Is AD E6-15422 a recurring Airworthiness Directive?

No — AD E6-15422 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD E6-15422 apply to?

AD E6-15422 applies to Raytheon — models B300. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive E6-15422

one-time

AD E6-15422 · 2006-09-19 · airframe

Airworthiness Directives; Raytheon Aircraft Company Model B300 Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Raytheon Aircraft Company (RAC) Model B300 airplanes. This AD requires you to modify the cabin passenger seats by installing a modification kit on each passenger seat, removing the existing technical standard order (TSO) label, and re-identifying each modified passenger seat assembly with a new part number. This AD results from the seats not meeting the ultimate load requirements of 14 CFR part 23 during structural testing of the seat with design changes. We are issuing this AD to prevent the passenger seats from failing during emergency landing conditions when high inertial loadings occur. Passenger seat failure may result in occupant injury.

Which aircraft AD E6-15422 applies to

MakesRaytheon

ModelsB300

certain

Whether AD E6-15422 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 E6-15422 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.