Challenger 604 Miscellaneous Avionics

Front 1

The cockpit voice recorder (CVR) records

Back 1

All audio signals selected or transmitted through either audio panel and all ambient noise in the cockpit via an area microphone

Front 2

The cockpit voice recorder

Back 2

Records a minimum of 30 minutes of data in solid state memory

Front 3

The cockpit voice recorder

Back 3

Is equiped with an inertia switch which turns off power to the recorder after an impact

Front 4

The flight data recorder

Back 4

Records up to 25 hrs of data in solid state memory

Front 5

The FDR EVENT advisory message indicates

Back 5

The FDR set a date and time marker after the FDR EVENT button is pushed

Front 6

The flight data recorder

Back 6

Is supplied from the AC essential bus

And recieves data from the DCUs, IRUs and ADCs,

Front 7

Can any static wicks be missing or inoperative

Back 7

Yes, as authorized by the configuration deviation list (CDL): 1 may be missing from each aileron, and horizontal stabilizer. The static wick on the winglet must be operable.

Front 8

The HF radios share a common antenna (the leading edge of the vertical stabilizer) for transmission and reception. How are simultaneous HF radio transmissions prevented.

Back 8

When an HF radio transmits, the associated antennna coupler prevents coupling transmission of the opposite HF radio

Front 9

The failure of an RTU is indicated by

Back 9

RTU FAILURE is displayed in red on the affected RTU display

Front 10

The weather radar panel (only one) is located on the left side of the pedestal. Weather radar information is displayed on the right MFD by?

Back 10

Synchronizing the range selection on the right display control panel with the range shown on the left MFD and pushing WX.

Front 11

Automatic tilt control mode for the radar antenna is controlled how

Back 11

Controlled by pushing the integral PUSH AUTO button in the TILT knob, and is indicated by the "A" suffix on the antenna tilt readout shown in the weather radar mode line on the MFDs

Front 12

Lightning activicty detected by the optional lightning detection system may be shown independent of radar information by

Back 12

Turning off the radar and cycling the WX button until LX is shown on the MFD weather radar mode line

Front 13

Windshear alerting and obstacle and terrain clearance floor alerting is available with:

Back 13

Enhanced GPWS installations, only

Front 14

Alerting for hazardous terrain located one minute ahead of the airplane is shown

Back 14

On the MFD in FMS map format at 10 nm range in a bright yellow pattern along with the "Caution Terrain" aurl alert

Front 15

Hazardous obstacle or terrain alers displayed on the MFDs

Back 15

Pops-up regardless even if the TERR button has not been pushed

Front 16

Windshear encounters with decreasing headwind/increasing tailwind are indicated by

Back 16

Flashing red WINDSHEAR annunciation on the PFD, removal of the flight director and disengagement of the autopilot, and the "Windshear, Windshear, Wendshear" aural alert

Front 17

"Too Low Flaps" aural alert is

Back 17

Prevented/cancelled by selecting the guarded FLAP OVERRIDE SWITCH

Front 18

Nuisance aural alerts and MFD indications for hazardous obstacles or terrain are cancelled by

Back 18

Pushing either GPWS TERR INHIB swithchlight

Front 19

"Soft" alerts for descent below ILS glide slope

Back 19

May be cancelled by pushing either illuminated GND PROX/PULL UP switchlight

Are triggered when below the glideslope more than 1.3 dots

Are overridden by "hard" alerts when descending below 300ft RA and more than 2 dots low

Front 20

GPWS system testing is accomplished by

Back 20

Pushing either GND PROX/PULL UP switchlight while on the ground

Front 21

TCAS traffic may be displayed on the MFDs up to

Back 21

40 miles

Front 22

TCAS traffic information may be shown in which MFD formats?

Back 22

Only in Nav Sector, FMS Map, and TCAS formats at 50nm or less

Front 23

The TA ONLY mode is selected

Back 23

By the MODE line key on the TCAS main page on either RTU

Automatically during takeoff while below 1100 ft RA, and below 900ft RA during landing

Front 24

"Other" traffic symbols are inhibited from display

Back 24

By the TRAFFIC line key on the TCAS main page

Front 25

Evasive maneuvers associated with resolution advisories are

Back 25

Integrated with the vertical speed scale (green/red bands) with red TRAFFIC below the scale

Aurally annunciated over the speakers

Front 26

TCAS system testing is accomplished by

Back 26

TEST line key on the TCAS main page