User's Manual

SYSTEM DESCRIPTION AND INSTALLATION MANUAL
TCAS 3000 Traffic Alert and Collision Avoidance System
34−43−23
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Page 7−5
15 Dec 2005
B. Adjustment Procedure
Not Applicable.
C. Repair Procedure
Most omnidirectional antennas are non−repairable. If the antenna is damaged or
determined to be faulty, it must be replaced with a new antenna.
D. Return to Service Procedures
Do the Return to Service Test Procedures referenced in the ADJUSTMENT/TEST section
of this manual.
6. Procedure for the Control Panel
A. Removal and Installation Procedure
(1) Remove the Control Panel.
(a) Disengage Dzus fasteners on control panel.
(b) Pull control panel out of aircraft mounting location and disconnect aircraft cable
connectors. Control panel is now free to be removed from aircraft.
(c) Put electrostatic protective covers on control panel and aircraft mating electrical
connectors.
(2) Reinstall the Control Panel.
(a) Remove protective covers from control panel and aircraft mating connectors.
(b) Connect aircraft cables to control panel connectors J1 and J2.
(c) Insert control panel into mounting location.
(d) Engage Dzus fasteners on the control panel to attach it to aircraft structure.
B. Adjustment Procedure
Not Applicable.
C. Repair Procedure
Any repair procedures should be in accordance with the manufacturer’s repair
instructions.
D. Return to Service Procedures
Do the Return to Service Test Procedures referenced in the ADJUSTMENT/TEST section
of this manual.