Airworthiness Directive 2000-15-19

one-time
Official AD 2000-15-19 · FR doc 00-20183 · 2000-08-09 · airframe

Airworthiness Directives; Eurocopter France Model SA-365N, N1, and AS-365N2, N3 Helicopters

What this AD requires

This amendment adopts a new airworthiness directive (AD) for Eurocopter France Model SA-365N, N1, and AS-365N2, N3 helicopters. This action requires inspecting the sand filter ejection nozzle (nozzle) for cracks and replacing any cracked nozzle. This amendment is prompted by the discovery of a cracked nozzle during a preflight inspection. This condition, if not corrected, could result in loss of the nozzle in flight, impact with the main or tail rotor, and a subsequent forced landing.

Which aircraft AD 2000-15-19 applies to

ModelsAS365

Daily visual inspection of left-hand and right-hand sand filter ejection nozzles for cracks, per Eurocopter AS 365 Service Bulletin No. 71.00.14; also addressed by DGAC (France) AD No. 2000-108-050(A).

Whether AD 2000-15-19 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 2000-15-19 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.