Specifications

CO Guardian LLC Document No. 01-2510-02
1951 E. AIRPORT DRIVE Date: 11/23/02
TUCSON, AZ. 85706 REV A
c. Install circuit breaker per Figure 3 and wiring per Figure 4. It is recommended
that the circuit breaker be installed on the Avionics Master switch buss. See
Figure 3.
FIGURE 3 - Circuit Breaker Cutout
Notes
1. Connect to +14 VDC or to +28 VDC power as applicable to aircraft and CO Detector rating.
2. Twist the power and ground return wires together approximately 6 turns per foot.
3. Ground power return wires to aircraft structure near circuit breaker panel.
4. All wire to be MIL-W-22759/16 or equivalent.
FIGURE 4 - Installation Schematic
d. Mount CO Detector per Figure 2.
e. With the CO Detector disconnected from the aircraft harness, conduct a
continuity check of the added aircraft wiring.
MODEL 452 INSTALLATION AND OPERATIONAL MANUAL Page 12 of 17