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Airworthiness Directive

AD 2001-18-07 66 FR 46515 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-22174
Amendment
39-12433
Published
2001-09-06
Effective
2001-10-12
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/2001-18-07 · 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

2001-18-07

FR doc 01-22174 · 66 FR 46515

AD 2001-18-07Published 2001-09-06Effective 2001-10-12

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 all four flap flexible shaft assemblies for the correct diagonal wrap and the correct installation.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Beech Models 1900, 1900C, and 1900D airplanes. This AD requires you to inspect all four flap flexible shaft assemblies for the correct diagonal wrap and the correct installation. This AD also requires you to replace any flap flexible shaft assembly that has an incorrect diagonal wrap or incorrect installation. This AD is the result of several occurrences of flap extension/retraction failures on the affected airplanes due to the inner flexible shaft ends separating or disengaging. The actions specified by this AD are intended to prevent these flap extension/ retraction failures due to incorrectly configured flap flexible shaft assemblies. Such failure could result in an asymmetric flap condition during flight if the flap safety switch fails to function properly.

More directives for Beechcraft 1900

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  3. AD 2011-27-51 Airworthiness Directives; Hawker Beechcraft Corporation Models 1900, 190... 2012-01-18
  4. AD 2009-23-03 Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificat... 2009-11-09
  5. AD 2009-23-01 Airworthiness Directives; Hawker Beechcraft Corporation Model 1900, 1900... 2009-11-03

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