AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2007-12-06 72 FR 31988 Active

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.

Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
E7-10758
Amendment
39-15084
Published
2007-06-11
Effective
2007-07-16
Models covered
3

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2007-12-06 · 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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2007-12-06

FR doc E7-10758 · 72 FR 31988

AD 2007-12-06Published 2007-06-11Effective 2007-07-16

Supersedes 2006-23-02

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.

Full official abstract

We are adopting a new airworthiness directive (AD) that supersedes AD 2006-23-02, which applies to certain Hawker Beechcraft Corporation (HBC) (Type Certificate (TC) No. 3A20 and TC No. A24CE formerly held by Raytheon Aircraft Corporation and Beech) Models C90A, B200, B200C, B300, and B300C airplanes. AD 2006-23-02 currently 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. Since we issued AD 2006-23-02, we have determined the need to add airplane serial numbers that were not previously included in the applicability. Consequently, this AD retains the actions of AD 2006-23-02 and adds airplane serial numbers to the applicability. 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.

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

  1. AD 2025-20-11 Airworthiness Directives; Textron Aviation Inc. Airplanes Effective 2025-10-17
  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 2006-23-02 Airworthiness Directives; Raytheon Aircraft Company Models C90A, B200, B... Effective 2006-12-13
  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

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 3 models in our index