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庞巴迪挑战者605公务机机组操作手册 CL605-飞行仪表 FLIGHT_INSTRUMENTS(3)

时间:2011-10-28 11:48来源:蓝天飞行翻译 作者:公务机 点击:
  
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:
.
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 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:
.
Attitude ADI;

.
Airspeed/Mach;

.
AOA;

.
Altitude;

.
 
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