Airworthiness Directive 2009-03-05

one-time
Official AD 2009-03-05 · FR doc E9-3046 · 2009-02-20 · turboshaft engine

Airworthiness Directives; Pratt & Whitney Canada PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and PW207E Turboshaft Engines

What this AD requires

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Which aircraft AD 2009-03-05 applies to

MakesPratt & Whitney Canada
ModelsPW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, PW207E, PW206, PW207

Installed on, but not limited to, MD Explorer; Agusta S.p.A. A109, A109E, A109S; Bell Helicopter Textron Canada Limited 427; Bell 429; and Eurocopter Deutschland GmbH EC135 P1 and EC135 P2 helicopters. For engines converted from one model to another, see Effectivity paragraph 1.A of PWC Alert Service Bulletin (ASB) PW200-72-A28280, Revision 4, dated August 28, 2007

Whether AD 2009-03-05 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 2009-03-05 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.