Is AD 06-4424 a recurring Airworthiness Directive?

No — AD 06-4424 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 06-4424 apply to?

AD 06-4424 applies to Cessna — models 208, 208B. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 06-4424

one-time

AD 06-4424 · 2006-05-16 · airframe

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

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2006-01-11 R1, which published in the Federal Register on March 16, 2006 (71 FR 13538), and applies to all The Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. AD 2006-01-11 R1 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). Current language in paragraph (e)(4) of AD 2006-01-11 R1 regarding the placard requirement inadvertently states: "You may insert a copy of this AD into the appropriate sections of the POH to comply with this action." This does not meet the intent of the AD. This document corrects that paragraph by removing the language referenced above.

Which aircraft AD 06-4424 applies to

MakesCessna

Models208, 208B

Whether AD 06-4424 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 06-4424 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.