment 39-12066.”

Action is taken herein to correct this reference in AD 2003-01-01 and to add this AD correction to section 39.13 of the Federal Aviation Regulations (14 CFR 39.13).

The effective date remains February 27, 2003.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

Effective datePage 1

The effective date of this AD remains February 27, 2003.

For further information contactPage 1

T.N. Baktha, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Wichita, Kansas 67209; telephone: (316) 946-4155; facsimile: (316) 946-4407.

DiscussionPage 1

On December 30, 2002, FAA issued AD 2003-01-01, Amendment 39-13012 (68 FR 997, January 8, 2003), which applies to certain Raytheon Beech Models 36, A36, A36TC, B36TC, 58, and 58A airplanes. This AD retains the actions required in AD 2000-26-16 and adds additional airplane models to the applicability section of this AD.

Need for the CorrectionPage 1

The FAA inadvertently omitted certain regulatory text to remove AD 2000-26-16, Amendment 39-12066 (66 FR 1253, January 8, 2001) from 14 CFR part 39. This regulatory text is needed to ensure that the affected airplane owners/operators do not have unnecessary action performed on their airplanes.

Adoption of the amendmentPage 1

Accordingly, the publication of January 8, 2003 (68 FR 997), of Amendment 39-13012; AD 2003-01-01, which was the subject of FR Doc. 03-148, is corrected as follows:

On page 998, in section 39.13 [Amended], 2., replace the current paragraph with the following text: “FAA amends § 39.13 by removing Airworthiness Directive (AD) 2000-26-16, Amendment 39-12066 (66 FR 1253, January 8, 2001), and by adding a new AD to read as follows:

Affected TCDS · 2

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 3,862

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Beech3,143 aircraft
  • Raytheon718 aircraft
  • Beech/Goedkerj L1 aircraft
By year built
19682007
Registered aircraft by year built: 3,391 aircraft
196877
196931
197051
197138
197278
1973109
1974108
1975143
1976129
1977192
1978192
1979204
1980211
1981190
1982116
198396
1984112
198582
198643
198750
198864
198944
199075
199182
199252
199371
199497
199568
199658
199795
199887
199992
200087
200187
200238
20039
200423
20059
20071

471 with no year recorded

By model

Aircraft

See all 3,862 aircraft