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AVIONICS SYSTEM
COCKPIT VOICE RECORDER (CVR)
(FL-30, FL-52, FL-62, FL-63, FL-65, FL-73, FL-84, FL-87, FL-114 AND
AFTER)
Delivered by Hawker Beechcraft Corporation or Installed by Kit 130-3407-1:
Airplanes equipped with an L3 Communications Fairchild Model FA2100 cock-
pit voice recorder have either a 30-minute (Model 2100-1010) or a 2-hour
(Model 2100-1020) capacity.
The CVR system consists of a cockpit voice recorder, a control unit, an area
microphone, and an impact switch. Electrical power to the recorder is provided
by the triple-fed bus. The recorder and impact switch are located in the aft avi-
onics bay behind the pressure bulkhead. The control unit is located in the cock-
pit pedestal. The area microphone is located in the leading edge of the
glareshield to the right of the fire extinguisher switch.
Input to the CVR recorder comes from the following four sources:
• Cabin Pager (What the pilot or copilot transmit over the cabin pager.)
• Copilot’s Audio (What the copilot hears or transmits over the boom mic,
hand mic, or oxygen mask mic.)
• Pilot’s Audio (What the pilot hears or transmits over the boom mic, hand
mic, or oxygen mask mic.)
• Area Mic
The CVR recorder is capable of reproducing the recorded audio data in one of
the following formats:
Both CVRs will reproduce the last 30 minutes of audio recorded by the above
channels in a high quality format on four separate channels. Additionally, when
CVR Model 2100-1020 is installed, the last 2 hours of audio recorded by the
above channels may be reproduced in a standard quality format on two chan-
nels, which contain the following material:
• A combination of the pilot, copilot, and cabin pager audio data.
• Area Mic audio data.
The control unit contains the test switch, erase switch, indicating meter, and
headset jack. The test switch and indicating meter provide a test of the recorder.
The headset jack provides a means of monitoring all audio data that is being
input to the CVR recorder to ensure that the recorder is receiving the proper
audio signals. Pressing the test switch should result in the following indications
if the recorder is functioning properly:
FAA Approved
Revised: March, 2010
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