Airworthiness Directive 2020-24-07

one-time
Official AD 2020-24-07 · FR doc 2020-26867 · 2020-12-08 · airframe

Airworthiness Directives; Airbus Helicopters

What this AD requires

The FAA is superseding Airworthiness Directive (AD) 2018-26-02 for Airbus Helicopters (previously Eurocopter France) Model AS350B3, EC130B4, and EC130T2 helicopters. AD 2018-26-02 required inspecting the pilot's and co-pilot's throttle twist for proper operation. This new AD retains the requirements of AD 2018-26-02 and adds calendar time compliance times for the required actions. This AD was prompted by a public comment that prompted additional review. The actions of this AD are intended to address an unsafe condition on these products.

Which aircraft AD 2020-24-07 applies to

MakesAirbus Helicopters
ModelsAS350B3, EC130B4, EC130T2, AS350, EC130

AS350B3: applies with an ARRIEL 2B1 engine (two-channel FADEC) and new twist grip MOD 073254, OR with an ARRIEL 2D engine installed. EC130B4: applies with an ARRIEL 2B1 engine (two-channel FADEC) and new twist grip MOD 073773 installed. EC130T2: applies with an ARRIEL 2D engine installed. Replaces AD 2018-26-02.

Whether AD 2020-24-07 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 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 2020-24-07 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.