Is AD E6-14781 a recurring Airworthiness Directive?

No — AD E6-14781 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD E6-14781 apply to?

AD E6-14781 applies to Raytheon — models 390. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive E6-14781

one-time

AD E6-14781 · 2006-09-08 · airframe

Airworthiness Directives; Raytheon Aircraft Company Model 390 Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Raytheon Aircraft Company Model 390 airplanes. This AD requires you to inspect the spigot bearing, part number (P/N) MS14104-16, for the proper position in the spigot fitting assembly and to install the wing spigot bearing retainer kit, P/N 390-4304-0001. We are issuing this AD to detect spigot bearings that are not positioned flush with the fitting assembly. This condition could result in the spigot bearing becoming disengaged from the fitting assembly, which could cause motion between the wing and the fuselage and degrade the structural integrity of the wing attachment to the fuselage. This could lead to wing separation and loss of control of the airplane.

Which aircraft AD E6-14781 applies to

MakesRaytheon

Models390

Part-conditional — 390-4304-0001.

certain

Whether AD E6-14781 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 E6-14781 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.