Airworthiness Directive

AD 2006-23-02 71 FR 65389 Superseded

Federal Aviation Administration · 14 CFR part 39

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.

FR document
E6-18727
Amendment
39-14814
Published
2006-11-08
Effective
2006-12-13
Models covered
3

Last live check: 2026-08-19

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.
AD

2006-23-02

FR doc E6-18727 · 71 FR 65389

AD 2006-23-02Published 2006-11-08Effective 2006-12-13

Superseded by 2007-12-06

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 the flight controls for improper assembly or damage, and if any improperly assembled or damaged flight controls are found, take corrective action.

1 correction to this AD FAA · 2006-12-21

Correction published 2006-12-21

Issued by
Federal Aviation Administration
Published
2006-12-21
Document
Federal Register E6-21748 · Final rule; correction
Corrects
the version published November 8, 2006 at 71 FR 65390

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."

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 E6-21748, retrieved 2026-08-17

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain Raytheon Aircraft Company (RAC) (formerly Beech) Models C90A, B200, B200C, B300, and B300C airplanes. This AD 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. This AD results from a report of inspections of several affected airplanes with improperly assembled or damaged flight controls. We are issuing this AD to detect and correct improperly assembled or damaged flight controls, which could result in an unsafe condition by reducing capabilities of the flight controls and lead to loss of control of the airplane.

More directives for Beechcraft King Air 200 (Super King Air)

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  2. AD 2010-26-03 Airworthiness Directives; Hawker Beechcraft Corporation Models B200, B20... Effective 2010-12-20
  3. AD 2008-07-10 Airworthiness Directives; Hawker Beechcraft Corporation Models B200, B20... Effective 2008-04-10
  4. AD 2007-12-06 Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificat... Effective 2007-07-16
  5. AD 98-20-38 R1 Airworthiness Directives; Raytheon Aircraft Company (Raytheon) Beech 200... Effective 2005-02-18

All Beechcraft King Air 200 (Super King Air) directives

Applies to 3 models in our index