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MSK pushbutton legend appears boxed if there is
at least one equipment that is masked on the corresponding
iimctional group format.
3. Unit masking is performed by selecting equipment
and MSK pushbuttons. Any number of WRAS
may be selectedp rior to selecting the MSK pushbutton
in order to mask more than one failure at
the same time. Each equipment pushbutton legend
is boxed to indicate its selection and is unboxed if
reselected.O nly those items that remain selected
(i.e., boxed) before selecting the MSK pushbutton
will be masked. Unit unmasking is performed by
selecting the equipment and MSK pushbuttons
when the MSK pushbutton legend is boxed.
Figure 38-8. OBC Display Format Types
3843 ORIGINAL
NAVAIR 01.Fl4AAD-1
OBC ACRONYM
4DAC
4FCS
KCELEROMETER
‘ITCH ACTUATOR
?ITCH COMPUTER
PITCH SENSOR
ROLL ACTUATOR
ROLL COMPUTER
ROLL SENSOR
YAW ACTUATOR
YAW COMPUTER
YAW SENSOR
AICS
AICS-L or AICS-R
PROGRAMMER
FHF
ACRONYM
4DAC
SFCS
4FCAM
SFCPA
4FCPC
4FCPS
4FCRA
4FCRC
AFCRS
4FCYA
RFCYC
RFCYS
AICS
AILP
AIRP
DEFINITION
,Irbome Data Acquisition
:omputer
utomatic Flight Control
iystem
ur Inlet Control System
4lr Inlet Control (Left or
3lght)
REMARKS
ADAC failure, Fatigue and Engine
Monltorlng data records will no longer be
recorded on the DSS
Failure of a system WRA as shown below
Yaw accelerometer failure
Pitch actuator position does not agree with
command
Pitch computer failure (Valid only with
corresponding CAUTION-ADVISORY lights
on. Autopilot caution light and indicated
failure is not valid)
Pitch sensor failure
Roll actuator position does not agree with
command
Roll computer failure
Roll sensor data failure
Yaw series servo actuator failure
Yaw computer failure (Check that ALPHA
COMP/PEDAL shaker clrcult breaker (RBl)
is engaged)
Yaw sensor failure
Failure of AICL or AICR (See below)
Indicates which AICS has falled. Used in
conjunctlon with INLET/ RAMPS caution
lights.
Programmer failure, without INLET light,
computer uses normal values
Figure 38-9. OBC Failure Acronyms (Sheet 1 of 11)
ORIGINAL m-14
NAVAIR Ql-Fl4AAD-l
FHF
OBC ACRONYM ACRONYM DEFINITION REMARKS
$0.1 RAMP AIlAl NO. 1 actuator position does not agree
\CTUATOR AIRAl with command
JO. 2 RAMP AllA NO. 2 actuator position does not agree
VZIJATOR AIRA with command
r10.3 RAMP AiLA NO. 3 actuator position does not agree
ACTUATOR AiRA with command
;TATlC PRESSURE AILS1 Static pressure sensor. With INLET light,
AIRS1 SENSOR fall safe mode. Without INLET
IigM, failure operational. No filght
restrictlon
rOTAL PRESSURE
4NGLE OF ATTACK
AlLS2
AIRS2
AILS4
AIRS4
Total pressure sensor. With INLET light,
SENSOR fall safe mode
Angie-of-Attack (AOA) or engine fan
speed. (AFTC may be in secondary
mode.) Without INLET light, fail
operational. No flight restriction
,D/MCS AIUD
AIRID
identifier conflict
WC APC Approach Power
Compensator
Auto throttle Inspection. System will defaui
to BOOST automatically. A REV 4 AIC
programmer is installed in lieu of correct
REV 5 programmer.
RCCELEROMETER APCAM APC accelerometer fail
No associated light
Auto throttle inoperative
APC not authorized for landing
COMPUTER APCPU APC computer fail
Auto throttle inoperative
ASPJ
PROCESSOR
ASPJ
SPJPR
Airborne Self-Protection
JammSr
ASPJ failure. ECM may not be available.
Run commanded BIT
Possible processor failure. Run
commanded SIT to provide fault isolation
to WRA level
RECEiVER LOW SPJRL Low-band receiver failure
Figure 38-9. OBC Failure Acronyms (Sheet 2 of 11)
38-15 ORIGINAL
NAVAIR 01-FI4AAD-1
FHF
OBC ACRONYM ACRONYM DEFINITION REMARKS
TECENER HIGH SPJRH High-band receiver failure
tECEtVER AUG SPJRA Augmentation receiver failure
RANSMtllER LOW SPJTL Low-band transmitter failure
nXAN.SMtlTERH IGH SPJTH High-band transmitlerf ailure
rRANSMtllER AUG SPJTA High-band augmentation transmitter failurs
3WR INTERFACE SPJRI Interface failure between ASPJ and RWR
3AG BAG Beacon Augmentor BAG not powered on
Run commanded SlT
Degraded position approach on automatic
carrier landing (ACL) and/or ground
vectoring
BSF BSF
FILTER I-RWR 315 BSFl
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F-14D 飞行手册 Flight Manual 3(66)
