Airworthiness Directive 06-3252

one-time
AD 06-3252 · 2006-04-05 · 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) 2006-06-06, which published in the Federal Register on March 16, 2006 (71 FR 13533), and applies to all The Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. AD 2006-06-06 requires you to incorporate information into the applicable section of the Airplane Flight Manual (AFM) and Pilots Operating Handbook (POH) and requires installation of placards. Current language in paragraph (f)(3) of AD 2006-06-06 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 06-3252 applies to

MakesCessna
Models208, 208B

Whether AD 06-3252 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 06-3252 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.