On our last two flights, when the ignition was switched OFF the auto retract failed & the engine had to be retracted manually.
Replicating the sequence on the ground, the ECU flashed "BRAKE? .. BRAKE? ..", an audible pulse tone sounded & automatic engine retraction did not occur.
Ref FM 7.3.31 Cancel this warning by pushing the Menu button, then automatic retraction will proceed (otherwise manual retraction & manual prop brake is required). The reason for this failure is " ... the requirements for starting the automatic retraction process have not been met"
And the requirements are:
1) "... engine rpm >2000 & >2000rpm for at least 10s" &
2) "... the limit switch for the extended position is closed"
I'm certain condition 1) was met. Unsure re Condition 2) as the extended limit switch is mounted on the spindle drive & appears to be a magnetic reed type? When fully extended, the "extended" LED is illuminated, suggesting the switch is closed.
I'd appreciate advice / suggestions on how to check this. The Wiring Diagram (MM #10) lacks detail. Thanks, Bill (VH-FIG)