Flight Instruments Flashcards
Weather radar and terrain information can be overlaid on most MFD formats except:
TCAS
HSI
FMS Map
FMS Plan
Navaid Sector
HSI
FMS Plan
How is the MFD controlled when the Display Reversionary Panel switch in in the EICAS position?
With the Source Selector Panel
With the EICAS Control Panel
With the Air Data Reference Panel
With the Display Control Panel
With the EICAS Control Panel
If EICAS Display 1 becomes inoperative, moving the EICAS switch on the Source Selector Panel to ED2 will allow all EICAS pages to be viewed on EICAS Display 2.
True
False
True
The CRJ 700 has ____ sources of pitot/static information.
1
2
3
4
3
After the aircraft “captures” an altitude (i.e. levels off), hearing a “C-chord” and seeing the preselect altitude indicators flash yellow indicates that the aircraft is:
1000’ off of its altitude
200’ off of its altitude
300’ off of its altitude
500’ off of its altitude
200’ off of its altitude
If an airborne alignment of the Altitude Heading and Reference System occurs, the system will take __________ to re-align. The aircraft should remain in straight and level unaccelerated flight
35 - 55 seconds
15 - 45 seconds
1 - 2 minutes
10 - 35 seconds
10-35 seconds
The slip/skid indicator is located under the
Roll pointer
The aircraft symbol
Sky/ground raster
Vertical deviation display
Roll pointer
In LOC, one dot on the Lateral Deviation indicator indicates ______ of deflection.
0.5 degrees
1.0 degrees
1.5 degrees
2.0 degrees
1.0 degrees
The Integrated Standby indicator receives it power from the ____________ bus.
ADG
DC ESS
DC EMERG
DC BATT
DC BATT
An amber YD on the PFD indicates: (see Navigaton Displays in “Flight Instruments, Displays” tab)
That one of the yaw dampers has disengaged
That both of the yaw dampers are disengaged
That the FCC has detected a rudder mistrim
A fault has been detected in the yaw damp system
That both of the yaw dampers are disengaged
How are captured/active modes and armed modes displayed on the FMA (Flight Mode Annunciator)? (see Navigation Displays section of “Flight Insruments, Displays” tab):
Active modes are indicated in green, armed modes are indicated in white
Active and armed modes are indicated in white
Active modes flash continuously; armed modes are indicated in white
Active modes are in blue, armed modes are in white
Active modes are indicated in green, armed modes are indicated in white
An amber GS flag on the PFD indicates:
That the glideslope signal has been lost
That the glideslope has not been captured
That there is a difference between the glideslope indications
That the aircraft has deviated from the glideslope
That there is a difference between the glideslope indications
The standby attitude indicator has both localizer and glideslope indications:
TRUE
FALSE
True
Radio Altitude will be displayed on the PFD below:
2500 ft. AGL
2500 ft. MSL
1500 ft. AGL
1500 ft. AFL
2500 ft. AGL
The Mach number will be displayed when the aircraft speed increases above:
200kts
25kts
.5 mach
.45mach
.45mach