Is AD 99-10314 a recurring Airworthiness Directive?

No — AD 99-10314 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 99-10314 apply to?

AD 99-10314 applies to Raytheon. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 99-10314

one-time

AD 99-10314 · 1999-04-28 · airframe

Airworthiness Directive; Raytheon Aircraft Company Beech Models A36, B36TC, 58, 58A, C90A, B200, B300, and 1900D Airplanes

What this AD requires

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Beech Models A36, B36TC, 58, 58A, C90A, B200, B300, and 1900D airplanes. This AD requires inspecting for interference or inadequate clearance between the flight control mechanism and any component located forward of the instrument panel. If interference or inadequate clearance is found, this AD requires securing all components so that they are clear of the flight control mechanism. This AD is the result of an incident where the electrical/avionics wires made contact with and restricted the control system of the affected airplanes. The actions specified by this AD are intended to prevent any component or wiring from interfering with the flight control mechanism caused by inadequate clearance, which could result in reduced or loss of aileron and/or elevator control.

Which aircraft AD 99-10314 applies to

MakesRaytheon

Boilerplate applicability only; the specific model/serial-number list precedes this excerpt and is not included. Requires inspecting for interference/inadequate clearance between the flight control mechanism and components forward of the instrument panel, and securing any interfering components, per Raytheon Mandatory Service Bulletin SB 27-3232 (March 1999), to prevent reduced or loss of aileron and/or elevator control.

Whether AD 99-10314 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 99-10314 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.