AVIONICS Flashcards
Failure of the ( ) IC 600 is displayed by two large red X’s on DU 3 and DU 4.
Right. PTM Pg. 16-6
Failure of the ( ) IC 600 is displayed by two large red X’s on DU 1 and DU 2.
Left. PTM Pg. 16-6
In the event of an IC 600 ( ), the appropriate checklist to run can be found using the table of contents pages, Instrument/Avionics category of the amber section in the QRH.
Failure. QRH Pg. A-4
Failure of ( ) is indicated by red X’s over the airspeed and altitude tapes on DU 1.
ADC 1 . PTM Pg. 16-30
Failure of ( ) is indicated by red X’s over the airspeed and altitude tapes on DU 4.
ADC 2. PTM Pg. 16-30
In the event of ( ) failure, the appropriate checklist to run can be found using the table of contents pages, Instrument/Avionics category of the amber section in the QRH.
ADC. QRH Pg. A-5
Failure of ( ) is indicated by ATT FAIL printed on a cyan ADI (‘blue ball of death’), a compass rose with a red X and the words HDG FAIL displayed on DU 1.
AHRS 1. PTM Pg. 16-35
Failure of ( ) is indicated by ATT FAIL printed on a cyan ADI (‘blue ball of death’) a compass rose with a red X and the words HDG FAIL displayed on DU 4.
AHRS 2. PTM Pg. 16-35
In the event of ( ), the appropriate checklist to run can be found using the table of contents pages, Instrument /Avionics category of the amber section in the QRH.
AHRS failure. QRH Pg. A-5
The QRH title for AHRS 1 or AHRS 2 failure is “Loss of PFD ( ) or ( ) Displays.”
Attitude or Heading. QRH Pg. A-5
If the auto-pilot does a self-monitoring disconnect, a red AP will be displayed on the PFDs along with a ( ) aural alert.
Cavalry charge. PTM Pg. 16-86
To extinguish a red AP and/or turn “OFF the ‘cavalry charge’ aural alert, either aircrew can depress the red ( ) button on the control yokes.
Control Wheel Master Switch (MSW). PTM Pg. 16-86
Activating the ( ) switch on either yoke will disconnect the auto pilot.
Trim. PTM Pg. 16-88
Depressing and holding the red Control Wheel Master Switch (MSW) button on either control yoke disconnects the auto pilot and yaw dampener along with:
Interrupting all trims, Rudder Boost and
Pitch Trim Bias. PTM Pg. 15-4 and 16-88
The ( ) can display engine data and navigation data along with radio and transponder information.
RMU. PTM 16-14
To display engine data on the RMU, select the PGE button, then depress the line select key next to:
ENGINE. PTM Pg. 16-14
To display navigation data on the RMU, depress the PGE button, then depress the line select key next to:
NAVIGATION. PTM Pg. 16-14
The Clearance Delivery Head (CDH) can be powered with both aircraft main ship batteries OFF by using the:
Radio Control Hot Bus switch. PTM Pg. 16-26
The Clearance Delivery Head (CDH) is an alternate way to tune:
Comm 1. PTM Pg. 16-26
To display FMS navigation information data, such as an RNAV/GPS approach on the PFD, select the ( ) button on the display controller.
FMS. PTM 16-41
To display ILS information on the PFD, select the ( ) button on the Display Controller.
NAV. PTM Pg. 16-41
To switch the display on the PFD between ILS 1 and ILS 2, ( ) the NAV button on the display controller.
NAV. PTM Pg. 16-41
If there is a mis-compare between AHRS 1 and AHRS 2 in pitch and/or roll, an ATT, PIT, or ROL will be posted on both ( ).
ADIs on the PFDs. PTM Pg. 16-44
If there is a mis-compare between AHRS 1 and AHRS 2 in heading, an amber ( ) will be posted just above the compass rose on both PFDs.
HDG. PTM Pg. 16-44
