Bombardier-Challenger_01-Flight_Instruments庞巴迪挑战者飞行仪表

航空发表于 2010-5-9 09:03:46

Bombardier-Challenger_01-Flight_Instruments
 
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航空发表于 2010-5-9 09:04:02

cftsuencjer OPERATING MANUAL PSP 601A-6 SECTION 11 FLIGHT INSTRUMENTS TABLE OF CONTENTS Page 1 . GENERAL 1 2. PITOT-STATIC SYSTEM AND TEMPERATURE SENSING SYSTEM 1 3. DIGITAL AIR DATA SYSTEM 1 4. ELECTRONIC FLIGHT INSTRUMENT SYSTEM 2 LIST OF ILLUSTRATIONS Figure Number Title Page 1 Pi t o t - S t a t i c System - Schematic 3 2 Pi t o t - S t a t i c System - Components 4 3 Pitot-Static System - Standby Indicators 5 4 DADS - Simplified Block. Diagram 6 5 DADS - Mach/Airspeed Indicators and Altimeters 7 6 DADS - Vertical Speed Indicators and Associated AFCS Advisory Display 8 7 DADS - EFIS EADI Air Data Displays (2 Sheets) 9 8 DADS - EFIS Instrument Remote Controllers 11 9 EFIS - Simplified Block Diagram 12 10 EFIS - EADI Normal Displays 13 11 EFIS - EADI Failure Warning Annunciators (2 Sheets) 14 12 EFIS - EADI Category 2 Annunciator 16 13 EFIS - EADI Comparison Monitor Annunciators 17 14 EFIS - EADI Reversionary Source Annunciators 18 11-CONTENTS Page 1 Apr 02/87 Fi gure Number 16 17 18 19 20 21 22 23 24 25 26 27 28 EFIS EFIS EFIS EFIS EFIS EFIS EFIS EFIS EFIS EFIS EFIS EFIS EFIS EFIS OPERATING WIMWL PSP601A-6 Title Page EHSI Full Compass Mode 19 EHSI ARC Mode 20 EHSI MAP Mode 21 EHSI Weather Radar Display 22 EHSI Failure Warning Annunciators 23 EHSI Comparison Monitor Annunciator 24 EHSI Reversionary Source Annunciators 25 Composite Display 26 MFD MAP Mode 27 MFD PLAN Mode 28 Display Controller 29 Instrument Remote Controllers 30 MFD Controller 31 Remote Switch/Lights 32 11- Page 2 Apr 02/87 OPERATING MANUAL PSP 601A-6 SECTION 11 FLIGHT INSTRUMENTS GENERAL The flight instrument systems consist of the pi tot-static system, the temperature sensing system, the digital air data system, the electronic flight instrument system and the vertical gyros. PITOT-STATIC SYSTEM AND TEMPERATURE SENSING SYSTEM (Figures 1, 2 and 3) The pi tot-static system provides the pi tot and static pressures required to operate the digital air data computers No- 1 and No. 2 (DADC 1 and DADC 2) and the standby pneumatic airspeed indicator (ASI). Static pressure is provided to operate the standby pneumatic altimeter (ALT), and the cabin pressure indicator (CPI). The pi tot-static system consists of the pilot's and copilot's pi tot-static heads, the left and right static ports, and the pilot's and copilot's STATIC PRESSURE SELECTOR valves. A dual temperature-sensing probe, located on the right side of the forward fuselage, provides a total-air-temperature (TAT) input to DADC 1 and DADC 2. The pi tot tubes, static ports and temperature probe contain anti-icing heater elements that are controlled from the A.D.S. HEATER CONT. panel. For a description of the CPI, refer to Section 2. DIGITAL AIR DATA SYSTEM (Figures 4 through 9) The digital air data system provides the flight guidance computers and control systems with altitude hold, airspeed programming, vertical speed and Mach control information. The digital air data system also provides altitude alerting and reporting and indications of altitude, airspeed, vertical speed, true airspeed, static air temperature and total air temperature. The digital air data system consists of two complete systems with two digital air data computers, DADC 1 and DADC 2. The DADCs receive total pi tot-static pressures from the pi tot-static system, and temperature signals from the total-air-temperature probe. Other inputs to the DADCs are from the BARO control on the barometric altitude indicator, the copilot's ALT SEL control on the electronic flight instrument system (EFIS) remote controller, and flap position information from the flap control unit. From these inputs, the DADCs compute and generate output signals for the following systems or components: Pilot's and copilot's Mach/airspeed indicators (MASI) Pilot's and copilot's altimeters SECTION 11 Page 1 Apr 02/87 ctvanenaer OPERATING MANUAL PSP 601A-6 Pilots and copilot's vertical speed indicators (VSI) Pilots and copilot's electronic flight instrument system (EFIS) Automatic flight control system (AFCS) Aural warning system Flight management system (FMS) ATC transponder system Master caution and warning system The AFCS advisory display panel displays static-air-temperature (SAT), total air temperature (TAT) and true airspeed (TAS). The digital air data system consists of two digital air data computers, two Mach/airspeed indicators, two altimeters, two vertical speed indicators and a dual TAT probe. ELECTRONIC FLIGHT INSTRUMENT SYSTEM (Figures 9 through 28) The electronic flight instrument system (EFIS) converts inputs from the aircraft sensors, long-range navigation (LRN) and short-range navigation (SRN) systems into video signals for display on electronic display units. The EFIS comprises three subsystems: the pilot's display system, the copilot's display system and the multifunction display (MFD) system. The pilot's and copilot's display systems are identical, each using two electronic display units to provide conventional attitude director and horizontal situation information, using a display controller, an instrument remote controller and a symbol generator. In addition to the conventional displays, the electronic attitude director indicator (EADI) and electronic horizontal situation indicator (EHSI) provide a number of other displays such as IAS/Mach, map and weather radar displays, selectable from the display controllers. The display controllers also provide for navigation source selection and bearing source selection. The pilot's and copilot's instrument remote controllers provide for control of the flight director related displays on the EADI and EHSIThe MFD system provides additional long-range mapping information, checklists and weather radar displays (refer to Section 11). The MFS system can also serve as a back-up system for either the pilot's or copilot's display system. The MFD controller provides for selection and control of the MFD formats, modes, waypoint designators and back-up modes. SECTION 11 Page 2 Apr 02/87 OPERATING MANUAL PSP 601A-6 LEGEND PILOTS PITOT-STATIC HEAD PITOT PRESSURE UNE STATIC PRESSURE LINE COPILOTS PITOT-STATIC HEAD 晻? ? 01 ALT. STATIC SOURCE SW. PILOTS SIOE CONSOLE DRAIN =<D>-fi DRAIN DADC1 SI DRAIN S2 DRAIN CENTRE INSTRUMENT PANEL P2 V COPILOTS SIDE PANEL anttp MANIFOLD S-_ limit DRAIN ?? STATIC PORT S3 STATIC PORT S3 atttittratintituiiii ALT. STATIC SOURCE SW. COPILOTS SIDE CONSOLE ?O DRAIN DADC2 DRAIN Pi tot-Static System - Schematic Figure 1 SECTION 11 Page 3 Apr 02/87 OPERATING MANUAL PSP G01A-6 f: IK'. PITOT HEAT FAIL ANNUNCIATOR Indicates a failure of the on-side pitot-static tube heater. O HTR FAIL SWTTCrVUGHT Indicates a static port, angie-ofattack <AOA> vane and/or totahairtemperture (TAT) probe heater failure. PWR ? METER SELECT SWITCH Turns on heater elements (when set to any position except HTRS OFF) for the static ports, the pitot-static tubes, the angje-of-attack (AOA) vanes, and the total-air-temperature (TAT) probe. The switch also selects the current readings indicated by the % HTR CURRENT meter. % HTR CURRENT METER Indicates the percentage of current drawn by the heater selected by the PWR B METER SELECT switch. SAFETY GUARD REMOVED FOR CLARITY PILOTS AND COPILOTS SELECTOR VALVES STATIC TUBE - The on-side cfigrtaJ air data computer receives static pressure inputs from the primary source. ALTERNATE SOURCE - The on-side dgrtai air data computer receives stauc pressure from the secondary (alternate) source. Pitot-Statlc System - Components Figure 2 SECTION 11 Page 4 Apr 02/87 BARO CONTROL OPERATING MANUAL PSP 601A-6 STANDBY AIRSPEED INDICATOR ALTITUDE POINTER ALTITUDE INDICATOR BARO INDICATOR CENTRE INSTRUMENT PANEL Pi tot-Static System - Standby Indicators Figure 3 SECTION 11 Page 5 Apr 02/87 OPERATING MANUAL PSP 601A-6 ATC1 PfTOT-STATIC INPUTS [FLAP .CONTROL UNIT FLAP POSITION COPILOTS INSTRUMENT REMOTE CONTROLLER ALTSEL TAT AFCS ADVISORY DISPLAY ALTITUDE REPORTING DADC1 MACH/AIRSPEED ALTTTUDE/BARO CORRECTION TO MASTER CAUTION AND WARNING SYSTEM VERTICAL SPEED PiLOT S MACH/AIRSPEED INDICATOR PILOTS ALTIMETER PILOTS VERTICAL SPEED INDICATOR ALTITUDE ALERT/OVERSPEED PILOTS EADI K ASCB ALTSEL TAT { PROBE TAT FLAP POSITION PfTOT-STATIC INPUTS DADC2 2EL/ TO FMS, EFIS IRS AND AFCS AURAL WARNING SYSTEM MACH/AIRSPEED ALTITUDE ALERT/OVERSPEED COPILOTS MACH/AIRSPEED INDICATOR ^ TO MASTER CAUTION ^ AND WARNING SYSTEM COPILOTS ALTIMETER COPILOTS VERTICAL SPEED INOICATCP. COPILOTS EADI ALTITUDE REPORTING ATC2 DADS - Simplified Block Diagram Figure 4 SECTION 11 Page 6 Apr 02/87 MACH COUNTER VMO POINTER AIRSPEED POINTER MEMORY INDEX POINTER (YELLOW) POINTBl BARO SET KNOB canaaair ctianentjer OPERATING MANUAL PSP 601A-6 MACH/AIRSPEED INDICATOR BARO COUNTERS ALTIMETER MEMORY INDEX POINTER (WHITE) FAILURE WARNING FLAG MEMORY INDEX POINTER (RED) MEMORY INDEX POINTER (GREEN) ALTITUDE ALERT ANNUNCIATOR FAILURE WARNING FLAG ALTITUDE COUNTER PILOTS AND COPILOT'S INSTRUMENT PANELS DADS - Mach/Airspeed Indicators and Altimeters Figure 5 SECTION 11 Page 7 Apr 02/87 OPERATING MANUAL PSP 601A-6 VERTICAL SPEED INDICATOR POINTER FAILURE WARNING FLAG PILOTS AND COPILOrS INSTRUMENT PANELS SAT DISPLAY Displays SAT in < t Celsius. TAT DISPLAY Displays TAT in degrees Celsius. TAS DISPLAY Displays TAS in knots. BRT CONTROL Controls the overall display brightness. CENTRE INSTRUMENT PANEL DADS - Vertical Speed Indicators and Associated AFCS Advisory Display Figure 6 SECTION 11 Page 8 Apr 02/87 ctianenefer OPERATING MANUAL PSP 601A-6 IAS ACCELERATION TREND VECTOR Indicates the air a aft IAS trend based on acceleration. Displayed in magenta and inhibited below GO knots. IAS/MACH REFERENCE BUG Indicates the IAS or Mach reference selected on the pilot's instrument remote controller. Displayed in cyan. MACH DISPLAY Displays Mach number at or above 0.45 Mach. Display is removed below 0.40 Mach. Resolution is 0.002 Mach. The colour of the Mach display is the same as described for the IAS display. FMS SPEED BUG indicates the FMS reference speed when the flight director VNAV mode is selected. Displayed in magenta. IAS/MACK REFERENCE DISPLAY Provides a readout of the lAS/Mach reference bug with respect to the PILOTS AND COPILOT'S INSTRUMENT PANEL DADS - EFIS EADI Air Data Displays Figure 7 (Sheet 1) SECTION 11 Page 9 Apr 02/87 OPERATING MANUAL PSP 601A-6 IAS COMPARISON MONITOR ANNUNCIATOR Rashes (amber) for 10 seconds and then comes on steady to indicate a 5 knots or more difference between tne on-side and cross-side (AS sources, for greater than 2 seconds. The IAS comparison monitor function is inhibited at SO knots or less. VMO INDICATOR Indicates the aircraft maximum operating velocity (VMO}. Displayed in red. AoLl. DISPLAY Ots&toys the selected amurfe for the flight atrector A 5 ?L mode, nartge & from 0 to 60,000 feet, selectable in 100 foot increments. When the on-side EHSI and DADC are coupled to the master flight guidance computer, the Display and surrounding box are displayed in cyan. When the cross-side EHSI and DADC are coupled to the master FGC. the surrounding box is changed to yellow. IAS DISPLAY AND SCALE The IAS display and scale provide an indication of the IAS from 40 to 450 knots. Below 40 knots the IAS display is removed. When the IAS data source is on-side the IAS display is green. When the source is cross-side, the cSsptay is yeBow. When the IAS exceeds the rafetence IAS. in the fSght director FLC or VFLC modes, by ?5 knots. the display is amber. When the IAS exceeds VMO. as indicated by the VMO indicator, the olspiay is red. Whan the IAS acceleration trend vector exceeds the VMO, the display is smber. IAS REVISION ANNUNCIATOR Indicates a cross-side transfer of IAS data. An amber boxed XIAS is displayed on the receiving side and an amber boxed green IAS is displayed on the transferring side NOTES 1 When IAS data from the coupled-side DADC is not vafid, an IAS related displays are removed and a ted boxed IAS annunciation is displayed. 2 When the altitude preselect "function faSs the ASEL display is removed and a red boxed ASEL is displayed. DADS - EFIS EADI Air Data Displays Figure 7 (Sheet 2) SECTION 11 Page 10 Apr 02/87 OPERATING MANUAL PSP 601A-6 PILOT'S INSTRUMENT REMOTE CONTROLLER IAS/MACH PUSH CHG CONTROL/ SWITCH Rotating the IAS/MACH PUSH CHG control/switch causes the IAS or Mach references displayed on the pilot's and copilot's EADls, to change. Pressing the IAS/MACH PUSH CHG control/switch causes the IAS reference to change to a Mach reference and vice versa. The push-to-change function is inhibited when the aircraft is on the ground. GLARESHIELD (PILOT'S SIDE) ALT SEL CONTROL Rotating the ALT SEL control causes the ASEL displays, on the pilot's and copilot's EADls to change. COPILOTS INSTRUMENT REMOTE CONTROLLER GLARESHIELD (COPILOTS SIDE) DADS - EFIS Instrument Remote Controllers Figure 8 SECTION 11 Page 11 Apr 02/87 OPERATING MANUAL PSP 601A-6 IRS1 DME: NAV 1 - ADF1 PILOT'S SIDE EADI CENTRE EHSi DISPLAY CONTROLLER Q O ?O PILOTS SYMBOL SENERATORl IRS1 - DME1- NAV1- ADF1 - WXINSTRUMENT REMOTE CONTROLLER MFD MFD CONTROLLER 00O甇D 皁g?? MFD SYMBOL GENERATOR ASCB COPILOTS SIDE e~L>: K>桲^A V EHSI DISPLAY CONTROLLER n M i i n Q O O O IRS 2 DME 2 NAV2 AOF2 RA COPILOTS SYMBOL GENERATOR IRS 2 OME2 NAV2 ADF2 RA WX TO/FROM FMS 1 AND FMS 2 IRS 1 AND IRS 2. AFCS 1 AND AFCS 2 AND DADS 1 AND DADS 2 INSTRUMENT REMOTE CONTROLLER EFIS - Simplified Block Diagram Figure 9 SECTION 11 Page 12 Apr 02/87 OPERATING MANUAL PSP 601A-6 FLIGHT DIRECTOR MODE ANNUNCIATORS DECISION HEIGHT ANNUNCIATOR ROLL SCALE VMO INDICATOR FLIGHT DIRECTOR COMMAND CUE IAS DISPLAY IAS ACCEL TREND VECTOR IAS SCALE FMS SPEED BUG IAS/MACH REFERBSICE BUG MACH DISPLAY MARKER BEACON ANNUNCIATOR AUTOPILOT ANNUNCIATOR ALTITUDE PRESELECT DISPLAY VERTICAL TRACK ALERT ANNUNCIATOR VERTICAL NAVIGATION POINTER GUDESLOPE POINTER AIRCRAFT SYMBOL LOCALIZER POINTER/ RISING RUNWAY RADIO ALTITUDE DISPLAY DECISION HEIGHT DISPLAY INCLINOMETER PILOTS AND COPILOTS INSTRUMENT PANELS EFIS - EADI Normal Displays Figure 10 SECTION 11 Page 13 Apr 02/87 OPERATING MANUAL PSP 601A-6 ATTITUDE FAILURE ANNUNCIATOR ATTITUDE FAILURE FLIGHT DIRECTOR FAILURE ANNUNCIATOR FLIGHT DIRECTOR FAILURE PILOTS AND COPILOT'S INSTRUMENT PANELS EFIS - EADI Failure Warning Annunciators Figure 11 (Sheet 1) SECTION 11 Page 14 Apr 02/87 cftanerujer OPERATING MANUAL PSP 601A-6 IAS FAILURE ANNUNCIATOR LOCALIZER FAILURE ANNUNCIATOR ASEL FAILURE ANNUNCIATOR CROSS-SIDE DATA FAILURE ANNUNCIATOR GLIDESLOPE FAILURE ANNUNCIATOR RADIO ALTITUDE FAILURE ANNUNCIATOR IAS, ALTITUDE PRESELECT. CROSS-SIDE DATA. GLIDESLOPE. VERTICAL NAVIGATION, RADIO ALTITUDE AND LOCALIZER FAILURES SYMBOL GENERATOR INTERNAL FAILURE ANNUNCIATOR SYMBOL GENERATOR INTERNAL FAILURE EFIS - EADI Failure Warning Annunciators Figure 11 (Sheet 2) SECTION 11 Page 15 Apr 02/87 OPERATING MANUAL PSP 601A-6 CAT 2 INVALID ANNUNCIATOR FOOTS AND COPILOTS INSTRUMENT PANELS EFIS - EADI Category 2 Annunciator Figure 12 SECTION 11 Page 16 Apr 02/87 OPERATING MANUAL PSP 601A-6 IAS COMPARISON MONITOR ANNUNCIATOR LOCALIZER COMPARISON MONITOR ANNUNQATOR ATTITUDE COMPARISON MONITOR ANNUNCIATOR GLIDESLOPE COMPARISON MONITOR ANNUNCIATOR PILOTS AND COPILOTS INSTRUMENT PANELS EFIS - EADI Comparison Monitor Annunciators Figure 13 SECTION 11 Page 17 Apr 02/87 OPERATING MANUAL PS? 601A-6 IAS REVERSION ANNUNCIATOR SG REVERSION ANNUNCIATOR IRS REVERSION ANNUNCIATOR PILOTS AND COPILOT'S INSTRUMENT PANELS EFIS - EADI Reversionary Source Annunciators Figure 14 SECTION 11 Page 18 Apr 02/87 ctvanenaer OPERATING MANUAL PSP601A-6 WIND VECTOR DISPLAY HEADING SELECT BUG FORE LUBBER LINE HEADING SOURCE ANNUNCIATOR COURSE SELECTS DESIRED TRACK DISPLAY BEARING POINTS? NO. 1 NAVIGATION* SOURCE ANNUNCIATOR COURSE PRESELECT SOURCE ANNUNCIATOR BEARING POINTER SOURCE ANNUNCIATOR COURSE DEVIATION 8AR FMS FMS MESSAGE DRIFT ANNUNCIATOR BUG TARGET ALERT ANNUNCIATOR DISTANCE DISPLAY WAYPOINT/DME RECIPROCAL IDENTIFIER COURSE PRESELECT POINTER RECIPROCAL COURSE POINTER COURSE 昉RESELECT POINTER GLIDESLOPE POINTER COURSE SELECT/DESIRED TRACK POINTER ?TO-FROM POINTER "AIRCRAFT SYMBOL COURSE PRESELECT DEVIATION BAR TIME-TO-GO DISPLAY PILOTS AND COPILOTS INSTRUMENT PANELS EFIS - EHSI Full Compass Mode Figure 15 SECTION 11 Page 19 Apr 02/87 OPERATING MANUAL PSP 601A-6 PARTIAL HEADING DIAL COURSE/DESIRED TRACK DISPLAY OFF SCALE ARROW NAV SOURCE ANNUNCIATOR COURSE PRESELECT ANNUNCIATOR BEARING POINTER SOURCE ANNUNCIATOR DISTANCE DISPLAY WIND VECTOR DISPLAY COURSE SELECT/ DESIRED TRACK POINTER FORE HEADING FMS LUBBER SOURCE MESSAGE UNE ANNUNCIATOR ANNUNCIATOR TARGET ALERT ANNUNCIATOR HEADING SELECT DISPLAY HEADING SELECT BUG FMS DRIFT BUG COURSE PRESELECT POINTER GUDESLOPE POINTER COURSE PRESELECT DEVIATION BAR GROUND SPEED DISPLAY WAYPOINT/DME IDENTIFIER BEARING POINTS NO. 1 COURSE AIRCRAFT TO/FR DEVIATION SYMBOL ANNUNCIATOR BAR PILOTS AND COPILOTS INSTRUMENT PANELS EFIS - EHSI ARC Mode Figure 16 SECTION 11 Page 20 ApT 02/87 ctiauenejer COURSE SELECT DISPLAY VOR STATION SYMBOL SELECTED COURSE UNE OPERATING MANUAL PSP 601A-6 SELECTED BEARING NO. 2 DISPLAY CROSS-TRACK DISTANCE DlSP! * v VOR NAVIGATION SOURCE VOR BEARING WAYPOINTS STATION SYMBOLOGY VOR ONLY - O ?MS ONLY) VOR/DME- ? DME ONLY -<? (FMS ONLY) CROSS-TRACK DISTANCE DISPLAY FMS NAVIGATION SOURCE WAYPOINT LEG TO WAYPOINT IDENTIFIER WAYPOINT FLIGHT LEVEL PILOTS AND COPILOTS INSTRUMENT PANELS EFIS - EHSI MAP Mode Figure 17 SECTION 11 Page 21 Apr 02/87 MODS ANNUNCIATOR OPERATING MANUAL PSP 601A-6 ALERT ANNUNCIATOR RANGE RING WX RETURN DISPLAY RANGE ANNUNCIATOR PILOTS AND COPILOTS INSTRUMENT PANELS EFIS - EHSI Weather Radar Display Figure 18 SECTION 11 Page 22 Apr 02/87 OPERATING MANUAL PS? 601A-6 IRS FAILURE ANNUNCIATOR / t IOI CRS 349 ^ \ V o ? R -=-? 1 r .xXM'i'/'/,. HDG 340 v? ir DME ?',/? s ?\ \ ^ 180 RNE I TTG 34.5 o V^z J X^LS HEADING FAILURE NAV SOURCE FAILURE ANNUNCIATOR /Z N j Q MAG V HDG 340 = > GLIDESLOPE FAILURE ANNUNCIATOR NAVIGATION SOURCE AND GUDESLOPE FAILURE PILOT'S AND COPILOTS INSTRUMENT PANELS EFIS - EHSI Failure Warning Annunciators Figure 19 SECTION 11 Page 23 Apr 02/87 OPERATING MANUAL PSP 601A-6 IRS HEADING COMPARISON MONITOR ANNUNCIATOR PILOTS AND COPILOTS INSTRUMENT PANELS EFIS - EHSI Comparison Monitor Annunciator Figure 20 SECTION 11 Page 24 Apr 02/87 OPERATING MANUAL PSP 601A-6 SG REVERSION ANNUNCIATOR IRS REVERSION ANNUNCIATOR PILOT'S AND COPILOTS INSTRUMENT PANELS EFIS - EHSI Reversionary Source Annunciators Figure 21 SECTION 11 Page 25 Apr 02/87 OPERATING MANUAL PS? 601A-6 COURSE SELECT/ DESIRED TRACK DISPLAY NAVIGATION SOURCE ANNUNCIATOR $ TO/!=R A*NEL,rrtClATC=: COURSE DEVIATION COURSE POINTER SELECT/DESIRED TRACK POINTER GLIDESLOPE POINTER HEADING SELECT DISPLAY HEADING SELECT BUG MOTE PILOTS AND COPILOTS INSTRUMENT PANELS The composite cfisptey is a reversionary mode, used to provide both essential attitude cfirector and horumiuri situation information on one display, in the event that an electrooic OBptoy unit fafls. EFIS - Composite Display Figure 22 SECTION 11 Page 26 Apr 02/87 OPERATING MANUAL PSP 601A-6 DISTANCE AND COURSE TO DESIGNATOR HEADING DIAL LUBBER LINE TUNED VOR/DME NAVIGATION SOURCE ANNUNCIATOR VOR/DME NAVAID SYMBOL ^ ^ VOR/DME ^ ^ D M E ONLY O VORONLY AIRPORT IDENTIFIER RANGE RING DESIRED TRACK LINE WEATHER RADAR MODE DESIGNATOR LATITUDE/ LONGITUDE DISPLAY TGT/VAR ANNUNCIATOR AIRCRAFT SYMBOL -TO** WAYPOINT DISPLAY ETA TTG IN OR IN GMT HR:MN DISTANCE T O T O ' WAYPOINT DISPLAY DESIGNATOR DISPLACEMENT LINE CROSS-TRACK DEVIATION DISPLAY CENTRE INSTRUMENT PANEL EFIS - MFD MAP Mode Figure 23 SECTION 11 Page 27 Apr 02/87 OPERATING MANUAL PSP 601A-6 DISTANCE AND COURSE TO DESIGNATOR AIRCRAFT SYMBOL TUNED VOR/DME SELECTED NAV SOURCE MAG ANNUNCIATOR -NORTH-UP* IDENTIFIER DISPLACEMENT LINE DESIGNATOR RANGE AIRPORT ANNUNCIATOR WEATHER RADAR MODE TGT/VAR ANNUNCIATOR TO" WAYPOINT DESIGNATOR LATITUDE/ LONGITUDE DISPLAY ETA TTG IN OR IN GMT HRrMN RANGE RING WAYPOINT DISTANCE TO T O " WAYPOINT CENTRE INSTRUMENT PANEL EFIS - MFD PLAN Mode Figure 24 SECTION 11 Page 28 Apr 02/87 cttanenefer OPERATING MANUAL PSP 601A-6 GSPD/TTG PUSHBUTTON Alternately selects ground speed (GS) or time-to-go (TTG) for display. /< WX PUSHBUTTON Selects weather radar returns for display in partial compass format. MAP PUSHBUTTON Selects display of active waypornts and VOR/DME ground station positions on partial compass display. ET PUSHBUTTON Selects elapsed time display instead of GS/TTG display. V/L PUSHBUTTON Selects between the on-side and cross-side SRN systems (see note). FULL/ARC PUSHBUTTON Selects full compass (360 degrees of heading} or partial compass (90 degrees of heading) format for display. BRG O KNOB Selects the bearing source for the No. 1 bearing pointer on the EHSl. ADl DIM (OUTER) CONTROL Adjusts the brightness of the EAOI display. When set to OFF. the EHSl displays a composite EAOI and EHSl. FMS PUSHBUTTON Selects between the on-side and cross-side LRN system (FMS). BRG O KNOB Selects the bearing source for the No. 2 bearing pointer on the EHSl. WX DIM (INNER) CONTROL Adjusts the brightness of the weather radar returns on the EHSl. OH/TST (INNER) CONTROL Rotating the control adjusts the decision height display on the EAOI. When pressed activates the test mode. HSl DIM (OUTER) CONTROL Adjusts the brightness of the EHSl display. When set to OFF. the EADl displays a composite EAOI and EHSL PILOT'S AND COPILOT'S SIDE PANELS NOTE SRN systems are the VHF navigation system and the DME system. EFIS - Display Controller Figure 25 SECTION 11 Page 29 Apr 02/87 OPERATING MANUAL PSP 601A-6 HDG PUSH SYNC PUSHBUTTON When rooted, moves the heading bug on the p8ot's EHSl. When pressed, causes the heading bug to synchronize to the aircraft heading. IAS/MACH PUSH CHG CONTROL/ SWITCH When rotated, adjusts the lAS/Mach reference on the pilot's and copilot's EAOis. When pressed. change the IAS reference to the Mach reference or vice versa. The push-to-change function is inhibited with the aircraft on the ground. CRS PUSH OCT CONTROL/ SWITCH When rotated, rnoves the course select pointer on the associated EHSl. When pressed, causes the course pointer to indicate the 2ero deviation course to the tuned VOR station. When an FMS source is selected, rotating the control causes the preselect course pointer to move. ALT SEL CONTROL When rotated, adjusts the AScL display on the pilot's and copilot's EADJs. HOG PUSH SYNC PUSHBUTTON When rotated, moves the heading bug on the copdot's EHSl. When pressed, causes the heading bug to synchronize to the aircraft heading. GlARESHiELD EFIS - Instrument Remote Controllers Figure 26 SECTION 11 Page 30 Apr 02/87 OPERATING MANUAL PSP 601A-6 WX PUSHBUTTON Selects the weather radar information for display on the MFD indicator. NORM PUSHBUTTON Selects checklist index page for display on MFD indicator. SRC PUSHBUTTON Selects long range navigation source for MAP and PLAN modes. MAP/PLAN PUSHBUTTON Alternately selects MAP or PLAN format for MFD indicator display. VOR PUSHBUTTON Selects VOR/DME information for display on MFD indicator. INC/DEC RNG CONTROL Increases or decreases the range display on the MFD indicator. EMER PUSHBUTTON Selects emergency checklist index page for display on MFD indicator. SKP PUSHBUTTON Allows skipping of designator or active lines. DAT PUSHBUTTON Allows additional long range navigation information to be added to the MAP or PLAN mode display ENT PUSHBUTTON Enters designator as a waypotm. checks off a line or selects an index line item for display. RCL PUSHBUTTON Recalls designator to home position or recalls lowest numbered skipped tine in a checklist. PAG PUSHBUTTON Advances the page count and places the active line selection at first line of the page. CENTRE PEDESTAL EFIS - MFD Controller Figure 27 SECTION 11 Page 31 Apr 02/87 OPERATING MANUAL PSP 601A-6 COMP WON SWITCH/LIGHT Comes on (amber) to indicate that a difference exists between one of the on-side and cross-side sources. The out-of -tolerance source is indicated on the EADl. When pressed, resets the comparison circuits. SG REV SWITCH/UGHT When pressed, selects the cross-side symbol generator as a back-up when the on-side symbol generator fafls. IAS REV SWITCH/LIGHT When pressed, selects the cross-side OADC as a back-up IAS source when the on-side source fails. IRS REV SWTTCH/UGHT When pressed, selects the cross-side IRS as back-up when the on-side IRS source fails. FD REV SWITCH/LIGHT When pressed, selects the cross-side flight guidance computer (FGC) as a back-up flight director when the onside FGC fails. PILOTS AND COPILOTS INSTRUMENT PANELS EFIS - Remote Switch/Lights Figure 28 SECTION 11 Page 32 Apr 02/87

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ericgyf 发表于 2011-6-28 20:24:31

回复 1# 航空的帖子

CRJ200 Flight Deck Book

ericgyf 发表于 2011-6-28 20:24:43

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CRJ200 Flight Deck Book

bocome 发表于 2011-7-31 07:40:37

庞巴迪挑战者飞行仪表

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