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Radio Altitude FailureRadio Altitude Miscompare
The altitude above the terrain indication for approach and landing phases of operation is displayed on the Primary Flight Display (PFD).
GF0610_052
The Decision Height (DH) is displayed on the PFD when the minimums on the PFD controller is set to RAD.
The following systems receive RA information:
.
TCAS.
.
EGPWS.
.
FCUs.
.
DAUs (to display processors for PFD displays).
Refer to FLIGHT INSTRUMENTS Chapter 11, for additional information on RA indications.
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
The airplane wings and tail sections contain static wicks installed to discharge static electricity, reducing radio interference. They are installed at the following locations:
.
Winglets/wingtips and ailerons.
.
Elevators, rudder, vertical stabilizer, horizontal stabilizer and tail cone.
There are two parts to each static discharge assembly: the static discharger and the mounting base. If any are found missing during the walkaround, refer to the configuration deviation list of the AFM to verify if you can dispatch.
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
The Cockpit Voice Recorder (CVR) is a crash survivable recording device that simultaneously records four channels of audio data representing the cockpit acoustic environment. The system consists of:
.
CVR.
.
Microphone monitor/control panel.
.
Remote area microphone.
.
Impact switch.
CVR LOCATION
The CVR retains the most recent two hours of recorded information in memory. Input is received from each audio control panel and CVR area microphone. The CVR also receives digital data (GMT time) from DAU 4 to synchronize the CVR with the flight data recorder.
The CVR is mounted in the aft equipment bay. The microphone monitor/control panel is located in the flight compartment right side panel.
MICROPHONE MONITOR CONTROL PANEL
HEADSET Monitor Jack
Used to monitor tone transmissions during test and audio signals currently
STATUS DisplayERASE Push buttonTEST Push button
Pushing the ERASE
Illuminates as a function
Pushing the test button of test and/or failure. push button initiates a will activate the CVR
memory erase sequence internal self-test.
within the CVR.
Volume 2 Flight Crew Operating Manual
GF0610_056
Rev 3, Apr 25, 2005
An area microphone is mounted in the flight compartment overhead panel.
AREA MICROPHONE
GF0610_057
IMPACT SWITCH
The impact switch mounted in the aft avionics bay removes electrical power to the CVR when the airplane experiences an impact.
IMPACT SWITCH
GF0610_058
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