Honeywell International Inc. 9PGTPL-100A Manuale Utente
Page 1004
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.
The second method is used if other traffic displays are unable to show the failure because
of a display malfunction or some other reason. To start the second method, push the TEST
button located on the front panel of the MILACAS-FR Processor and read the fault codes
shown on the front panel LED indicator.
of a display malfunction or some other reason. To start the second method, push the TEST
button located on the front panel of the MILACAS-FR Processor and read the fault codes
shown on the front panel LED indicator.
Before doing a Mode S/TCAS system self test, make sure the following aircraft systems
are powered and operate with no failure flags on the cockpit instruments:
are powered and operate with no failure flags on the cockpit instruments:
•
Air data systems
•
Radio altimeter systems
•
Altitude (vertical gyro) systems
•
Heading (compass) systems.
NOTE: If the attitude and heading data supplied to the system is from an attitude
heading reference system (AHRS), inertial reference system (IRS) or inertial
navigation system (INS). Make sure they are aligned and in an operational
mode.
navigation system (INS). Make sure they are aligned and in an operational
mode.
D. Using Transponder Control Unit
NOTE: If a PPI radar/TCAS display is used as the traffic display and has a TCAS mode on
the selector switch, it must be turned to the TCAS position for the test. If not, the
selector switch should be turned to the OFF position to allow the traffic display
enable discrete (from the MILACAS-FR processor) to turn the display on. It needs
about 5 seconds after the test is started for the display to warm up.
selector switch should be turned to the OFF position to allow the traffic display
enable discrete (from the MILACAS-FR processor) to turn the display on. It needs
about 5 seconds after the test is started for the display to warm up.
(1) In dual Mode S-equipped aircraft, set the transponder selector on the transponder
control unit to position 1 to test the No. 1 transponder.
(a) Rotate the function selector counterclockwise to the TEST position and hold the
switch in this position for at least one second.
(b) Thereafter, the self-test continues automatically for approximately 12 seconds.
(2) If there are no malfunctions, the test sequence is as follows:
(a) A test pattern appears on the display to verify each type of intruder symbol. See
Figure 1001.
(b) For aircraft equipped with RA/VSI:
1
During the first few seconds of the test, the RA/VSI red and green
circumference lamps (climb/descend indicators) illuminate sequentially. The
TCAS flag is in view throughout the test period.
circumference lamps (climb/descend indicators) illuminate sequentially. The
TCAS flag is in view throughout the test period.