EFFECTIVITY
AF AF, AT, GN, MD, VN, AF ALL AIRPLANES WITH AEB ATG X Page 509 AF 34-588 Apr 25/96
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AF 5) Position the TCAS ramp test set antenna at 0. relative AF bearing to the aircraft. AF (b) Descent advisory. AF 1) Set the test set to simulate an intruder aircraft with the AF following parameters: AF a) intruder type: ATCRBS AF b) range: 6 NM AF c) range rate: 400 Kts AF d) altitude: 11100 ft AF e) altitude rate: 0 ft/mn AF 2) Check the TCAS operation is the same as Table 1 below. AF 3) Start scenario and chronometer simultaneously. AF AF ~êêê AF DISTANCE TIME AUDIO IVSI AF è”””. AF Start scenario: 6 NM t0 AF Traffic advisory: 5 NM t1 2X TRAFFIC AF Resolution advisory: 3.3 NM t1+15 sec 3X DESCENT Red/Green arcs AF Followed by: 2X INCREASE DESCENT Red/Green arcs AF Clear of conflict: 0 NM t0+54 sec 1X CLEAR OF CONFLICT AF ééé AF Table 1 AF 4) Stop scenario. AF (c) Climb advisory. AF 1) Set the test set to simulate an intruder aircraft with the AF following parameters: AF a) intruder type: mode S AF b) range: 6 NM AF c) range rate: 400 Kts AF d) altitude: 10800 ft AF e) altitude rate: 0 ft/mn AF 2) Check the TCAS operation is the same as Table 2 below. AF 3) Start scenario and chronometer simultaneously. AF AF ~êêê AF DISTANCE TIME AUDIO IVSI AF è”””. AF Start scenario: 6 NM t0 AF Traffic advisory: 5 NM t1 2X "TRAFFIC" AF Resolution advisory: 3.3 NM t1+15 sec 3X "CLIMB" Red/Green arcs AF Followed by: 2X "INCREASE CLIMB" Red/Green arcs AF Clear of conflict: 0 NM t0+54 sec 1X "CLEAR OF CONFLICT" AF ééé AF Table 2 AF 4) Stop scenario.
EFFECTIVITY AF AF, AT, GN, MD, VN, AF ALL AIRPLANES WITH AEB ATG X Page 510 AF 34-588 Apr 25/96
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AF (10) Bearing precision check.
AF
AF NOTE:____This check may be performed either on an outside open area
AF clear of ground equipment, by displacing the ramp tester
AF around the plane, or inside docks with the help of the TCAS
AF antenna coupler, without moving the ramp tester.
AF
AF (a) Initial settings.
AF 1) Set flaps up.
AF 2) Place airplane in simulated in-air condition.
AF 3) Set radioaltitude above 2500 ft.
AF 4) Set ADC 1 to 11000 ft as read on altimeters.
AF 5) Set both IVSI to 4 NM range.
AF 6) Position the TCAS ramp test set antenna or antenna coupler
AF at 0. relative bearing to the aircraft.
AF 7) Set the test set to simulate an intruder aircraft with the
AF following parameters:
AF a) intruder type: mode S
AF b) range: 2 NM
AF c) range rate: 0 Kts
AF d) altitude: 11000 ft
AF e) altitude rate: 0 ft/mn
AF 8) Check the intruder symbol bearing on each IVSI does not
AF differ by more than 15. for each of the following test set
AF bearing relative to the checked antenna:
AF
AF Bearing: 0., 30., 60., 90., 120., 150., 180., 210., 240.,
AF 270., 300., 330..
AF 9) Repeat this test for each upper and lower antenna.
AF 10) Stop the test set.
AF (11) Verify RA inhibition for intruder without altitude.
AF (a) Initial settings for TCAS operation with an intruder reporting
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本文鏈接地址：747飛機維護手冊AMM CHAPTER 34 - NAVIGATION 第34章導航4(39)
