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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 Description Vol. 2 11.10.1
Oct 05/06
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:
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Two adaptive flight displays to act as primary flight displays (PFDs);
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Two adaptive flight displays to act as multi-function displays (MFDs);
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Two display control panels (DCPs);
.
Two cursor control panels (CCPs);
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One reversion panel; and
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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 data system and the inertial reference system (IRS).
FLIGHT INSTRUMENTS Description Vol. 2 11.10.2
Oct 05/06
Integrated Flight Instruments
Figure 11.10.1
FLIGHT INSTRUMENTS Description Vol. 2 11.10.3
Oct 05/06
Description
The two primary flight displays (PFDs) provide the pilots with the information necessary for the safe operation of the aircraft. They are integrated displays of attitude, air data, and navigation information. The PFD is divided into the following main areas:
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Attitude ADI;
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Airspeed/Mach;
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AOA;
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Altitude;
.
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