COMPONENT MAINTENANCE MANUAL
AVIATION RECORDERS
Model FA5000
Initital Issue Page 5
Sep. 30/11
Description and Operation
23–70
−
40
Use or disclosure of information on this sheet is subject to
the restrictions on the cover page of this document.
FA5001 CVDR
DATA LINK
VIDEO
FDR
CVR
CAM
PREAMP
POWER
SUPPLY
Integral
BITE
BEACON
VIDEO
GSE
CSMU
A/C SYSTEMS
OMS
ARINC 429
TECHOMETER
MIC 3
MIC 2
MIC 1
CAM
HEADSET
AIRCRAFT
POWER
ATE
J1
J2
ATC DIGITAL INPUT
FDR DATA INPUT ARINC 717
FDR DATA OUTPUT ARINC 717
FDR INPUT DATA RATE PROGRAM PINS
ARINC 429 OUTPUT
ARINC 429 INPUT
ROTOR SPEED
CHANNEL 3 INPUT
CHANNEL 2 INPUT
CHANNEL 1 INPUT
AREA MICROPHONE
CAM INPUT ATTENUATION
FDR MAINTENANCE FAULT
FDR STATUS
CVR MAINTENANCE FAULT
AUDIO OUTPUT (MONITOR)
PUSH TO TEST
ERASE CVR INPUT
+28 VDC PRIMARY
+28 VDC SECONDARY
+28 VDC RETURN, PRI/SEC
ATE ETHERNET TX RX
ATE PRESENT
VIDEO IN
35/36
33/41
34/42
29/30
27/28
32/40
51/52
23/24
15/16
8/9
38/39
48/49
50/54
18
19
17
4/10
47
5/11
12
CESSATION OF RECORDING
55
44
43/53
1/2
3
6/7
25/26
VIDEO
(Ethernet)
(PAL B)
RIPS
Charger
with
Figure 3. CVDR Block Diagram
Figure 3 – Recorder Data Flow Diagram shows the data flow diagram for the Model
FA5000. The software data flow diagram shows the relationship between the hardware
The document reference is online, please check the correspondence between the online documentation and the printed version.
