曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
AF 2) Set radioaltitude above 2500 ft.
AF 3) Place the airplane in simulated in-air condition.
AF 4) Position the TCAS ramp test set antenna at 0. relative
AF bearing to the aircraft.
AF 5) Set the test set to simulate an intruder aircraft with the
AF following parameters:
AF a) intruder type: ATCRBS
AF b) range: 5 NM
AF c) range rate: 400 Kts
AF d) altitude: 10800 ft
AF e) altitude rate: 0 ft/mn
AF 6) Set flaps to 30. to test the climb inhibit.
AF 7) Start scenario.
AF a) Check the TCAS issues the "TRAFFIC TRAFFIC"
AF annunciation and then issues the Resolution Advisory
AF "MONITOR VERTICAL SPEED".
AF b) Verify the TCAS does not issue the "CLIMB, CLIMB,
AF CLIMB" and the "INCREASE CLIMB, INCRASE CLIMB"
AF resolution advisories.
AF 8) Stop scenario.
AF (b) Increase climb inhibit test.
AF 1) Set flaps to 10..
AF 2) Start the same scenario as above.
AF a) Check the TCAS issues the "TRAFFIC, TRAFFIC"
AF annunciation, then the "CLIMB, CLIMB, CLIMB" resulotion
AF advisory.
AF b) Verify the TCAS does not issue the "INCREASE CLIMB,
AF INCREASE CLIMB" resolution advisory.
AF 3) Stop scenario.
AF (c) Altitude limit operation.
AF 1) Set flaps to 0..
AF 2) Set ADC to 30500 ft as read on altimeter.
AF 3) Set radioaltitude above 2500 ft.
AF 4) Place the airplane in simulated in-air condition.
AF 5) Position the TCAS ramp test set antenna at 0. relative
AF bearing to the aircraft.
AF 6) Set the test set to simulate an intruder aircraft with the
AF following parameters:
AF a) intruder type: ATCRBS
AF b) range: 10 NM
AF c) range rate: 250 Kts
AF d) altitude: 100 ft below aircraft altitude
AF e) altitude rate: 0 ft/mn
AF 7) Start the scenario.
AF a) Check the TCAS issues the "TRAFFIC, TRAFFIC"
AF annunciation but does not command a CLIMB advisory.
AF The advisory may be either a descend or a maintain.
EFFECTIVITY
AF AF, AT, GN, MD, VN, AF ALL AIRPLANES WITH AEB ATG X Page 506 AF 34-588 Apr 25/96
34-45-00
AF 8) Stop scenario.
AF
AF NOTE:____ A "CLIMB NOW" may occur but only after the descend
AF or maintain advisory.
AF
AF (7) Aural Warning priorities verification.
AF (a) Check of GPWS warning:
AF 1) Set flaps up.
AF 2) Set ADC to 11000 ft as read on altimeter.
AF 3) Set radioaltitude above 2500 ft.
AF 4) Place the airplane in simulated in-air condition.
AF 5) Position the TCAS ramp test set antenna at 0. relative
AF bearing to the aircraft.
AF 6) Set the test set to simulate an intruder aircraft with the
AF following parameters:
AF a) intruder type: ATCRBS
AF b) range: 5NM
AF c) range rate: 400 Kts
AF d) altitude: 10900 ft
AF e) altitude rate: 0 ft/mn
AF 7) Start scenario.
AF a) Check the TCAS issues the "TRAFFIC, TRAFFIC"
AF annunciation.
AF 8) Generate a GPWS test sequence and verify the TCAS system
AF automatically switches to TCAS OFF mode.
AF a) Check the GPWS "PULL UP" audio warning occurs.
AF b) Verify the TCAS system returns to normal operation at
AF the end of the test sequence.
AF 9) Stop scenario.
AF (b) Check of GPWS advisory:
AF 1) Set ADC to 900 ft as read on altimeter.
AF 2) Set radioaltitude to 1200 ft.
AF 3) Decrease to 1000 ft.
AF 4) Place the airplane in simulated in-air condition, with the
AF gear DOWN.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：747飞机维护手册AMM CHAPTER 34 - NAVIGATION 第34章导航4(37)
