PhaseOne PAS 280 - PAS 280 System Installed in Aircraft; Disassembling the System

PAS 280 Operation Guide
4. System Installation and Disassembly
Page 32 of
46
Order
P/N
Description
Connects to
19
-
IMU-POS AV (supplied with POS
AV)
POS AV PCS, IMU
IMU
20
-
Ground cable (not supplied with
system)
POS AV PCS Ground screw
Aircraft Ground
4.5 PAS 280 System Installed in Aircraft
Figure 20 shows the complete system installed and connected.
Figure 20. PAS 280 System Installed in Aircraft
4.6 Disassembling the System
1. Power switch on switches panel - verify that lowered.
2. Power supply circuit breaker in circuit breakers panel – verify pulled out.
3. Power cable - disconnect from aircraft power outlet.
4. Pilot monitor and operator monitor - disconnect from the cables, remove from monitor mount and
remove mounts from aircraft.
5. GPS antenna connection - disconnect and remove the antenna wiring from the aircraft.
6. System frame - remove screws securing system frame to stabilizer and remove system frame from
aircraft.
7. Stabilizer – remove screws securing stabilizer to the interface plate and remove stabilizer from aircraft.
8. Interface plate - remove screws securing interface plate to the aircraft floor and remove interface plate
from aircraft.
9. Perform any other changes required to return the aircraft to the regular approved configuration.