AD 2009-04-14

final rule
Data completeness: 70%

Airworthiness Directives; PILATUS AIRCRAFT LTD. Model PC-12/47E Airplanes

AD Number
2009-04-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2009-0146
FR Citation
74 FR 7810

Applicability

TypeManufacturerModelDetails
aircraft Pilatus AIRCRAFT LTD Airworthiness Directives; PILATUS AIRCRAFT LTD. Model PC-12/47E Airplanes
aircraft Aviat Various Airworthiness Directives; PILATUS AIRCRAFT LTD. Model PC-12/47E Airplanes

Unsafe Condition

During take-off with light turbulences or after rapid roll/heading attitude changes soon after take-off, both PFDs may indicate a roll attitude offset of up to 10 degrees in the same direction. This could result in an undesired bank angle.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Insert the limitation 'Maximum bank angle during climb must not exceed 30 degrees' into the POH. Insert procedures into the POH's Abnormal Procedures section for handling discrepancies between the PFD and ESIS, including using the ESIS as the primary attitude reference and engaging the flight director and autopilot until the error corrects itself.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight after the effective date of this AD

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

PILATUS AIRCRAFT LTD. Model PC-12/47E airplanes, manufacturer serial number (MSN) 545 and MSN 1001 and subsequent, certificated in any category.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.