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DESCRIPTION General 03−10−1 Central Display System 03−10−2 Crew Alerting Messages 03−10−3 Master Warning/Master Caution Lights 03−10−12 Aurals 03−10−13 Aural Warning Test 03−10−17 Aural Warning Panel 03−10−18 Inhibits 03−10−18 Central Aircraft Information and Maintenance System (CAIMS) 03−10−21 Flight Data Recorder 03−10−23 Stall Warning 03−10−23 Takeoff Configuration Warnings 03−10−24 Landing Configuration Warning 03−10−25 EICAS Display 03−10−26 Systems Display (STAT Page) 03−10−27 Reversion Control Panel 03−10−28 PFD Reversion Control 03−10−29 PFD Reversion 03−10−30 EICAS Reversion Control 03−10−31 EICAS Reversion 03−10−32 SG Reversion Control 03−10−33 SG Reversion 03−10−34 EICAS Control Panel 03−10−37 Systems Reversion Control 03−10−38 Message Scrolling 03−10−40 Systems Synoptics 03−10−41 STAT Page 03−10−41 Bleed/AntiIce Synoptic Page 03−10−42 Air Conditioning Synoptic Page 03−10−43 Hydraulic Synoptic Page 03−10−44 AC Electrical Synoptic Page 03−10−45 DC Electrical Synoptic Page 03−10−46 Fuel Synoptic Page 03−10−47 AURAL AND VISUAL WARNINGS TABLE OF CONTENTS CHAPTER 3 03−00−1 Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 03−00−1 Page TABLE OF CONTENTS DESCRIPTION Flight Controls Synoptic Page 03−10−48 Aural and Visual Warning EICAS Messages 03−10−49 EMS CIRCUIT PROTECTION CB − Ind/Record System 03−20−1 CB − CAIMS System 03−20−2 AURAL AND VISUAL WARNINGS TABLE OF CONTENTS Flight Crew Operating Manual Rev 2A, Apr 11, 2005 CSP 700−5000−6 Volume 2 03−00−2 Page GENERAL The aural and visual warning system provides indications to warn of potentially unsafe operating conditions or airplane configurations, system malfunctions, and nonnormal situations. Indications can be generated by the following: · Crew alerting subsystem within the Engine Indication and Crew Alerting System (EICAS). · Enhanced Ground Proximity Warning System (EGPWS). · Weather Radar (WX) system. · Traffic alert and Collision Avoidance System (TCAS). · Altitude alert portion of the Air Data Computer (ADC). · Stick shaker portion of the Stall Protection System (SPS). EICAS provides crew with the necessary displays for airplane engine control and monitoring, control surface monitoring and all major subsystem synoptic displays. During normal operation, the engine and control surface information is displayed on the EICAS display unit (DU3) and the system synoptic information is displayed on the SYSTEMS display (DU4). GF0310_001 DU 1 DU 2 DU 3 DU 4 DU 5 DU 6 PFD 1 MFD 1 EICAS SYSTEMS MFD 2 PFD 2 VS 2000 TOC 3 KSRP 180 220 210 200 170 160 150 0.88 0.856 M 190 KPHX WX SAT GSPD −56 TAT TAS −40 234 345 LX HDG 330 ETE 1+36 KLAX TOC KPHX KDVT KSRP 4000 4000 FL180 FMS1 DTK 360 20 20 10 10 20 20 10 10 33 30 W 24 21 15 12 E 6 3 0 1 2 1 2 3 VAPP VNAV HDG AP1 ASEL 10400 29.92 IN H23.4NM SRP BARO 9500 10500 10000 HDG 330 3 12.5NM KDVT LUF KDVT 1300 5 1000 N 5 360 S N TERR OFF 30 6 33 185 6 4 TOTALFUEL(LBS) 41550 1.54 1.54 73.3 73.3 789 789 14600 10000 14600 2350 ND STAB NU NL RUDDER LWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 1.65 1.65 CRZ EPR SYNC N1 ITT OIL QTY (QTS) ENG APU www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier_Global_000-Aural_and_Visual_Warnings
