Honeywell International Inc. 9PGTPL-100A Manuale Utente

Pagina di 180
Page 2019
1 Mar 2006
34-45-54
MAINTENANCE MANUAL
TPL-100A Processor / Part No. 940-0530-001
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
(c) Secure the antenna to the aircraft using four or eight screws. Apply approved 
lock-tight sealant to the mounting screws.
(d) Connect the four coaxial cables to the corresponding connectors J1-J4 on the 
antenna.
(e) Apply approved sealant around the outer edge of the antenna to seal the antenna 
to the aircraft fuselage.
C. System Functional Testing (Self-Test)
After removal and replacement of any component of the system, do an inspection and 
system checkout as described in paragraph 5.A and 5.B.
7.
Maintenance Procedures
A. In-Aircraft Adjustments
All alignment and adjustment procedures are accomplished during bench maintenance. 
When unit performance indicates an adjustment or an alignment is required, the technician 
must remove the unit from the aircraft. See the applicable component maintenance manual 
for the unit.
B. System Protection
There are no fuses integral to the system equipment. The system is protected by circuit 
breakers located at the circuit breaker panel in the aircraft.
C. Lubrication
There are no moving parts in the system. No lubrication is required.
D. Cleaning
When necessary, depending upon the environment to which the equipment is exposed and 
the intensity of use, periodic cleaning must be done. The exterior of the units must be wiped 
with a lint-free cloth dampened with an approved cleaning agent.
NOTE: Any cleaning of equipment interiors must be limited to that required when 
performing overhaul (bench-type) work.