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Vertical"Power"VP.200"Release"Notes""""""Tech"Support"505"715.6172"
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Version 14.3 changes:
• Configuration change: You can now configure which devices remain on if the battery
contactor fails. This is in the Device Setup menu, and all devices are set to off by default.
• Circuit protection algorithms have been upgraded to reduce nuisance trips.
• Configuration change: You can now configure a fuse to be standard blow (default) or
slow blow (2x delay).
• Load shedding setup has been moved to the device setup menu.
• The starter is now shown in yellow when it is disabled. It is always disabled in pre-flight
mode.
• Devices are now yellow when their status is unknown. This occurs when 1) loss of
comm. with control unit 2) the CU is not responding to requests to switch a device 3) a
device with multiple pins has some on and some off.
• Battery voltage is now read off the e-bus line, giving a more accurate reading.
• The e-bus and battery contactor are now items on the device list, and can be used to
reset faults but not turn them on or off manually.
• Flaps device now shows current.
• Configuration change: CU J5-6 can now be configured like any other power pin (for
configurations 1, 2, 3). Note this pin is grounded when active (rather than providing bus
voltage).
• Serial data communication is more robust.
• Faults are now listed below each pin on a device, so you can see which pin the fault is
associated with.
Version 14.3.h updates:
• Configuration change: J4P7 has been inadvertently handled as a 5 amp circuit, when it’s
only a 3 amp circuit. If you have configured your system to use J4P7 on CU1 and CU2
(for VP-200 duals), then you need to re-configure J4P7 by going into the Device Setup
screen, updating the circuit breaker to the desired level, and Saving you changes for
each device affected.
• False-positives and multiple-notifications for low voltage alerts have been fixed.
• The MapCom engine data stream input capability from the newer Chelton EFIS systems
has been fixed.
Version 15.1 changes:
• Added stronger synchronization capabilities for importing and exporting the settings
data.
• Battery and E-bus were removed from the device list. They were first introduced in V14,
but found to cause inconsistencies when faults associated with those devices were
"cleared". The pilot now needs to cycle power in order to clear these faults; typically this
would be performed on the ground while diagnosing the problem with the battery
contactor and e-bus fuse(s).
• Configuration Change: Optional Engine Data inputs for OAT, fuel flow, carburetor
temperature, and air speed are now enabled for all Engine Data systems. The pilot
should verify/set the appropriate YES/NO indicators under the Serial Setup screen. The
default value is NO.
(21 Seiten)
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