Is AD 2013-14247 a recurring Airworthiness Directive?

No — AD 2013-14247 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 2013-14247

Q: Which aircraft does AD 2013-14247 apply to?

AD 2013-14247 applies to Hawker Beechcraft Corporation — models 800A, C-29A, U-125, 800B, 800, U-125A, 800XP, BAe.125. Serial/part conditions may narrow it to specific aircraft.

one-time

AD 2013-14247 · 2013-06-17 · airframe

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Model BAe.125 Series 800A (including C-29A and U-125), and 800B airplanes; and Model Hawker 800 (including variant U-125A) and 800XP airplanes modified in accordance with a certain winglet supplemental type certificate. This AD requires revising the Limitations section of the airplane flight manual (AFM) and installing placards on the instrument panel. This AD was prompted by reports of several instances of severe vibration and wing/aileron oscillations. We are issuing this AD to prevent vibration and wing/aileron oscillations, which could cause structural damage or lead to divergent flutter, and result in loss of integrity of the wing, loss of control of the airplane, and in-flight breakup.

Which aircraft AD 2013-14247 applies to

MakesHawker Beechcraft Corporation

Models800A, C-29A, U-125, 800B, 800, U-125A, 800XP, BAe.125, Hawker 800

Type certificate previously held by Raytheon Aircraft Company. Model BAe.125 Series 800A includes variants C-29A and U-125. Model Hawker 800 includes variant U-125A. Applies only to airplanes modified by Aviation Partners Inc. Supplemental Type Certificate (STC) ST01411SE.

Whether AD 2013-14247 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 2013-14247 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.