Is AD 2013-29060 a recurring Airworthiness Directive?

No — AD 2013-29060 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2013-29060 apply to?

AD 2013-29060 applies to Beechcraft Corporation — models 1900, 1900C, 1900C (C-12J), 1900D. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2013-29060

one-time

AD 2013-29060 · 2013-12-09 · airframe

Airworthiness Directives; Beechcraft Corporation Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Beechcraft Corporation (type certificate previously held by Hawker Beechcraft Corporation) Models 1900, 1900C, and 1900D airplanes. This AD was prompted by reports of cracking in the front spar cap angles and hat section structure of the vertical stabilizer. This AD requires inspections of the vertical stabilizer spar angles and hat section for cracks with corrective actions as necessary. We are issuing this AD to correct the unsafe condition on these products.

Which aircraft AD 2013-29060 applies to

MakesBeechcraft Corporation

Models1900, 1900C, 1900C (C-12J), 1900D

Serial-conditional — narrows to serials UA-3–UA-3, UB-1–UB-74, UC-1–UC-174, UD-1–UD-6, UE-1–UE-439.

Serial ranges are per model: 1900 UA-3; 1900C UB-1 through UB-74 and UC-1 through UC-174; 1900C (C-12J) UD-1 through UD-6; 1900D UE-1 through UE-439.

Whether AD 2013-29060 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 2013-29060 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.