FAA airworthiness directive publication

AD 2006-23-02

2006-12-21 · Correction notice · Federal Register document E6-21748

This page records a selected historical publication. Its current legal status, applicability to an individual aircraft and compliance have not been determined. Consult the current FAA directive and aircraft configuration and maintenance records.

This correction remains a separate publication; it is not presented as a newly issued independent directive.

What this historical correction says

Source publication 2006-12-21 · Document E6-21748.

The notice publishes only a correction fragment. The summary or discussion below is not a complete applicability clause or a complete model list.

Correction of Publication

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Accordingly, the publication of November 8, 2006 (71 FR 65390), of 
Amendment 39-14814; AD 2006-23-02, which was the subject of FR Doc. E6-
18727, is corrected as follows:


Section 39.13  [Corrected]

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On page 65391, in section 39.13 [Amended], in paragraph (e), change the 
text to read: ``To address this problem, you must do the following, 
unless already done:''
    Action is taken herein to correct this reference in AD 2006-23-02 
and to add this AD correction to section 39.13 of the Federal Aviation 
Regulations (14 CFR 39.13).
    The effective date remains December 13, 2006.

Original date wording

DATES: The effective date of this AD (2006-23-02) remains December 13, 
2006.

Dates describing the correction and the original rule remain separate as written.

Original summary or discussion context

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2006-23-02, which was published in the Federal Register on 
November 8, 2006 (71 FR 65390), and applies to certain Raytheon 
Aircraft Company (RAC) (formerly Beech) Models C90A, B200, B200C, B300, 
and B300C airplanes. AD 2006-23-02 requires you to inspect the flight 
controls for improper assembly or damage, and if any improperly 
assembled or damaged flight controls are found, take corrective action. 
We proposed in the notice of proposed rulemaking (NPRM) ``unless 
already done'' credit if the actions were already accomplished. 
However, we inadvertently left that language out of paragraph (e) of AD 
2006-23-02. This document corrects that paragraph by inserting the 
phrase ``unless already done.''

Literal source labels for discovery: C90A, B200, B200C, B300, B300C. Labels remain as written; series, aliases and engine suffixes are not expanded.

Dated original publication

AD 2006-23-02 · 2006-11-08 · document E6-18727

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2006-23-02, which was published in the Federal Register on 
November 8, 2006 (71 FR 65390), and applies to certain Raytheon 
Aircraft Company (RAC) (formerly Beech) Models C90A, B200, B200C, B300, 
and B300C airplanes. AD 2006-23-02 requires you to inspect the flight 
controls for improper assembly or damage, and if any improperly 
assembled or damaged flight controls are found, take corrective action. 
We proposed in the notice of proposed rulemaking (NPRM) ``unless 
already done'' credit if the actions were already accomplished. 
However, we inadvertently left that language out of paragraph (e) of AD 
2006-23-02. This document corrects that paragraph by inserting the 
phrase ``unless already done.''

Each link opens a separate dated source. These words and dates do not determine which directive controls today, aircraft applicability, installed configuration or compliance. No corrected rule body has been merged.

Historical relationship observation unknown

This correction notice is a separate source edition and was not interpreted as a new rule. This does not establish that there are no related or currently applicable directives.

Earlier extraction record

The earlier extraction kept these fields unknown. Its original record is preserved below. Newly retained correction excerpts are shown above; applicability and compliance remain undetermined.

Applicability text in this publication

An applicability clause was not extracted from this publication. Applicability remains undetermined.

Effective-date text

An effective-date observation was not extracted from this publication.

Publication context

A relationship to prior directives has not been established from this publication.

Official sources

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This selected source edition is not a complete list of current airworthiness directives. Referenced manufacturer service documents are not reproduced here.