User's Manual

SYSTEM DESCRIPTION AND INSTALLATION MANUAL
TCAS 3000 Traffic Alert and Collision Avoidance System
34−43−23
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Page 7−7
15 Dec 2005
8. Procedure for the Pressure Transducer Module
A. Removal and Installation Procedure
(1) Remove the Pressure Transducer Module.
(a) Disconnect aircraft electrical mating connector from PTM connector J1.
(b) Disconnect pneumatic fitting from PTM.
(c) Loosen the two captive fasteners used to attach the PTM to its mounting bracket
or plate and remove unit.
(2) Reinstall the Pressure Transducer Module.
(a) Attach PTM to mounting bracket or plate with two captive screws.
(b) Connect pneumatic line to fitting on PTM.
(c) Connect aircraft electrical cable to PTM connector J1.
B. Adjustment Procedure
Not Applicable.
C. Repair Procedure
Not Applicable.
D. Return to Service Procedures
Do the Return to Service Test Procedures referenced in the ADJUSTMENT/TEST section
of this manual.