COMPONENT MAINTENANCE MANUAL
AVIATION RECORDERS
Model FA5000
Rev. 03 Page 222
Feb. 27/13
FDR Function Testing & Fault Isolation
23–70
−
40
Use or disclosure of information on this sheet is subject to
the restrictions on the cover page of this document.
Table 204. Aircraft Interface Troubleshooting Chart (Continued)
Pin
ID
Signal Type
Signal Function
Failure Mode
Local Effect
End Effect
50
Discrete I/P
24dB CAM Input At
tenuation
The signal path is
open
No Effect
No Effect
50
Discrete I/P
24dB CAM Input At
tenuation
The signal path is
shorted
24dB CAM Input At
tenuation signal soft
ware receives continu
ous 24 dB attenuation
24dB CAM Input At
tenuation signal soft
ware receives continu
ous 24 dB attenuation
51
Differential
Analog ()
Rotor Speed Low
The signal path is
open
Rotor Speed Low sig
nal data is disrupted
Unable to record Rotor
Speed
51
Differential
Analog ()
Rotor Speed Low
The signal path is
shorted
Rotor Speed Low sig
nal data is disrupted
Unable to record Rotor
Speed
52
Differential
Analog (+)
Rotor Speed High
The signal path is
open
Rotor Speed High sig
nal data is disrupted
Unable to record Rotor
Speed
52
Differential
Analog (+)
Rotor Speed High
The signal path is
shorted
Rotor Speed High sig
nal data is disrupted
Unable to record Rotor
Speed
53
Power Rtn
28VDC Return
Primary; Connect to
DC Power Supply
Ground
The signal path is
open
Loss of 28VDC
Loss of CVDR function
ality
53
Power Rtn
28VDC Return
Primary; Connect to
DC Power Supply
Ground
The signal path is
shorted
No Effect
No Effect
54
Ground
CAM Input Attenu
ation Common
Ground
The signal path is
open
The CAM Input Attenu
ation (Common
Ground) signal fails to
enable Pins 20, 21 or
22
Degraded functionality
54
Ground
CAM Input Attenu
ation Common
Ground
The signal path is
shorted
No Effect
No Effect
55
Power
28VDC Input Primary
The signal path is
open
Loss of 28VDC
Loss of CVDR function
ality
55
Power
28VDC Input Primary
The signal path is
shorted
Loss of 28VDC
Loss of CVDR function
ality
Rev.04 Page 222
Mar. 21/14
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