Airworthiness Directive 2018-08-01
one-timeAirworthiness Directives; Airbus Helicopters
What this AD requires
We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model EC225LP helicopters. This AD requires inspecting each main rotor rotating swashplate (swashplate) control rod attachment yoke (yoke). This AD is prompted by a finding that the yoke is susceptible to cracking. The actions of this AD are intended to address an unsafe condition on these products.
Which aircraft AD 2018-08-01 applies to
Applies only to helicopters with an M/R rotating swashplate P/N 332A31-3074-00 or 332A31-3074-01 with a serial number listed in Appendix 4.A of Airbus Helicopters EASB 05A051, Revision 1, dated November 16, 2017, installed.
Whether AD 2018-08-01 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:
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.