Airworthiness Directive 2010-10-15

one-time
Official AD 2010-10-15 · FR doc 2010-11420 · 2010-05-21 · airframe

Airworthiness Directives; Eurocopter France (ECF) Model AS332L1 and AS332L2 Helicopters

What this AD requires

We are adopting a new airworthiness directive (AD) for the specified ECF model helicopters. This AD results from a mandatory continuing airworthiness information (MCAI) AD issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The MCAI AD states that with certain pilot and copilot seats in the rear high position and seat backrest fully tilted the seat shoulder harness could become jammed between the seat and bulkhead. This condition, if not corrected, could result in the shoulder harness binding and causing the inertial reel to malfunction and no longer retain the flight crew member in the seat in the event of an emergency or hard landing.

Which aircraft AD 2010-10-15 applies to

ModelsAS332L1, AS332L2, AS332
Part-conditional332P76-9012-02, 332P76-9012-03.

Applies only to helicopters with customized 'rails with the rear stop moved aft' rail assemblies P/N 332P76-9012-02 or -03 installed, without MOD 332V080210.00.

Whether AD 2010-10-15 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2010-10-15 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.