Honeywell International Inc. 9PGTPA-100A Manuale Utente
Page 2049
1 Dec 2003
34-45-4
7
MAINTENANCE MANUAL
CAS-100 COLLISION AVOIDANCE SYSTEM
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(q) Above/Normal/Below Test
Using the TCAS Ramp Test Set, create scenario 1 to simulate an approaching
Mode C transponder equipped aircraft beginning at 10 nautical miles, an altitude of
12,000 feet, a closure rate of +450 knots, a 0 degree bearing, and an altitude rate
of 0 feet per minute.
Mode C transponder equipped aircraft beginning at 10 nautical miles, an altitude of
12,000 feet, a closure rate of +450 knots, a 0 degree bearing, and an altitude rate
of 0 feet per minute.
1 Set RA No. 1 to 2500 feet and pressure altitude of No. 1 and No. 2 air data
systems to 5000 feet.
2 Set Above/Normal/Below switch to ABOVE.
3 Observe target intruder appear as proximate traffic in 12 o’clock position on
TA/VSI +7000 ft.
4 Change the pressure altitude of No. 1 and No. 2 air data system to 10,000 feet.
Using the TCAS Ramp test set, create scenario 2 to simulate approaching Mode
C transponder equipped aircraft beginning at 10 nautical miles, an altitude of
3000 feet, a closure rate of +450 knots, a 0 degree bearing, and an altitude rate
of 0 feet per minute.
C transponder equipped aircraft beginning at 10 nautical miles, an altitude of
3000 feet, a closure rate of +450 knots, a 0 degree bearing, and an altitude rate
of 0 feet per minute.
5 Set Above/Normal/Below switch to BELOW.
6 Observe target intruder appear as proximate traffic in 12 o’clock position on
TA/VSI – 7000 ft.
7 Set Above /Normal/Below switch to NORMAL and observe intruder disappear
from display.
8 Change pressure altitude of No. 1 and No. 2 air data systems to 3000 feet and
repeat scenario 2 in test 100. Observe intruder on display as proximate traffic in
12 o’clock position, 0 feet.
12 o’clock position, 0 feet.