Honeywell International Inc. 9PGTPA-100A 用户手册
Page 2056
1 Dec 2003
34-45-4
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MAINTENANCE MANUAL
CAS-100 COLLISION AVOIDANCE SYSTEM
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9. Maintenance Procedures
A. In-Aircraft Adjustments
All alignment and adjustment procedures are done during bench maintenance. When the unit
performance shows an adjustment or an alignment is necessary, the technician must remove
the unit from the aircraft, then reference must be made to the related Component Maintenance
Manual.
performance shows an adjustment or an alignment is necessary, the technician must remove
the unit from the aircraft, then reference must be made to the related Component Maintenance
Manual.
B. System Protection
There are no fuses integral to the CAS-100 equipment. The system is protected by the circuit
breakers found at the circuit breaker panel in the aircraft.
breakers found at the circuit breaker panel in the aircraft.
C. Lubrication
There are no movable parts in the CAS-100. Thus, there is no lubrication necessary.
D. Cleaning
When thought necessary, depending upon the condition to which the equipment is exposed
and the intensity of use, periodic cleaning must be done. The exterior of the units must be
cleaned with a lint-free cloth moistened with an approved cleaning agent.
and the intensity of use, periodic cleaning must be done. The exterior of the units must be
cleaned with a lint-free cloth moistened with an approved cleaning agent.
NOTE: The cleaning of equipment interiors must be limited to that required when performing
overhaul (bench-type) work.