Airworthiness Directive 2009-08-10
one-timeAirworthiness Directives; Pilatus Aircraft Ltd. Model PC-12/47E Airplanes
What this AD requires
We are adopting a new airworthiness directive (AD) for the products listed above that will supersede an existing AD. This AD results from mandatory continuing airworthiness information (MCAI) issued by the 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 2009-08-10 applies to
Addresses both Primary Flight Displays potentially indicating a roll attitude offset of up to 10 degrees after an accelerated turn onto the runway followed immediately by take-off; requires a revised operational procedure (POH limitation on bank angle during climb).
Whether AD 2009-08-10 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:
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.