EasyManua.ls Logo

L3 Communications FA2100 - Voice Data Interface Characteristics

L3 Communications FA2100
360 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
COMPONENT MAINTENANCE MANUAL
AVIATION RECORDERS
FA2100CVR
Page 9
Nov. 01/98
Description and Operation
23–70–04
The Push-To-Test signal is activated when the TEST pushbutton on the associated
control unit is pressed. During this time, a 620 Hz to 660 Hz signal is generated
within the FA2100 which is used to test the circuitry of all the audio channels. In a
successful test, the FA2100 Recorder provides a TEST INDICATOR signal which
lights the green TEST indicator mounted on the front panel of the S151/S161,
S152/S162, and S251/261 Control Units.
NOTE
: For all P/N: 2100102502/2100102602/2100102702, no
test tone will be heard and the Monitor Output will be muted
during the test. After the test, if the Test Good tone is not
heard, then the 2100CVR has failed and the test. Monitor
Output will resumes in both a passed and failed test.
NOTE
: The Model 21001025XX, when used with the S161139001
Control Unit, does not have a LED test indicator present. Ho-
wever, the audible test tone is still present.
D. Voice Data Interface Characteristics
The FA2100 CVR is used in an ARINC 557/757A configuration, with interface to the air-
craft provided through a 57-pin DPXB rear panel connector. The Reference Signal, as
required by ED-56A & ED112, is defined as an input signal with a frequency of 1 kHz at
an input level of 3 Vrms for Channels 1, 2, and 3, and 2 Vrms for Channel 4. The Audio
input sensitivity level is .05 Vrms 3 Vrms for Channels 1, 2, and 3, and .02 2 Vrms for
Channel 4.
The Model FA2100 CVR provides for four audio inputs which are connected as fol-
lows:
Channel 1 – Cockpit Spare Audio Input (3rd crew member CAA)
Channel 2 – Co-Pilot’s Audio, Boom, Mask, and Hand-Held Microphone Input
Channel 3 – Pilot’s Audio, Boom, Mask and Hand-Held Microphone Input
Channel 4 – Cockpit Area Microphone (CAM) Input
These audio signals are applied through the rear connector to the Aircraft Interface
PWA, then are digitally converted into 16Bit words, compressed and stored in
memory. Refer to Paragraph 5 for detailed pin-outs of the rear interface connector.
In the 02 FSK version of the FA2100 CVR, CH 1 or CH 3 may have an FSK GMT
input applied along with the standard audio signal.
May 21/1
3
Rev. 11 Page
9

Table of Contents

Related product manuals