AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2006-24-11 71 FR 70297 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires you to repetitively inspect the forward, vertical, and aft flanges of both the left and right wing rear spar lower caps for cracks, repair any cracks found, and report the inspection results to RAC.

Superseded by AD 2009-23-03Federal Register (opens in a new tab)

FR document
E6-20326
Amendment
39-14840
Published
2006-12-04
Effective
2006-12-11
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/2006-24-11 · 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

2006-24-11

FR doc E6-20326 · 71 FR 70297

AD 2006-24-11Published 2006-12-04Effective 2006-12-11

Superseded by 2009-23-03

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 repetitively inspect the forward, vertical, and aft flanges of both the left and right wing rear spar lower caps for cracks, repair any cracks found, and report the inspection results to RAC.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Raytheon Aircraft Company (RAC) Models 1900, 1900C, and 1900D airplanes. This AD requires you to repetitively inspect the forward, vertical, and aft flanges of both the left and right wing rear spar lower caps for cracks, repair any cracks found, and report the inspection results to RAC. This AD results from additional fatigue cracks found in this area since inspections were performed to comply with Emergency AD 2006-18-51, which required immediate visual inspections of this area. We are issuing this AD for the purpose of performing a more rigorous inspection requiring cleaning and paint stripping of this section of the wing rear spar to detect and correct cracking in the wing spar lower caps of the affected airplanes before the cracks lead to failure. These wing rear spar cracks may result in wing failure which could result in the wing separating from the airplane with consequent loss of control.

More directives for Beechcraft 1900

  1. AD 2014-02-03 Airworthiness Directives; Beechcraft Corporation Airplanes Effective 2014-03-07
  2. AD 2013-24-03 Airworthiness Directives; Beechcraft Corporation Airplanes Effective 2014-01-13
  3. AD 2011-27-51 Airworthiness Directives; Hawker Beechcraft Corporation Models 1900, 190... Effective 2012-01-18
  4. AD 2009-23-03 Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificat... Effective 2009-12-14
  5. AD 2009-23-01 Airworthiness Directives; Hawker Beechcraft Corporation Model 1900, 1900... Effective 2009-12-08

All Beechcraft 1900 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2006-24-11 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index