PhaseOne PAS 280 - Connecting the System to the Aircraft Power Source; Component Connections

PAS 280 Operation Guide
4. System Installation and Disassembly
Page 29 of
46
4.4.2 Connecting the System to the Aircraft Power Source
Table 3 lists the PAS 280 system power requirements.
Table 3 PAS 280 System Power Requirements
Parameter
Requirement
Voltage
28 VDC
Maximum current
10 A
Table 4 and Figure 19 show the pinout for the aircraft to iX Controller and stabilizer power cable
(P/N 75011000).
Table 4 Aircraft Power Cable Pinout
Wire
Pin
Voltage
Red
1
+28 VDC
Black
2
0 VDC
Figure 19. Aircraft Power Cable Pin Designation
To connect the aircraft power cable to the aircraft power outlet:
Note
Before connecting the power cable to the aircraft power outlet, make sure you have verified
voltage polarity.
1. Connect the PAS power cable to the aircraft power connector.
4.4.3 Component Connections
Note
• Do not excessively bend cables. Allow a bending radius of at least 40mm for all cables.
• Insert connectors into ports with care to prevent damage to pins.
• Make sure that the monitor port plug is properly secured in its socket.
• Use cable ties to secure the cables to the appropriate points on the monitor to ensure
that the plugs remain secured in their sockets.