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position, also indicates that the APX-76 made a valid
interrogation. The bottom line on the DD indicates that
ORIGINAL 21-6
NAVAIR 0%FI4AAD-1
the APX-100 responded in mode and the top line indicates
it responded in code. Both lines together indicate
that the APX-76 is decoding properly. Biasing of the
mode and code lines enables them to be spread out on
the DD during test. Ifthe first attempt to test the APX-76
fails because of lack of video on the DD, or the amber
fault light on the control panel illuminates, the RIO
should initiate a validchallenge by momentarily holding
the CHAL CC/TEST switch in CHAL CC in order to
reset the BIT flags associated with the APX-76. The
APX-76 normally powers up with the BIT flags in the
fault position. The system will continuously fault until
the flags are reset. The APX-76 antenna is checked
during the test by receiving actual video from the APX-
100 antenna.F ailure of any part of the APX-76 closed
loop test will cause IFI to be displayed in continuous
monitor. A further breakdown as to what portion of the
system has failed can be verified by calling up the maintenance
tile. Testing of all modes of the APX-76 should
be performed independently.F ailure of one mode does
not necessarily mean that all modes are malfunctioning.
The APX-76 receiver-transmitter, switch amplifier,
interrogator (KIR) computer, and synchronizer are
checked during CNI OBC. Results can be called up on
any MFD. These units are also subject to continuous
monitoring. Status can be read by calling up the failure
history file. In addition, the TID displays the IF1 acronym
if the receiver-transmitter or switch transponder
fails continuous monitoring. During OBC, CHALLENGE
IFF is displayed on MFD 3 in order to remind
the RIO to reset the BIT flags by making a valid
challenge.
ORIGINAL
NAVAIR 01.F14AAD-1
RIO HAS MODE 3, CODE 1200 SET
SEARCH MODES
SINGLE-TARGET TRACK
TARGET UNHOOKED
PROPEMR ODE PROPEMR OOE
AND CODE RETURNS AND CODE RETURNS
WT” TARGETV IDEO NOT AROETW DEO
MODER ETURN TARGETN OT SO”AWKlNG STT TARGET*o ”AWKINO
ONLYW ITH OR SO”AWKINGA NOTHERM ODE PROPEMRO DEA ND CODE
TARGETV IDEO ,PDSTTB -OUNP RESENTATION,
SINGLE-TARGET TRACK
TARGET HOOKED
TEST
ORIGINAL
Figure. 21-3. IFF Display Formats
21-a
NAVAIR O1-F14AAD-I
PART VIII
Weapon Systems
Chapter 22 -TARPS Subsystem
Chapter 23 -Navigation Command and Control Grid
Chapter 24 -Resewed for LANTIRN Targeting System
The followingchaptersare tobc foundinNAVAIROl-F14&4D-IA:
Chapter 25 - F-14D Weapon System
Chapter 26 - Weapon System Controls and Displays
Chapter 27 - AN/AFG-71 Radar System
Chapter 28 - ANlAAS-42 l&wed Search and Track System
Chapter 29 - AN/AXX-1 Television Camera Set
Chapter 30 - Integrated Sensor Operation
Chapter 3 1 - Stores Management System
Chapter 32 -Air-to-Air Weapons
Chapter 33 - Air-to-Ground Weapons
Chapter 34 -Electronic Warfare Systems
Chapter 35 -Data-Link Systems
Chapter 36 -Weapon System Degraded Operation
89 (Reverse Blank) ORIGINAL

NAVAIR 01-F14AAD-l
CHAPTER 22
TARPS Subsystem
22.1 RECONNAISSANCE SYSTEM
The reconnaissancsey stem establishesth e aircrafi as
a multisensorr econnaissancaei rcraftw ith the flexibility
for a wide range of reconnaissancem issions. Specific
missions include order-of-battle generation, prcstrike/
poststrike photography, and maritime surveillance.
The sensorsa nd associatede quipment are contained
in the pod? four compartments (Figure 22-l). The sensors
am serial fhme camera !J&87D), low- to mediumaltitude
panoramic camera (KA-99), or long-range
standoff frame camera (KS-153A with 24-&h lens),
and AN/AAD-5A in&red reconnaissances et .
This capability is compatible with the F-14 tactical
air reconnaissance pod system and includes target
designation and steering command functions and
reconnaissance sensor control as well as specific
reconnaissancdei splays to crew and in-flight BnnOtation
of reconnaissanced ata.
The TARPS consists ofthe following components (as
shown in Figure 22-l):
1. TARPS pod
2. Serial frame camera
3. Panoramic camera
2-wm-263-O
Figure 22-l. Tactical Air ReconnaissancPe od System
22-1 ORIGINAL
NAVAIR Ol-Fl4AAD-1
4. I&S,& lime scanner set
5. Data display system
6. TARPS environmental control system
7. Control indicator power distribution unit
8. Controller processor signal unit
The TARPS location on the aircraft is shown in
　
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本文鏈接地址：F-14D 飛行手冊 Flight Manual 3(42)