Is AD 2008-13-06 a recurring Airworthiness Directive?

No — AD 2008-13-06 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2008-13-06 apply to?

AD 2008-13-06 applies to Cessna — models 208B, 208. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2008-13-06

one-time

Official AD 2008-13-06 · FR doc E8-13564 · 2008-06-25 · airframe

Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes

What this AD requires

The FAA adopts a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. This AD requires you to inspect the left and right wing wire bundle(s) and repair or replace damaged wire. This AD also requires inspecting the wire bundles for correct attachment to the anchor points and correcting any deficient attachments. This AD results from chafed wiring found on wire bundles in the left and right wings containing the auto-control wing de-ice system, fuel quantity indication, and low fuel annunciation on the Cessna 208B airplanes. Improper installation of wire bundle supporting hardware can cause chafed wiring in the affected bundles. We are issuing this AD to detect and correct damaged wiring of the auto- control wing de-ice system, fuel quantity indication, and low fuel annunciation systems. This condition could result in incorrect fuel quantity indications, loss of low fuel quantity annunciations, or loss of the autocontrol wing de-ice system.

Which aircraft AD 2008-13-06 applies to

MakesCessna

Models208B, 208

Serial-conditional — narrows to serials 20800001–20800415, 208B0001–208B1299.

Chafed wiring found on wire bundles in left and right wings containing the auto-control wing de-ice system, fuel quantity indication, and low fuel annunciation system, per reports on several Cessna Model 208B airplanes.

Whether AD 2008-13-06 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 2008-13-06 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.