Airworthiness Directive 2013-16-01

one-time
Official AD 2013-16-01 · FR doc 2013-20098 · 2013-08-20 · airframe

Airworthiness Directives; Beechcraft Corporation and Hawker Beechcraft Corporation

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 58, 95-C55, E55, and 56TC airplanes; and Hawker Beechcraft Corporation Models 58P and 58TC airplanes (both type certificates previously held by Raytheon Aircraft Company). This AD was prompted by reports of elevator balance weights becoming loose or failing because the balance weight material was under strength and did not meet material specifications. This AD requires inspections of elevator balance weights and replacement of defective elevator balance weights. We are issuing this AD to correct the unsafe condition on these products.

Which aircraft AD 2013-16-01 applies to

MakesBeechcraft CorporationHawker Beechcraft Corporation
Models58, 58P, 58TC, 95-C55, 95, E55, 56TC

Applies to all serial numbers of the listed models. Beechcraft Corporation Models 58, 95-C55, E55, and 56TC: type certificate previously held by Hawker Beechcraft Corporation. Hawker Beechcraft Corporation Models 58P and 58TC: both type certificates previously held by Raytheon Aircraft Company.

Whether AD 2013-16-01 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2013-16-01 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.