Airworthiness Directive 2013-19-19

one-time
Official AD 2013-19-19 · FR doc 2013-23580 · 2013-10-01 · airframe

Airworthiness Directives; Eurocopter France (Eurocopter) Helicopters

What this AD requires

We are adopting a new airworthiness directive (AD) for Eurocopter Model AS332C, AS332L, AS332L1, AS332L2, and EC225LP helicopters. This AD requires replacing certain serial-numbered main gearbox (MGB) bevel gear vertical shafts because they are no longer airworthy. Also, this AD requires certain inspections of each MGB bevel gear vertical shaft (shaft) for a crack. Also, this AD requires if there is a crack, replacing the shaft with an airworthy part before further flight. This AD is prompted by two incidents of emergency ditching after warning indications of loss of MGB oil pressure. These actions are intended to detect a cracked shaft, which could result in loss of MGB oil pressure, loss of the MGB lubrication system, and subsequent loss of control of the helicopter.

Which aircraft AD 2013-19-19 applies to

ModelsAS332C, AS332L, AS332L1, AS332L2, EC225LP, AS332, EC225
Part-conditional332A32-5101-00, 332A32-5101-05, 332A32-5101-10, 332A32-5101-15.

Applies only to helicopters with main gearbox (MGB) bevel gear vertical shaft P/N 332A32-5101-00, -05, -10, or -15 installed.

Whether AD 2013-19-19 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 2013-19-19 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.