曝光台 注意防骗
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continuously displayed as long as an OBC or CSS format is presented and is
removed when the handbrake is set.
iAD JTID DATA LOAD Displayed when JTIDS test is selected during initialization (Down Load) of
JTIDS.
ACAN FAIL DETECTED Displayed for a TACAN failure or JTIDS NOT READY.
TIDS FAIL DETECTED Displayed for a JTIDS failure or JTIDS NOT READY.
ORIGINAL
Figure 38-13. OBC/CSS Messages
38-30
NAVAIR 0%FMAAD-1
ACRONYM
MCI
MC2
CIU
INS
IMU
DISPLAYED CONDITION CAUSE
Mission computer No. 1 is NO GO or NOT Mission computer No. 1 is failed, or
READY powered off
Mission computer No. 2 is NO GO or NOT Mission computer No. 2 is failed, or
READY powered off
CIU is NO GO or NOT READY CIU is failed, or powered off
INS is NO GO or NOT READY INS is failed,or powered off
IMU is not valid IMU is failed. Loss of inertial and attitude
data from INS
RWR
FWD ASPJ
AFT ASPJ
MCI HOT
MC2 HOT
ASPJ HOT
CIU HOT
DPI HOT
DP2 HOT
SMS HOT
RDR HOT
HUD HOT
RWR HOT
DSS HOT
DEU HOT
MPS HOT
IRST HOT
SAHRS HOT
JTID HOT
IPF
SDU ALRM
RWR is NO GO or NOT READY RWR is failed, or powered off
ASPJ receiver (low or high), ASPJ ASPJ RECEIVER, TRANSMITTER, or
transmitter (low or high) or processor is PROCESSOR is failed
NO GO
ASPJ processor, receiver augmentation or ASPJ PROCESSOR, RECEIVER AUG, or
transmitter augmentation is NO GO TRANSMITTER AUG is failed
Mission computer No. 1 overheated Possible loss of cooling air
Mission computer No. 2 overheated Possible loss of cooling air
ASPJ is overheated Possible loss of cooling air
CIU is overheated Possible loss of cooling air
DPl is overheated Possible loss of cooling air
DP2 is overheated Possible loss of cooling air
SMS is overheated Possible loss of cooling air
RDR is overheated Possible loss of cooling air
HUD is overheated Possible loss of cooling air
RWR is overheated Possible loss of cooling air
DSS is overheated Possible loss of cooling air
DEU is overheated Possible loss of cooling air
MPS is overheated Possible loss of cooling air
IRST is overheated Possible loss of cooling air
SAHRS is overheated Possible loss of cooling air
JTIDS R/T is overheated Possible loss of cooling air or a high JTIDS
transmit duty cycle.
JTIDS Interference Protection Feature JTIDS is failed, a momentary glitch or 20%
detected failure duty cycle has been exceeded in “Limit”.
Select IPF Reset on JTIDS Control Panel.
JTIDS Secure Data Unit failure or no crypt0 SDU fail or the crypt0 key is erased.
load
Figure3 8-14.O BC-RelateWd aming/CautiodAdvisoMrye ssages
30-31 ORIGINAL
NAVAIR Ol-Fl4AAD-1
30.4 COOPERATNE SUPPORT SOFTWARE
CSSauowScaptureanddisplayofsystemdatainreal
time and the optional recording of data from avionics
procemors that are CSS compatible. CSS is typically
used to aid in troubleshooting system problems. The
CSS compatiile processors include mission computer
No. 1, mission computer No. 2, multifunction display
system No. 1, multit%nction display system No. 2, airborne
data acquisition sysm stores management pmcessor,
converter interface unit, data enuy unit, intImed
search and track system joint tactical infomtation distribution
system, and sensor display indicator set. Note
thatradarflycatcherdisplaysareprovidedonthetactical
information display.
Note
The JTIDS processor only supports the flycatcher
functions (start address, increment,
decrement, and disable).
CSS supports the following modes, all of which
are selectable on the DEU: flycatcher, block address,
and trap. CSS data is displayed on the MFD
CSS format. The CSS format is selected by pressing
the FAULT pushbutton on the OBC basic format
and then pressing CSS on the MAINT
CURRENT FAILURES format.
38.4.1 CSS Operation. The CSS page (see Figme
38-15), displayed on the DEU. allows the entry of
DATA TYPE and OPER CODE used for data recording
purposes, and allows the selection of ail CSS
modes including flycatcher, block address, and trap.
Ail CSS data is displayed on an h4FD CSS format,
using pushbutton controls. Note that if the DEU is
slaved to the RIO MFD, selection of the CSS format
on that MFD will cause the CSS page of the DEU to
be displayed.
38.4.1.1 Data Recording Operations. The CSS
DATA TYPE page (see Figure 38-16) allows the optional
selection of a recording/storage device for the
retention of data that is captured via a CSS mode. CSS
data can be telemetered or recorded for offline analysis
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F-14D 飞行手册 Flight Manual 3(73)
