Is AD 2001-23-05 a recurring Airworthiness Directive?

No — AD 2001-23-05 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2001-23-05 apply to?

AD 2001-23-05 applies to Socata. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2001-23-05

one-time

Official AD 2001-23-05 · FR doc 01-28419 · 2001-11-19 · airframe

Airworthiness Directives; SOCATA-Groupe Aerospatiale Models TB 9, TB 10, TB 20, TB 21, and TB 200 Airplanes

What this AD requires

This amendment adopts a new airworthiness directive (AD) that applies to all SOCATA--Groupe Aerospatiale (SOCATA) Models TB 9, TB 10, TB 20, TB 21, and TB 200 airplanes that do not have factory Modification 165, any edition, incorporated on the front seats. This AD requires you to modify the front seats that have solid metal seat pans. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to eliminate the potential for the front seats to inadvertently unlock from their fixed positions. Such uncontrolled movement could prevent the pilot from making the necessary flight maneuvers to control the airplane.

Which aircraft AD 2001-23-05 applies to

MakesSocata

Applies to specific airplane(s) identified in AD paragraph (a); model/serial detail is not present in the extracted applicability text. Compliance required per SOCATA Service Bulletin SB-10-115-25, dated December 2000.

Whether AD 2001-23-05 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 2001-23-05 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.