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Airworthiness Directive

AD 2009-23-03 74 FR 57567 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E9-26385
Amendment
39-16075
Published
2009-11-09
Effective
2009-12-14
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/2009-23-03 · 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.

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AD

2009-23-03

FR doc E9-26385 · 74 FR 57567

AD 2009-23-03Published 2009-11-09Effective 2009-12-14

Supersedes 2006-24-11

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 the manufacturer.

Full official abstract

We are adopting a new airworthiness directive (AD) to supersede AD 2006-24-11, which applies to certain Hawker Beechcraft Corporation (HBC) (Type Certificate previously held by Raytheon Aircraft Company) Models 1900, 1900C, and 1900D airplanes. AD 2006-24- 11 currently 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 the manufacturer. Since we issued AD 2006-24-11, the manufacturer has developed a modification kit to install on the wing rear spar lower caps that will terminate the 200-hour repetitive inspection required in AD 2006-24-11. Consequently, this AD requires installing the new modification kits on the wing rear spar lower caps and terminates the repetitive inspections required in AD 2006-24-11 when the kits are installed. We are issuing this AD to prevent fatigue cracks in the wing rear spar lower caps, which could result in fatigue failure of the wing rear spar lower caps. A rear spar failure could result in complete wing failure and the wing separating from the airplane.

More directives for Beechcraft 1900

  1. AD 2014-02-03 Airworthiness Directives; Beechcraft Corporation Airplanes 2014-01-31
  2. AD 2013-24-03 Airworthiness Directives; Beechcraft Corporation Airplanes 2013-12-09
  3. AD 2011-27-51 Airworthiness Directives; Hawker Beechcraft Corporation Models 1900, 190... 2012-01-18
  4. AD 2009-23-01 Airworthiness Directives; Hawker Beechcraft Corporation Model 1900, 1900... 2009-11-03
  5. AD 2006-24-11 Airworthiness Directives; Raytheon Aircraft Company Models 1900, 1900C, ... 2006-12-04

All Beechcraft 1900 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index