Airworthiness Directive 2016-25-19
one-timeAirworthiness Directives; Airbus Helicopters (Previously Eurocopter France) Helicopters
What this AD requires
We are superseding airworthiness directive (AD) 2010-21-07 for Eurocopter France (now Airbus Helicopters) Model AS350B3 and EC130B4 helicopters. AD 2010-21-07 required inspecting the pilot's and co- pilot's throttle twist for proper operation of the contactors. This new AD retains the requirements of AD 2010-21-07, includes additional inspection procedures, and revises the inspection interval. These actions are intended to address the unsafe condition on these products.
Which aircraft AD 2016-25-19 applies to
Applies only to helicopters with the Arriel 2B1 engine equipped with two-channel FADEC and with new twist grip modification (MOD) 073254 installed (AS350B3) or MOD 073773 installed (EC130B4).
Whether AD 2016-25-19 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:
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.