Description
Upper power lever located in the engine control quadrant for Cirrus SR 20, SR22 and SR22T generation 7 aircraft. For effectivity on your specific aircraft, reference Cirrus IPC 76-10-01
This power lever is subject to AD Â 2024-24-11 which calls for a dye penetrant inspection every 100hrs. Reference most recent revision of Cirrus SB2X-76-05 for effectivity and compliance.
Cirrus Service Bulletin SB2X-76-07 satisfies AD by replacing existing power lever with P/N 100079-001 (information For Reference Only) Refer to latest revision of SB2X-76-07 for effectivity.
