Is AD 2001-18-07 a recurring Airworthiness Directive?

No — AD 2001-18-07 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2001-18-07 apply to?

AD 2001-18-07 applies to Raytheon Aircraft Company. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2001-18-07

one-time

Official AD 2001-18-07 · FR doc 01-22174 · 2001-09-06 · airframe

Airworthiness Directives; Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes

What this AD requires

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.

Which aircraft AD 2001-18-07 applies to

MakesRaytheon Aircraft Company

Applies to specific airplane(s) identified in AD paragraph (a); model/serial detail is not present in the extracted applicability text. Compliance required per Raytheon Aircraft Mandatory Service Bulletin SB 27-3397, issued January 2001.

Whether AD 2001-18-07 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of compliance — The specific action taken (inspected, replaced, modified) and to what revision.

Date — When the work was done.

Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.

Signature & certificate — The A&P/IA who returned it to service, with certificate number.

Is AD 2001-18-07 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.