Is AD 2006-01-11 a recurring Airworthiness Directive?

No — AD 2006-01-11 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2006-01-11 apply to?

AD 2006-01-11 applies to Cessna — models 208, 208B. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2006-01-11

one-time

Official AD 2006-01-11 · FR doc 06-2546 · 2006-03-16 · airframe

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

What this AD requires

This document clarifies the intent of AD 2006-01-11, which was published in the Federal Register on January 12, 2006 (71 FR 1941). AD 2006-01-11 applies to Cessna Models 208 and 208B airplanes and requires the installation of a pilot assist handle and deicing boots on the cargo pod and landing gear fairings; and the incorporation of changes to the Pilot's Operating Handbook (POH) and FAA-Approved Airplane Flight Manual (AFM). The compliance time for the AFM/POH change currently reads "prior to further flight" after the installation of the pilot assist handle, which is required within 125 days after the effective date. The AFM/POH change is related to operation in ground icing conditions and should not be attributed to the pilot assist handle installation. Therefore, the compliance time should also be within 125 days after the effective date. Additionally, the requirement of installing the accessory kit or installing a placard should only apply to those airplanes equipped with a cargo pod and pneumatic deicing boots. The way it currently is written makes it apply to all airplanes equipped with pneumatic deicing boots. This AD action rewords the compliance time and the wording for the installation or placard requirement to reflect the above concerns.

Which aircraft AD 2006-01-11 applies to

MakesCessna

Models208, 208B

Whether AD 2006-01-11 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 2006-01-11 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.