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IR door will remain closed during cooldown. After cooldown Is
achieved mlrror spin motor is energlzed and IR door will open
unless landing gear handle is down.
NFOVI - SYSTEM switch In RDY Sensor in ready mode. Sensor selects
WFOV narrow (or wide) field of view In response to switch posltlon.
Sensor Is ready to cycle if cool down has occurred. IR door will
open if gear handle is UP
Note
FILM switch In RUN. IR LS flashes green (one
flash/foot of film travei). If cooldown is Incomplete, the
IR NR will be Illuminated amber and the sensor will not
respond.
012 MAN V/H light OFF - Vg/H from aircraft computer within acceptable Ilmits.
l Amber
ON- lllumlnated amber:
V/H switch In TEST With VEL set at 90 (900 MS) and ALT set at
995 (599 ft), or any equivalent of 1.9 ratio, the thumbwheel
circuitry has failed If the light stays on.
V/H switch In AUTO. Computer failed or computer fall discrete Is
received with or without TARPS pod on aircraft. Manual VgjH
being used. Set correct values to Vs/H In thumbwheels. Set V/H
switch to MAN.
If negative AGL or computed Vg/H = 0, MAN VgfH is being
used. Set corrected values of VgfH In thumbwheels.
Figure 22-3. Controller Pmc&sor Signal Unit (Sheet 4 of 6)
22.7 ORIGINAL
NAVAIR 0%F+lAAD-I
NOMENCLATURE FUNCTION
V/H switch in MAN. Manual V/H intentionally selected. Values set
in thumbwheels being used. Set correct values in thumbwheels.
Note
l A TARPS advisory will appear on the Reconnaissance
MFD CAWS window when MAN V/H Is
selected (figure 24-6). In addition, a TARP1 is
generated on the OBC Basic Display and Maintenance
Failure Format (figure 24-7).
l If negative AGL or Vg/H = 0, and the TARPS pod is
not on the aircraft, there is no MAN Vg/H advtsory.
0 DATA IlgM OFF - Data received from computer. ON -Data from alrcrafl computer
failed (via CPS DATA FAIL discrete).
Note
014 ALTFTX 190
015 VELKTXlO
thumbwheels
@
FILM swttch
A TARPS advisory will appear on the Reconnaissance
MFD CAWS window (figure 24-S) when MAN V/H Is
selected. In addition, a TARP1 and TARP2 are
generated on the OBC Basic Display and Maintenance
Format. (Figure 24-7).
Used to set manual altitude Inputs to pod. Counter range Is from 000 to 999,
read In multiples of 100 feet.
Use to set manual ground speed inputs to pod. Counter range is from 00 to
99, read In multiples of 10 knots.
MARK - (momentary position) Allows RIO to mark special interest frame
with * in data block.
RUN - Activates selected sensor when SYSTEM switch is set to RDY.
OFF - Terminates TARPS sensor operation
Figure 22-3. Controller Processor Signal Unit (Sheet 5 of 6)
ORIGINAL 22-8
NAVAIR Of-F’blAAD-1
NOMENCLATURE FUNCTION
017 V/H selector switch MAN - Selects manual thumbwheel inputs. (TARPS advisory appears on
MFD CAWS figure 24-6. TARP1 appears on OBC Basic Display
and Maintenance Failure Format figure 24-7).
AUTO - Selects aircraft computer value of Motion Compensation Factor
WV.
TEST - (Momentary position) Tests proper functioning of thumbwheels
Vs/H circuitry. With a 1.6 ratio set in the thumbwheels, a good test
is Indicated by the MAN V/H light extinguishing.
69
EXPOSURE selector UNDER - -1 f-stop exposure for doubled S/C film setting.
swkh
NORM - Normal exposure for doubled S/C film setting.
OVER - + 1 f-stop for doubled S/C film setting.
@ SYSTEM switch OFF - AIrcraft power denied to TARPS. No sensors can be operated.
ROY - Aircraft power available at sensor connectors. If respective sensor
moved from OFF position, sensor is placed in standby or ready
mode.
RESET - Clears TARPS failure signal. If failure Is other than transient,
TARPS advisory remains.
Figure 22-3. Controller Processor Signal Unit (Sheet 6 of 6)
8. Provide selection of TARPS air-to-ground ranging
for altitude above ground level determination. NOMENCLATURE CIRCUIT
CARD
22.3 TARPS EQUIPMENT CIRCUIT
BREAKERS
RECON HTR PWR PHA
RECON HTR PWR PHS
The main power circuit breakerst hat control TARF’S
equipment are in the aft cockpit. FO-8 and FO-9 show
their location. The circuit breakers are numbered and
labeled as follows:
RECON HTR PWR PHC
RECON ECS CONT AC
RECON ECS CONT DC
281
2D1
2Fl
2G4
6El
NOMENCLATURE
RECON POD
RECON POD CONT
RECON POD DC PWR NO. 1
RECON POD DC PWR NO. 2
c%ZT
lE2
6E2
6E4
6E3
Refer to Chapter 2 for an alphanumeric listing of
circuit breakers.
22.4 RECONNAISSANCE DISPLAYS AND
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F-14D 飞行手册 Flight Manual 3(45)
