FAA airworthiness directive publication
AD 2006-23-02
2006-11-08 · Final rule publication · Federal Register document E6-18727
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.
Later correction publications citing this dated source
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- AD 2006-23-02 · 2006-12-21 · document E6-21748
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 model wording
Source publication: 2006-11-08 · Document E6-18727. Observation edition: selected-ad-source-text-extension-2.0.0.
These are exact source labels for discovery. Manufacturer identity remains unresolved. Serial numbers, installed equipment and all other conditions have not been evaluated. The complete applicability clause below retains all conditions and notes.
Original model and serial-number table
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Model Serial Nos.
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C90A........................... LJ-1697 through LJ-1726, LJ-1728, LJ-
1729, and LJ-1731 through LJ-1739.
B200........................... BB-1827 through BB-1912.
B200C.......................... BL-148 and BL-149.
B300........................... FL-379 through FL-423, FL-426, FL-428
through FL-450, and FL-452.
B300C.......................... FM-11.
------------------------------------------------------------------------
Rows and serial-number conditions are reproduced as written; they are not an aircraft configuration or applicability determination.
C90A
B200
B200C
B300
B300C
These observations do not determine aircraft applicability, compliance, installed configuration or current legal status.
Applicability text in this publication
Applicability
(c) This AD affects the following airplane models and serial
numbers that are certificated in any category:
------------------------------------------------------------------------
Model Serial Nos.
------------------------------------------------------------------------
C90A........................... LJ-1697 through LJ-1726, LJ-1728, LJ-
1729, and LJ-1731 through LJ-1739.
B200........................... BB-1827 through BB-1912.
B200C.......................... BL-148 and BL-149.
B300........................... FL-379 through FL-423, FL-426, FL-428
through FL-450, and FL-452.
B300C.......................... FM-11.
------------------------------------------------------------------------
[[Page 65391]]
Effective-date text
This AD becomes effective on December 13, 2006.
Publication context
Historical effective date recorded in the publication: 2006-12-13. This date does not establish which directive controls today.
The publication records no affected prior directives in its Affected ADs paragraph. This says nothing about the number of directives applicable to an aircraft.
Affected ADs
(b) None.
Official sources
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Sources retrieved: HTML 2026-09-08; PDF 2026-09-08.
The displayed text comes from the HTML publication. Refer to the official documents for the original wording.
This selected source edition is not a complete list of current airworthiness directives. Referenced manufacturer service documents are not reproduced here.