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Figure 11−10−11 MFD Direct Access TR/WX Menu 11−10−10
Figure 11−10−12 MFD with a Chart (Full Window) 11−10−12
Figure 11−10−13 Flight Control Panel (FCP) 11−10−13
Figure 11−10−14 BARO Knob 11−10−13
Figure 11−10−15 Reversionary Panel 11−10−14
Figure 11−10−16 Pitot Static System 11−10−15
Figure 11−10−17 PFD Airspeed Information 11−10−17
Figure 11−10−18 PFD REFs Speed Indications 11−10−19
Figure 11−10−19 Overspeed/Low-Speed Cues 11−10−21
Figure 11−10−20 AOA Indicator 11−10−22
Figure 11−10−21 BARO SET Menu/BARO Knob 11−10−23
Figure 11−10−22 Altitude Display and Readout 11−10−24
Figure 11−10−23 Altitude Alert Operation 11−10−25
Figure 11−10−24 BARO MIN Display 11−10−26
Figure 11−10−25 Radio Altitude (RA) Displays 11−10−27
Figure 11−10−26 RA MIN Display 11−10−28
Figure 11−10−27 Vertical Speed Display 11−10−29
Figure 11−10−28 Air Data Flags/RA Flag/Negative Altitude Indication 11−10−30
Figure 11−10−29 ADC Reversionary Annunciation 11−10−30
Figure 11−10−30 Aircraft Symbols 11−10−31
FLIGHT INSTRUMENTS
Table of Contents
Vol. 2 11−00−3
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
Page
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 11−10−31 Normal Attitude Display 11−10−32
Figure 11−10−32 PFD Declutter 11−10−34
Figure 11−10−33 Heading Information 11−10−36
Figure 11−10−34 Attitude and Heading Failure Flags 11−10−37
Figure 11−10−35 IRS Reversionary Annunciation (Dual IRS Configuration) 11−10−37
Figure 11−10−36 IRS Reversionary Annunciation (Triple IRS Configuration) 11−10−38
Figure 11−10−37 PFD Navigation Formats 11−10−40
Figure 11−10−38 MFD Navigation Formats 11−10−41
Figure 11−10−39 Bearing Pointer Menu 11−10−44
Figure 11−10−40 Navigation Display Indications 11−10−45
Figure 11−10−41 Navigation Indications on ADI and FLT PATH VCTR Menu
Selection 11−10−46
Figure 11−10−42 Navigation Source Warning Flags 11−10−47
Figure 11−10−43 Comparator Annunciations 11−10−50
Figure 11−10−44 Reversion Normal Switch Selections 11−10−51
Figure 11−10−45 Reversion L−PFD Failure 11−10−52
Figure 11−10−46 Reversion R−PFD Failure 11−10−52
Figure 11−10−47 Reversion L−MFD Failure 11−10−53
Figure 11−10−48 Reversion R−MFD Failure 11−10−54
Figure 11−10−49 ISI Alignment (Attitude) 11−10−55
Figure 11−10−50 ISI Functions 11−10−56
Figure 11−10−51 Standby Magnetic Compass 11−10−57
Figure 11−10−52 Clock/Chronometer (GPS-Synchronized) 11−10−58
FLIGHT INSTRUMENTS
Table of Contents
Vol. 2 11−00−4
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
Page
GENERAL
The flight instruments chapter includes the electronic flight instruments system (EFIS), pitot static &
air data system, inertial reference system (IRS), standby flight instruments and clock/chronometer.
The Challenger 605 is equipped with an electronic flight instruments system (EFIS),which is
comprised of the following:
• Two adaptive flight displays to act as primary flight displays (PFDs);
• Two adaptive flight displays to act as multi-function displays (MFDs);
• Two display control panels (DCPs);
• Two cursor control panels (CCPs);
• One reversion panel; and
• Two BARO knobs.
EFIS interfaces with the integrated avionics processing system (IAPS). The IAPS is the focal point of
information flow for the entire aircraft. In addition to performing the integration functions required to
connect the various aircraft systems, the IAPS contains the flight control computers (FCCs), flight
management computers (FMCs), and maintenance diagnostic computer (MDC). Other systems
provide information to the EFIS for display as conventional flight instruments. This includes the air
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庞巴迪挑战者605机组操作手册 CL605-FLIGHT_INSTRUMENTS(2)
