BMS F-16C/D 4.34 Flight Manual page 198

T.O. BMS1F-16CM-1
The subsystems are identified by one of the following mnemonics:
•
AMUX
•
BLKR
•
BMUX
•
CADC
•
CMDS
•
DLNK
•
DMUX
•
EGI
•
ENG
•
FCC
•
FCR
•
FDR
•
FLCS
•
FMS
•
GPS
•
HUD
•
IFF
•
IDM
•
INS
•
MC04
•
MC13
•
MMC
•
MFDS
•
MSL
•
NVP
•
RALT
•
RWR
•
SMS
•
TCDS
•
TCN
•
TGP
•
UFC
•
TOF
•
LAND
When a fault occurs the PFL is displayed on the TEST page and the corresponding test number
(3 digits) is displayed in the second column. The test number is the key to identify the subsystem that
failed. Refer to section 3.4.3. for a list of test numbers.
In some cases the PFL might be the same and only the different test number will provide additional
information about the exact cause of the malfunction.
For instance, a NVP COMM FAIL might have 2 causes: number 14 refers to a failure of the NVP due
to INS, while number 15 refers to NVP failure because of a radar altimeter problem. In this particular
case the pilot, knowing the exact cause of the problem, can quickly remedy it by checking the relevant
system.
BMS 4.34 Dash 1
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A-multiplex bus
Interference blanker unit
B-multiplex bus
Central air data computer
Countermeasures dispensing set
Data modem
D-multiplex bus
Embedded Global Positioning System / Inertial Navigation Set
Engine
Fire control computer
Fire control radar
Crash survivable flight data recorder
Digital flight control system (DFLCS)
Fuel measurement system
Global positioning system
Head-Up display
Advanced identification friend or foe
Improved Data Modem
Inertial navigation set
Modular Mission Computer
Modular Mission Computer
Modular Mission Computer
Multifunction display set
Missile slaving loop
Navigation Pod
Radar altimeter
Radar warning receiver
Stores management set
Threat Adaptive Countermeasures Dispensing Set
TACAN
Targeting Pod
Upfront control set
Pseudo fault recording the take-off time.
Pseudo fault recording landing time.
BMS 4.34 Change 2.00
Page: 198