Honeywell PRIMUS 1000 Pilot's Manual page 23

Model
Remote Mounted
IC–600 Integrated Avionics Computer
(Pilot) (Symbol Generator (SG)/
Flight Director (FD)/
Autopilot (AP)
IC–600 Integrated Avionics Computer
(Pilot) (SG/FD/AP/TCAS)
IC–600 Integrated Avionics Computer
(Copilot) (SG/FD)
IC–600 Integrated Avionics Computer
(Copilot) (SG/FD/TCAS)
IC–600 Integrated Avionics Computer
(Pilot) (SG/FD/TCAS)
IC–600 Integrated Avionics Computer
(Copilot) (SG/FD)
IC–600 Integrated Avionics Computer
(Pilot) (SG/FD/AP/TCAS)
IC–600 Integrated Avionics Computer
(Copilot) (SG/FD/TCAS)
SM–200A Rudder/Aileron Servo Drive
Assembly
SM–200A Elevator Servo Drive Assy
SB–201A Servo Bracket
FX–220 Flux Valve
WU–660 Weather Receiver/
Transmitter/Antenna
VG–14A Vertical Gyro
CS–412 Dual Flux Valve Compensator
C–14D Directional Gyro
A28–1146–134
REV 1 Jan/03
R
PRIMUS 1000 Integrated Avionics System
Unit
Equipment List
Table 1–1 (cont)
Qty Part No.
1 7017000–80171
1 7017000–80172
1 7017000–81171
1 7017000–81172
1 7017000–80173
1 7017000–81173
1 7017000–80174
1 7017000–81174
2 4006719–906
1 4006719–904
3 4005842
2 2594484
1 7021450–601
2 7000622–901
1 2593379–1
2 4020577–3
Introduction
1-3