Airworthiness Directive 2024-01-11

one-time
Official AD 2024-01-11 · FR doc 2024-01932 · 2024-01-31 · appliance

Airworthiness Directives; Various Helicopters

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for all helicopters with certain Pacific Scientific Company rotary buckle assemblies (buckles) installed. This AD was prompted by a report of a manufacturing defect in the screws used inside the buckle. This AD requires inspecting the buckle screws and, depending on the results, reidentifying the buckle, replacing the screws and reidentifying the buckle, or replacing the buckle. This AD also prohibits installing certain buckles. The FAA is issuing this AD to address the unsafe condition on these products.

Which aircraft AD 2024-01-11 applies to

MakesPacific Scientific Company
Applies to all models of the make above.
Part-conditional1111475, 1111548-01.

Applies to all helicopters, certificated in any category, with a restraint system having a Pacific Scientific Company rotary buckle assembly P/N 1111475 (all dash numbers) or P/N 1111548-01 installed, manufactured between January 2012 and September 2012 inclusive, or with an unknown date of manufacture. These buckles may be installed on, but are not limited to, Airbus Helicopters model helicopters.

Whether AD 2024-01-11 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 2024-01-11 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.