Is AD 2010-06-07 a recurring Airworthiness Directive?

No — AD 2010-06-07 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 2010-06-07

Q: Which aircraft does AD 2010-06-07 apply to?

AD 2010-06-07 applies to Eurocopter — models AS332C, AS332L, AS332L1, AS332L2, AS350B3, AS355F, AS355F1, AS355F2. Serial/part conditions may narrow it to specific aircraft.

one-time

Official AD 2010-06-07 · FR doc 2010-5288 · 2010-03-17 · airframe

Airworthiness Directives; Eurocopter France Model AS 332 C, L, L1, and L2; AS 350 B3; AS355 F, F1, F2, and N; SA 365N and N1; AS 365 N2 and N3; SA 366G1; EC 130 B4; and EC 155B and B1 Helicopters

What this AD requires

We are adopting a new airworthiness directive (AD) for the specified 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 the AD is issued following a manufacturing nonconformity found on one batch of the servo-control caps. With a defective servo-control, rotation of the distributor might not be stopped mechanically since only friction of inner seals holds the distributor sleeve in its position. The AD actions are intended to address the unsafe condition created by a manufacturing nonconformity found on one batch of servo-control caps. If not corrected this condition could cause untimely movements of servo-controls, which are used on main and anti-torque rotors, and lead to the loss of control of the helicopter.

Which aircraft AD 2010-06-07 applies to

MakesEurocopter

ModelsAS332C, AS332L, AS332L1, AS332L2, AS350B3, AS355F, AS355F1, AS355F2, AS355N, SA365N, SA365N1, AS365N2, AS365N3, SA366G1, EC130B4, EC155B, EC155B1, AS332, AS350, AS355, SA365, AS365, SA366, EC130, EC155

Whether AD 2010-06-07 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 2010-06-07 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.