Output Command DOl-Power-On Destination: DOI Acceptable Values: ( high] Initiation Delay: 0 milliseconds Completion Deadline: 50 milliseconds Exception-Handling: ( What to do if cannot issue command within deadline time) Feed back Information Variables: DOl-status-signal Values: high(on) Relationship: Should be on if ASW sent signal to turn on Min. time(latency ) 2 seconds Max time: 4 second Exception Handling: Dol-Status changed to Fault-Detected Reversed By: Turned off by some other component or components. Do not know which ones Comments: I am assuming that if we do not know if the dol is on, it is better to turn it on again, i.e., that the reason for the restriction is simply hysteresis and not possible damage to the device This product in the family will turn on the doE only when the aircraft descends below the threshold altitude. Only this page needs to change for a product in the family that is triggered by rising above the threshold References: CONTENTS discrete signal on line PWR set to high TRIGGERING CONDITION Control Mode Operational Not inhibited State values Ititude below-threshhold Prev(Altitude)= At-or-above-thresholdOutput Command DOI-Power-On Destination: DOI Acceptable Values: Initiation Delay: {high} 0 milliseconds Completion Deadline: 50 milliseconds Exception-Handling: Feedback Information: Variables: (What to do if cannot issue command within deadline time) DOI-status-signal Values: high (on) Relationship: Should be on if ASW sent signal to turn on Min. time (latency): 2 seconds Max. time: 4 seconds Exception Handling: Reversed By: DOI-Status changed to Fault-Detected Turned off by some other component or components. Do not know which ones. Comments: I am assuming that if we do not know if the DOI is on, it is better to turn it on again, i.e., that the reason for the restriction is simply hysteresis and not possible damage to the device. This product in the family will turn on the DOE only when the aircraft descends below the threshold altitude. Only this page needs to change for a product in the family that is triggered by rising above the threshold. References: CONTENTS = discrete signal on line PWR set to high TRIGGERING CONDITION T Prev(Altitude) = At-or-above-threshold T Altitude = Below-threshhold State Values DOI-Status = On F Operational T Not Inhibited T Control Mode