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Like I remember the function, when Rev Lever is pulled >6 deg and the Thrust Reverser switch is activated.
> Switch controls the thrust reverser isolation VLV solenoid and
> inhibits the control input from EEC/TCM discrete cards to the ECU.
The ECU takes over now and controls the thrust according to TAT/T12 and P0
Cannot remember if the A/T disconnect switches are activated when the lever is pulled to REV. or they only pulled by flightcrew
rgds
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