Airworthiness Directive 2008-07-10

one-time
Official AD 2008-07-10 · FR doc E8-6959 · 2008-04-07 · airframe

Airworthiness Directives; Hawker Beechcraft Corporation Models B200, B200GT, B300, and B300C Airplanes

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation (HBC) Models B200, B200GT, B300, and B300C airplanes. This AD requires you to fabricate and install a placard incorporating information that limits operation when there is known or forecast icing and requires you to replace a section of the pneumatic supply tube for the tail deice system with a new tube of a different material. This AD results from reports of collapsed tail deice boot pneumatic supply tubes. We are issuing this AD to prevent collapsed pneumatic supply tubes, which could result in failure of the tail deice boots to operate. This failure could lead to loss of control in icing conditions.

Which aircraft AD 2008-07-10 applies to

MakesBeechcraft
ModelsB200, B200GT, B300, B300C
Serial-conditional — narrows to serials BB-1926–BB-1926, BB-1978–BB-1978, BB-1988–BB-2000, BY-1–BY-26, FL-427–FL-427, FL-493–FL-493, FL-500–FL-573, FM-14–FM-18.

Reports of collapsed tail deice boot pneumatic supply tubes; could result in failure of tail deice boots to operate, potentially leading to loss of control in icing conditions.

Whether AD 2008-07-10 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 2008-07-10 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.