EA-18G. FLIGHT MANUAL (2008) - page 10

 

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EA-18G. FLIGHT MANUAL (2008) - page 10

 

 

A1-E18GA-NFM-000
CHAPTER 22
Cold Weather Procedures
22.1 EXTERIOR INSPECTION
If the aircraft has not flown within 4 hr -
1. Pay particular attention to the nosewheel oleo, and APU and brake accumulator pressures.
22.2 BEFORE ENTERING COCKPIT
If a battery/APU start is anticipated -
1. Consider using external power to raise the canopy to conserve battery power.
22.3 INTERIOR CHECK
1. Canopy - Consider leaving open until the right engine has been started to (1) conserve battery
power and (2) permit rapid egress.
If the aircraft has been cold soaked below -18°C (0°F) -
1. Rudder pedal adjustment may be difficult or impossible and the inertia reel may not retract
automatically until the cockpit warms up (typically 5 to 10 minutes).
22.4 ENGINE START
1. Perform normal engine starts (windmilling is not required)
APU starts should be successful if the battery and the APU accumulator are fully charged. The
FADEC modulates fuel flow as required to prevent a hung start. Successful engine starts have been
demonstrated at ambient temperatures down to -40°F without start anomalies; however, expect engine
starts to be slower than at nominal temperatures.
2. Avoid activating any hydraulic actuated system for 2 minutes after both engines are online.
This allows hydraulic fluid to warm both systems and prevents hydraulic seal damage and potential
hydraulic leaks.
3. Oil pressure on the EFD may appear as invalid if 200 psi is exceeded. Maximum oil pressure 2½
minutes after engine start is 180 psi.
22.5 BEFORE TAXI
If ambient temperature between 0 and 7°C -
1. Minimize engine operation above IDLE to reduce the potential for ice accumulation on the engine
inlet lips. Inlet lip icing can occur at these conditions without the INLET ICE caution.
VI-22-1
ORIGINAL
A1-E18GA-NFM-000
If visible moisture exists (rain, fog) and the temperature is 45°F (7°C) or less-
1. ENG ANTI ICE switch - ON (after engine start)
2. PITOT ANTI ICE switch - ON (after taxi but prior to takeoff)
If the aircraft has not flown within 4 hr with ambient temperature below -18°C (0°F) -
1. Up to three selections of the FCS exerciser mode may be required in order to obtain a successful
FCS RESET after the initial 2 minute warm-up.
For cold weather operations below -18°C (0°F) -
1. Three arresting hook cycles should be performed to bring extension time within specification (2
seconds is nominal).
2. Proper operation of the OBOGS monitor may not occur until 2 minutes of warm up.
22.6 TAKEOFF
If snow or slush has accumulated on the landing gear -
1. Leave the gear down for 1 minute after takeoff to clear snow or slush.
2. The landing gear may be slow to retract (up to 30 seconds) following cold soak below -18°C (0°F).
Gear retraction times in excess of 15 seconds annunciate the landing gear warning tone.
3. Carefully monitor gear uplock signals (all three landing gear position lights out, landing gear
warning light out).
VI-22-2
ORIGINAL
A1-E18GA-NFM-000
PART VII
COMM-NAV EQUIPMENT
AND PROCEDURES
Chapter
23 - Communications-Identification Equipment
Chapter
24 - Navigation Equipment
Chapter
25 - Backup/Degraded Operations
Chapter
26 - Visual Communications
Chapter
27 - Deck Ground Handling Signals
67
(Reverse Blank)
ORIGINAL
A1-E18GA-NFM-000
CHAPTER 23
Communication-Identification
Equipment
23.1 Multifunction Information Distribution System (MIDS).
MIDS is an advanced, high capacity, jam resistant, digital communication link. MIDS is an
omnidirectional radio that uses frequency-hopping techniques similar to HAVEQUICK, and encryp-
tion for security. It is like a Local Area Network (LAN) in that multiple users can access information
simultaneously. MIDS is used to exchange near real-time information among air, ground and sea
elements engaged in tactical operations. LINK 16 equipped platforms can transfer voice and data.
Refer to NTRP 3-22.2-EA-18G (EA-18G Classified Manual) for Tactical information. Refer to Chapter
24 for navigation information.
23.2 ICS - INTERCOM SYSTEM
The ICS provides amplification and distribution of intercockpit voice communications, aircrew-to-
ground crew voice communications, ICS voice alerts and tones, as well as advisory tones originating
external to the ICS.
Volume controls are provided to control headset volume for:
1. Voice Activated Intercom (VOX)
2. Transmit sidetone/aircrew intercom audio/ground crew intercom audio
3. MIDS A audio
4. MIDS B audio
5. RWR audio
6. WPN delivery audio
7. TACAN ident
8. Auxiliary audio (available for other uses).
The ICS is also used to control the following COMM/IFF related functions:
1. Selection of PLAIN voice or CIPHER relay modes (RLY switch).
2. Selection of guard transmit (G XMT) for COMM 1 and 2 (G XMIT switch).
3. Hold or zeroize of IFF crypto code (CRYPTO switch).
4. Selection of IFF Mode 4 cautions, advisories, and voice alerts (MODE 4 switch).
5. Selection of IFF NORM or EMERG operating modes (IFF MASTER switch).
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ORIGINAL
A1-E18GA-NFM-000
23.2.1 ICS Function Selector Switch. The ICS function selector switch is located in each cockpit and
is used to select the operating mode for ICS voice communications.
23.2.1.1 ICS Function Selector Switch Front Cockpit. The switch is located on the ANT SEL panel
on the outboard left console in the front cockpit. In order for a crewmember to communicate on the
ICS, the ICS function switch in that cockpit must be in HOT MIC and the ICS VOL knob must be set
(as desired) above the LO position.
RADIO
Selects HOT MIC in both cockpits and ensures ICS volume is louder than COMM
ORIDE
volume.
HOT MIC Enables the front (rear) cockpit microphone for ICS transmissions.
COLD MIC Disables front (rear) cockpit microphone.
23.2.1.2 ICS Function Selector Switch Aft Cockpit. The switch is located on the VOL control panel
on the left console in the aft cockpit. In order for a crewmember to communicate on the ICS, the ICS
function switch in that cockpit must be in NORM and the ICS VOL knob must be set (as desired)
above the LO position.
RADIO
Selects HOT MIC in both cockpits and ensures ICS volume is louder than COMM
ORIDE
volume.
NORM
Enables aft cockpit microphone for ICS transmissions.
23.2.1.3 ICS Aft Cockpit Kick Switches. Two ICS kick switches are located on the inboard side of
each rudder pedal. These switches are in addition to COMM transmit switches on the rudder pedals.
Either switch will activate the ICS for intercockpit communication.
23.3 VHF/UHF COMMUNICATION SYSTEM
The aircraft has two ARC-210 voice communication radios. The VHF/UHF radios, COMM 1 and
COMM 2, provide air-to-air/air-to-ground voice communications. The radios can be operated in plain
mode, anti-jam (Have Quick 1 or 2) mode, secure mode (KY-58), or relay mode; in either normal or
secure voice. An additional function is generation by either COMM 1 or COMM 2 of a 1,020 hz tone
(AM) or a 15 hz tone (FM) which serve as audio cues to the pilot. The COMM 1 and COMM 2 radios
operate in the frequency bands listed below. When enabled, integral guard receivers continuously
monitor the emergency guard channels for each frequency band.
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A1-E18GA-NFM-000
Figure 23-1. Aft Cockpit Rudder Pedal Switches
Frequency Band (MHz)
Modulation
Guard Channel (MHz)
30 to 87.995
FM
121.5
*108 to 135.995
AM
136 to 155.995
AM/FM
156 to 173.995
FM
225 to 399.975
AM/FM
243.0
(AM)
*Cannot transmit on 108 thru 117.995 MHz
Transmission and reception of amplitude and frequency modulated signals (AM and FM) occur in
the respective frequency bands on spaced channels of 5 kHz. Twenty channels in the 30 to 400 MHz
band may be pre-set to assigned frequencies.
23.3.1 VHF/UHF Controls and Indicators. The COMM 1 and COMM 2 are operated by
1. Controls on the UFCD,
2. Controls on the ICS,
3. COMM 1 and 2, MIDS A and B transmit switches on the right (inboard) throttle grip,
4. COMM 1 and 2 transmit switches on the left and right rear cockpit rudder pedals respectively.
The PTT panel controls the rudder pedal selection of Comm 1 or MIDS A, and Comm 2 or MIDS
B. The PTT panel is located on the left hand outside bulkhead.
VII-23-3
ORIGINAL
A1-E18GA-NFM-000
23.3.1.1 UFCD - Up Front Control Display. The UFCD is on the main instrument panel above the
MPCD. The rear cockpit UFCD is on the main instrument panel above or below the MPCD. See figure
23-2 for top level CNI format. Controls on the UFCD for COMM 1 and 2 are:
1. VOL (volume) 1 and 2 COMM control knobs,
2. COMM 1 and 2 channel select knobs,
3. keypad options and scratchpad display,
4. touch options/displays,
5. ID (identification) button,
6. OFF/BRT (brightness) control knob,
7. CONT (contrast) control knob,
8. SYM (symbology) brightness control knob,
9. EM CON (emission control) pushbutton switch.
10. MIDS - turned on/off by pressing either the TACAN or LINK 16 options, then ON/OFF.
23.3.1.1.1 COMM 1 and 2 VOL (Volume) Control Knobs. Operation of the VOL control knobs is not
dependent on the operation of the MPCD or the UFCD. Each VOL control knob controls power
(on/off) and audio level to the associated COMM 1 and 2 radio. Tick marks on the VOL control knobs
and the face of the UFCD are used to indicate OFF for the associated COMM 1 or 2 radio. Clockwise
rotation from OFF applies power to the associated radio and continued rotation increases the audio
level. The cockpit and rear cockpit VOL control knobs must both be OFF to remove power from the
associated radio. When a radio is powered (on), the associated COMM radio (unlabeled) touch
option/display is corner highlighted (upper left corner).
23.3.1.1.2 COMM 1 and COMM 2 Channel Select Knobs. Operation of the COMM 1 or COMM 2
select knobs is not dependent on the operation of the MPCD or UFCD. Clockwise rotation of either
COMM channel select knob changes the associated COMM 1 or COMM 2 preset channel selections in
the order:
1. CH (1 thru 20) one of twenty preset channels,
2. CH G (guard channel),
3. CH M (manual frequency selection mode),
4. CH C (cue channel/frequency for Single Channel Ground and Airborne Radio System) (SINC-
GARS),
5. CH S (ship maritime).
Continued clockwise rotation repeats the change sequence. Counterclockwise rotation reverses the
change sequence. Rotating either COMM select knob to CH G tunes the associated radio to 243.0 MHz
UHF. To communicate on a guard frequency other than 243.0 MHz UHF, a different guard frequency
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ORIGINAL
A1-E18GA-NFM-000
must be manually entered. Rotating either knob with any AJ MENU sublevel selected returns the
UFCD to the COMM sublevel.
Figure 23-2. Top Level CNI Format on Up Front Control Display (UFCD)
23.3.1.1.3 COMM Keypad Options and Scratchpad Display. In the top level CNI format twelve
keypad options and a scratchpad display may be used to change the CH 1 thru 20 preset channel
numbers, CH G (guard) frequency, CH M (manual frequencies), CH C (cue channel/frequency) or CH
S (ship maritime frequencies). The keypad options are 0 thru 9, CLR (clear) and N-E-W-S (shifted).
23.3.1.1.4 COMM Touch Option/Displays. On the top level CNI format ten touch option/displays
may be used to select COMM 1, COMM 2, or other sublevel formats. The upper right and lower right
touch option/displays are dedicated to the COMM 1 and COMM 2 radios respectively. Selecting other
sublevel formats does not remove the COMM 1 and 2 touch option/displays.
The COMM 1 and COMM 2 channel displays are also utilized to visually identify which audio
sources are currently active. When an active radio transmission is occurring, the upper half of the
COMM 1/2 option is background shaded. When an active MIDS transmission is occurring, the lower
half of the COMM 1/2 option is background shaded.
Both UFCDs indicate an active transmission in progress when either cockpit initiates the
communication. The active transmission indication is a rectangular border around the source (upper
for COMM, lower for MIDS). When the active transmit cue is illuminated, the frequency of the related
radio is partially covered on the aft UFCD.
VII-23-5
ORIGINAL
A1-E18GA-NFM-000
The remaining eight touch option/displays are:
1. D/L, BCN, ILS (data link, beacon and instrument landing system),
2. A/P (auto pilot),
3. TCN (TACAN with channel number),
4. IFF (identification friend or foe with mode numbers),
5. DDI (digital display indicator),
6. RALT (radar altimeter with altitude reading),
Channels 10 and 20 are valid entries for Low Altitude Warning settings.
Due to the close proximity of the COMM 1 and RALT touch options/
displays, it is possible to inadvertently change the low altitude warning
setting for the radar altimeter when using COMM 1 fast data entry.
7. AEA (airborne electronic attack),
8. FLIR (forward looking infrared radar).
23.3.1.1.5 UFCD OFF/Brightness (BRT) Control Knob. The OFF/BRT control knob adjusts the
overall brightness of the UFCD for both symbology and video. Clockwise rotation from OFF applies
power to the UFCD and progressively increases brightness. Counterclockwise rotation to OFF removes
power from the UFCD. The UFCD does not need to be powered for COMM 1 or 2 to function.
23.3.1.1.6 UFCD Contrast (CONT) Control Knob. Clockwise rotation of the CONT control knob
increases video contrast. Counterclockwise rotation decreases video contrast.
23.3.1.1.7 UFCD Symbology (SYM) Control Knob. Clockwise rotation of the SYM brightness
control knob increases the brightness of the UFCD symbology only. Video brightness is not affected by
this knob.
23.3.1.1.8 Emission Control (EMCON) Pushbutton. The EMCON pushbutton switch may be used
to terminate all onboard emitters except COMM transmitters and ALQ-165. If emergency is selected
on the ACI panel, the IFF and D/L respond with emergency, if interrogated. When EMCON is selected
with the EM CON pushbutton switch, emission can be restored only with this switch. When EMCON
is selected with the sensor control switch, emission can be restored with the sensor control switch or the
EM CON pushbutton switch. During EMCON operations, EMCON is displayed in the scratchpad for
top level CNI display or vertically in the left options for DDI displays on the UFCD.
23.3.1.2 COMM Control Panel. The COMM control panel is on the left console. The switches which
are used for VHF/UHF operation are the COMM relay switch and the COMM G XMT select switch.
23.3.1.2.1
Relay (RLY) Switch. The RLY switch, located on the COMM control panel, is used to
enable relay communications by allowing information received through one radio to be routed to the
other radio for transmission. The switch must be placed in the OFF position prior to the initial
VII-23-6
ORIGINAL
A1-E18GA-NFM-000
application of power to the aircraft.
CIPHER Enables CIPHER relay mode.
OFF
Relay mode disabled.
PLAIN
Enables PLAIN voice relay mode.
23.3.1.2.2
Guard Transmit (G XMIT) Switch. The G XMIT switch, located on the COMM control
panel, is used to manually tune the COMM 1 or COMM 2 receiver-transmitter to the guard frequency
of 243.0 MHz (AM). This function is provided in case the normal (UFCD) and primary backup modes
(UFC BU format) of frequency selection are lost.
COMM 1
Selects COMM 1 transmit.
OFF
Normal COMM operation selected.
COMM 2
Guard frequency manually selected on COMM 2.
23.3.1.3 COMM 1 Antenna Select (ANT SEL) Switch. The COMM 1 ANT SEL switch, located on the
ANT SEL panel on the outboard left console, is used to manually select the upper or lower blade
antenna for COMM 1 reception/transmission.
UPPER
Manually selects the upper blade antenna.
AUTO
COMM 1 automatically selects the antenna receiving a usable signal.
LOWER Manually selects the lower blade antenna.
COMM 1 receiver-transmitter automatically selects the antenna receiving a usable signal.
23.3.1.4 COMM Throttle Switch. The COMM throttle switch, located on the inboard side of the
right throttle, is used to enable radio transmission on COMM 1, MIDS A, COMM 2, or MIDS B. The
switch is spring-loaded to the center position.
Top
Selects COMM 1 transmit.
Bottom
Selects COMM 2 transmit.
Forward Selects MIDS A transmit.
Aft
Selects MIDS B transmit.
23.3.1.5 COMM Foot Pedal Switches. The COMM switches, located on the fixed foot pedals of the
rear cockpit, are used to enable radio transmission on COMM 1 and COMM 2, or MIDS A and MIDS
B depending on the position of the PTT panel switches. Each switch is spring-loaded to the up
position.
VII-23-7
ORIGINAL
A1-E18GA-NFM-000
Left
Selects COMM 1 or MIDS A transmit.
Down
(Unmarked)
Both Up Both COMMs in receive.
(Unmarked)
Right
Selects COMM 2 or MIDS B transmit.
Down
(Unmarked)
23.3.2 COMM 1 AND 2 OPERATION. The operation of COMM 1 and 2 is identical. The following
description addresses only COMM 1; however, it should be understood that the description is
applicable to COMM 2. Power to COMM 1 is applied by rotating the VOL 1 COMM control knob
clockwise. Power application is identified by a corner highlight in the upper left corner of the COMM
1 touch option/display. The channels and preset frequencies (CH 1 thru 20), CH G, CH M, CH C and
CH S may be selected by rotating the COMM 1 channel select knob until the desired CH sub level and
fixed frequency are displayed in the COMM 1 touch option/display. In the anti-jam mode, the fixed
frequency is replaced with H1, H2 or SG. When COMM 1 is actively receiving, the upper half of the
touch option/display is half intensity highlighted. The active receive indication is available only if the
radio is powered.
23.3.2.1
Top Level CNI Format Channel or Manual Frequency Change. In the top level CNI
format, the preset channel number is changed by touching the desired channel number on the keypad
and then touching the COMM 1 touch option/display. If an invalid channel entry is made, ERROR is
displayed in the scratchpad.
The manual frequency is entered by entering the desired frequency on the keypad display and
touching the COMM 1 or COMM 2 touch option display. Trailing zeroes need not be selected. If an
invalid manual frequency entry is made, ERROR is displayed in the scratchpad and the radio does not
go to the CH M (manual) channel. Selecting 0 and subsequently touching the desired radio, changes
that radio to the programmed MAN radio frequency.
23.3.2.2 COMM Sublevel Selection. Touching the COMM 1 touch option/display while on CH 1
thru 20, CH G, CH M, CH C, or CH S selects that sublevel mode. When applicable, the sublevel mode
is used to:
1. Change a fixed frequency,
2. Change ship maritime preset,
3. Change the guard or cue frequency,
4. Enable or disable cipher mode,
5. Adjust squelch,
6. Enable or disable guard receive,
7. Select modulation type (AM or FM),
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ORIGINAL
A1-E18GA-NFM-000
9. Enter anti-jam mode (AJ or AJ MENU),
10. Access Have Quick, Have Quick time, SINCGARS coldstart, Have Quick manual data fill, or
SINCGARS zeroize.
Figure 23-3. COMM Sublevel - Ship Maritime Preset
23.3.2.3 COMM Sublevel - Ship Maritime Preset. The Ship Maritime Preset COMM Sublevel is
selected by touching the COMM 1 touch option/display with CH S previously selected (see figure 23-3).
This sublevel is used to enable or disable squelch, cipher mode, or guard receive. Selecting this sublevel
displays a 1: (selected radio) followed by an S and the current ship maritime preset number. The ship
maritime preset number is changed by touching the desired number(s) on the keypad options
(numbers 1 thru 28 or 60 thru 88), verifying the new number in the scratchpad, and touching the CH
S option. If an invalid number is entered, ERROR is displayed in the scratchpad. CPHR (cipher),
SQCH (squelch), and GRCV (guard receive) are enabled or disabled by touching the respective touch
options/displays. An enabled option has a highlighted border. CPHR operation is available for only one
radio at a time. Enabling CPHR on COMM 1 automatically disables CPHR on COMM 2 if previously
enabled.
The modulation type (AM or FM), AJ, or AJ MENU options are not available on this sublevel.
23.3.2.4 COMM Sublevel - Guard and Cue Presets. The Guard or Cue Preset COMM Sublevel is
selected by touching the COMM 1 touch option/display with CH G or CH C previously selected (see
figure 23-4). This sublevel is used to change the G (guard) or C (cue) frequency, to enable or disable
squelch, cipher mode, guard receive, or to select modulation type (AM or FM). Selecting this sublevel
displays a 1: (selected radio) followed by a G or C and the current fixed frequency. The fixed frequency
is changed by touching the desired numbers on the keypad options, verifying the new number in the
scratchpad, and the desired Comm option. Valid frequencies are:
VII-23-9
ORIGINAL
A1-E18GA-NFM-000
Figure 23-4. COMM Sublevel - Guard and Cue Presets
1.
30 thru 87.995 MHz (FM) - at increments of 0.005, 0.025 MHz for C
2.
108 thru 135.995 MHz (AM) - at increments of 0.005, 0.025 MHz for C
3.
136 thru 155.995 MHz (AM/FM) - at increments of 0.005, 0.025 MHz for C
4.
156 thru 173.995 MHz (FM) - at increments of 0.005, 0.025 MHz for C
5.
225 thru 399.975 MHz (AM/FM) - at increments of 0.025 MHz.
If an invalid number is entered, ERROR is displayed in the scratchpad.
SQCH (squelch), GRCV (guard receive), and AM/FM are enabled or disabled by touching the
respective touch options/displays. An enabled option has a highlighted border. The AM/FM option is
always border highlighted and toggles between AM and FM. If the current frequency is available only
in AM or FM, the AM/FM option is not displayed. While in the UHF AM mode, the cipher option
cycles as follows: CPHR (no highlighted border-cipher disabled), CPHR (border highlighted-cipher
baseband enabled), CPDP (border highlighted-cipher diphase enabled). The CPHR and CPDP
options are mutually exclusive. Continued selection of this option repeats the above cycle. CPHR (both
diphase and baseband) is available for only one radio at a time. Enabling CPHR on COMM 1
automatically disables CPHR on COMM 2 if previously enabled.
The AJ and AJ MENU options are not available on this sublevel.
23.3.2.5 COMM Sublevel - Manual Preset. The Manual Preset COMM Sublevel is selected by
touching the COMM 1 touch option/display with CH M previously selected (see figure 23-5). This
sublevel is used to change the M (manual) frequency, to enable or disable squelch, cipher mode, guard
VII-23-10
ORIGINAL
A1-E18GA-NFM-000
receive, select modulation type (AM or FM) or to access Have Quick, Have Quick time, SINCGARS
coldstart, Have Quick manual data fill, and SINCGARS zeroize. Selecting this sublevel displays a 1:
(selected radio) followed by an M and the current fixed frequency. The fixed frequency is changed by
touching the desired numbers on the keypad options, verifying the new number in the scratchpad, and
touching the desired option.
Valid frequencies are:
1.
30 thru 87.995 MHz (FM) - at increments of 0.005 MHz,
2.
108 thru 135.995 MHz (AM) - at increments of 0.005 MHz,
3.
136 thru 155.995 MHz (AM/FM) - at increments of 0.005 MHz,
4.
156 thru 173.995 MHz (FM) - at increments of 0.005 MHz,
5.
225 thru 399.975 MHz (AM/FM) - at increments of 0.025 MHz.
Figure 23-5. COMM Sublevel - Manual Preset
If an invalid number is entered, ERROR is displayed in the scratchpad.
SQCH (squelch), and GRCV (guard receive) are enabled or disabled by touching the respective
touch options/displays. An enabled option has a highlighted border. The AM/FM option is always
border highlighted and toggles between AM and FM. If the current frequency is available only in AM
or FM, the AM/FM option is not displayed. While in the UHF AM mode, the cipher option cycles as
follows: CPHR (no highlighted border-cipher disabled), CPHR (border highlighted-cipher baseband
enabled), CPDP (border highlighted-cipher diphase enabled). The CPHR and CPDP options are
mutually exclusive. Continued selection of this option repeats the above cycle. CPHR (both diphase
and baseband) is available for only one radio at a time. Enabling CPHR on COMM 1 automatically
disables CPHR on COMM 2 if previously enabled.
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A1-E18GA-NFM-000
The AJ option is not available on this sublevel.
23.3.2.6 COMM Sublevel - Presets 1 Thru 20 (Fixed Frequency). The Preset 1 Thru 20 COMM
Sublevel is selected by touching the COMM 1 touch option/display with CH (1 thru 20) previously
selected (see figure 23-6). This sublevel is used to change the frequency, to enable or disable squelch,
cipher mode, guard receive, to select modulation type (AM or FM), to enter anti-jam mode or to access
Have Quick, Have Quick time, SINCGARS coldstart, Have Quick manual data fill, or SINCGARS
zeroize. Selecting this sublevel displays a 1: (selected radio) followed by the current channel number
and fixed frequency. The fixed frequency for any channel number (1 thru 20) is changed by touching
the desired numbers on the keypad options, verifying the new frequency number in the scratchpad, and
touching the desired option.
1.
30 thru 87.995 MHz (FM) - at increments of 0.005 MHz,
2.
108 thru 135.995 MHz (AM) - at increments of 0.005 MHz,
3.
136 thru 155.995 MHz (AM/FM) - at increments of 0.005 MHz,
4.
156 thru 173.995 MHz (FM) - at increments of 0.005 MHz,
5.
225 thru 399.975 MHz (AM/FM) - at increments of 0.025 MHz.
Figure 23-6. COMM Sublevel - Presets 1 Thru 20 (Fixed Frequency)
If an invalid number is entered, ERROR is displayed in the scratchpad. SQCH (squelch) and GRCV
(guard receive) are enabled or disabled by touching the respective touch options/displays. An enabled
option has a highlighted border. While in the UHF AM mode, the cipher option cycles as follows:
CPHR (no highlighted border-cipher disabled), CPHR (border highlighted-cipher baseband enabled),
CPDP (border highlighted-cipher diphase enabled). The CPHR and CPDP options are mutually
exclusive. Continued selection of this option repeats the above cycle. CPHR
(both
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ORIGINAL
A1-E18GA-NFM-000
diphase and baseband) is available for only one radio at a time. Enabling CPHR on COMM 1
automatically disables CPHR on COMM 2 if it was previously enabled.
Selecting the AJ option on this sublevel selects COMM 1 anti-jam mode. If Have Quick is
pre-defined for the current preset, the radio enters Have Quick mode. If SINCGARS is pre-defined for
the current preset, the radio enters SINCGARS. If no data/waveform or time is stored in the radio for
the current preset, NO FILL is displayed in the scratchpad and the radio is in neither Have Quick or
SINCGARS. For Have Quick or SINCGARS data entry, see Have Quick or SINCGARS System
paragraphs, this chapter. Once the radio is in the anti-jam mode it remains in the anti-jam mode, even
if the preset channel is changed using the COMM channel select knob or the Top Level CNI Format
Channel Change paragraph procedure (fast data entry). The anti-jam mode is disabled by touching the
border highlighted AJ touch option/display.
23.3.3 Anti-Jam Operation. There is no AJ or AJ MENU option on the Ship Maritime Preset, Guard
Preset, or Cue Preset Sublevels. The Manual Preset Sublevel has an AJ MENU option but does not
have an AJ option. Anti-Jam operation is described in the Have Quick and SINCGARS System
paragraphs, this chapter.
Figure 23-7. AJ MENU From Fixed Frequency COMM Sublevel
23.3.3.1 AJ MENU From Fixed Frequency COMM Sublevel. Touching the AJ MENU touch
option/display while on the COMM sublevel with a fixed frequency selects the AJ MENU From Fixed
Frequency COMM Sublevel (see figure 23-7). This sublevel initializes with no options selected and
displays a 1: (selected radio) in the scratchpad but does not display the fixed frequency. The AJ fixed
frequency sublevel is used to control Have Quick time, to control SINCGARS coldstart, to manually
load Have Quick fill, and to control Have Quick and SINCGARS zeroize.
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A1-E18GA-NFM-000
The TIME RSTRT option is used to restart the radio clock. To prevent inadvertent selection, this
option requires a double selection to start the radio clock. Touching TIME RSTRT option changes the
touch option/display to RSTRT ENABLE. Touching the RSTRT ENABLE option starts the radio
clock and returns the display to TIME RSTRT. If any option other than RSTRT ENABLE is touched
after touching TIME RSTRT the radio clock is not started and the display returns to TIME RSTRT.
The LOAD DAY option is used to load the Have Quick calendar day. Touching the LOAD DAY
touch option/display border highlights the option and enables calendar day entry by touching the
desired numbers on the keypad options (01 thru 31), verifying the new calendar day in the scratchpad,
and touching the LOAD DAY option. When the calendar day is entered into the radio a tone sounds
in the head set. Touching any other touch option/display removes the border highlight from the LOAD
DAY option and data entry is no longer available.
The ZERO option is used to erase the stored Have Quick word-of-day (WOD) and SINCGARS
transec data. To prevent inadvertent selection, this option requires a double selection to zero radio
data. Touching ZERO option changes the touch option/display to ZERO ENABLE. Touching the
ZERO ENABLE option zeroizes both (COMM 1 and 2) radios. The ZERO ENABLE option is border
highlighted for 2 seconds and the display returns to ZERO. If any option other than ZERO ENABLE
is touched after touching ZERO the radios are not zeroized and the display returns to ZERO.
The RTN option is used to return to the fixed frequency COMM sublevel.
23.4 HAVE QUICK SYSTEM
Have Quick is a slow hopping, UHF, AM line-of-sight jam-resistant voice communication system.
The operation involves coordinating and establishing communications nets. These nets have multiple
users that have the same ECCM information and are time synchronized. The nets are established and
operate with information for a specific word-of-day. The WOD is used to define the frequency hopping
pattern for that day. In conjunction with the WOD, a precise time-of-day (TOD), which is effectively
the net time synchronizer, is also required. The net number and type can be entered using the keypad
options. The three digits to the left of the decimal point are the net number and range from 000 to 999.
The three digits to the right of the decimal point represent type: .025 = HQII (NATO), and .050 = HQII
(non-NATO).
NOTE
The radios do not contain a clock. Time must be set during aircraft
preflight.
The principle functions available for Have Quick control are:
1. Anti-jam (AJ) mode and net selection.
2. Time synchronization including either the reception or the transmission of the TOD.
3. WOD verification and manual entry.
4. Zeroing WOD.
5. Training net control and manual entry.
23.4.1 Have Quick Menu From AJ Menu Fixed Frequency COMM Sublevel. Touching the HQ
MENU touch option/display while on the AJ COMM sublevel with a fixed frequency selects the Have
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Figure 23-8. Have Quick Fixed Frequency Sublevel
Quick fixed frequency sublevel (see figure 23-8). This sublevel initializes with no options selected and
displays a 1: (selected radio) in the scratchpad. This sublevel is used for manual fill operation.
The HQ TIME option is used to transmit or receive Have Quick time. Touching the HQ TIME touch
option/display border highlights the option and enables the use of the RCV and XMIT options. With
HQ TIME selected, touching the RCV touch option/display border highlights the RCV option until
time is received, or until 60 seconds has elapsed. With HQ TIME selected, touching the XMIT touch
option/display border highlights the XMIT option for 2 seconds and time is transmitted. The HQ
TIME option remains border highlighted until HQ VDAY, HQ WOD or HQ TNET is selected.
The HQ VDAY option is used to verify that a Have Quick word-of-day is loaded for a particular day
(see figure 23-9). Touching the HQ VDAY touch option/display border highlights the option and
enables calendar day data entry by touching the desired numbers on the keypad options (01 thru 31),
verifying the new calendar day data entry and then touching the HQ VDAY option. If there is a stored
word of day for the entered calendar day a tone sounds in the head set. The HQ VDAY option remains
border highlighted until HQ TIME, HQ WOD or HQ TNET is selected.
The HQ WOD option is used to manually enter the Have Quick word of day. Touching the HQ WOD
touch option/display border highlights this option and enables Have Quick word-of-day entry by
touching the desired numbers on the keypad options (WOD segments 200.000 thru 399.975 in
increments of 0.025), verifying the word of day in the scratchpad, and touching the WOD # option.
Each word-of-day is six-segments that look like frequencies. When the HQ WOD is first selected, 20
is displayed in the scratchpad followed by the first six-segments of data. There are six individual
word-of-day segments identified by the numbers 20 thru 15. As each six-segment data is entered, the
number decrements thru 15. Trailing zeros need not be entered.
• 1st Segment - 20 000.000 HQ WOD option
• 2nd Segment - 19 000.000 HQ WOD option
• 3rd Segment - 18 000.000 HQ WOD option
• 4th Segment - 17 000.000 HQ WOD option
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Figure 23-9. Have Quick WOD Loading
• 5th Segment - 16 000.000 HQ WOD option
• 6th Segment - 15 000.000 HQ WOD option
The last segment (7th) is calendar day and is only two numbers (01 thru 31). After the calendar day
is entered, the HQ WOD option changes to an unhighlighted border WOD LOAD. No data entry is
available with WOD LOAD displayed. Touching the WOD LOAD option sends the word-of-day to the
radio, the option changes back to an unhighlighted border HQ WOD touch option/display, and a tone
sounds in the head set.
At any time during the data entry of the word- of-day, the border highlighted HQ WOD option may
be used to cycle to the next segment without changing the current segment. If on the calendar day
segment, touching HQ WOD cycles to WOD LOAD without changing the calendar day segment. The
HQ WOD option remains border highlighted until WOD LOAD, HQ TIME, HQ VDAY or HQ TNET
is selected. If HQ WOD data entry is exited before completion, the previously entered segments are
maintained and are displayed in the scratchpad when HQ WOD entry is continued.
Selecting the RTN option returns the Have Quick MENU format to the Fixed Frequency Anti-Jam
Menu format.
The HQ TNET option is used to manually enter the Have Quick 2 training nets (see figure 23-10).
Touching the HQ TNET touch option/display border highlights this option and enables Have Quick
2 training net data entry by touching the desired numbers on the keypad options, verifying the
frequency in the scratchpad, and then touching HQ TNET option. When the HQ TNET is first
selected, 20 is displayed in the scratchpad followed by the first training net frequency. There are 16
training net frequencies identified by the numbers 20 thru 5. As each frequency is entered the number
decrements thru 5. Trailing zeros need not be entered.
• 1st Segment - 20 000.000 HQ TNET option
• 2nd Segment - 19 000.000 HQ TNET option
• 3rd Segment - 18 000.000 HQ TNET option
---- ----------- --
--
----- ---
---
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• 14th Segment - 7 000.000 HQ TNET option
• 15th Segment - 6 000.000 HQ TNET option
• 16th Segment - 5 000.000 HQ TNET option
The valid training net frequencies are:
1.
30.000 thru 87.995 MHz (FM) - at increments of 0.025 MHz,
2.
108.000 thru 173.975 MHz (AM) - at increments of 0.025 MHz,
3.
225.000 thru 399.975 MHz (AM/FM) - at increments of 0.025 MHz.
Figure 23-10. Have Quick TNET Loading
After the last training net frequency is entered, the HQ TNET option changes to an unhighlighted
border TNET LOAD. No data entry is available with TNET LOAD displayed. Touching the TNET
LOAD option sends the training net to the radio, the option changes back to an unhighlighted border
HQ TNET touch option/display and a tone sounds in the head set.
At any time during the data entry of the training net, the border highlighted HQ TNET option may
be used to cycle to the next frequency without changing the current frequency. If on the last training
net frequency, touching HQ TNET cycles to TNET LOAD without changing the last training net
frequency. The HQ TNET option remains border highlighted until TNET LOAD, HQ TIME, HQ
VDAY or HQ WOD is selected. If HQ TNET data entry is exited before completion, the previously
entered frequencies are maintained and are displayed in the scratchpad when HQ TNET entry is
continued.
Selecting the RTN option returns the Have Quick MENU format to the Fixed Frequency Anti-Jam
Menu format.
23.4.2
SINCGARS Menu From AJ Menu Fixed Frequency COMM Sublevel. Touching the SG
MENU touch option/display while on the AJ COMM sublevel with a fixed frequency selects the Single
Channel Ground and Airborne Radio System (SINCGARS) MENU fixed frequency sublevel (see
figure 23-11). This sublevel initializes with no options selected and displays a 1: (selected radio) in the
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scratchpad. This sublevel is used for SINCGARS coldstart operation. The SINCGARS coldstart
operation is used for receiving or transmitting SINCGARS hopsets and locksets so a user can be added
to the net. There is a 30 second time-out during option selections.
Figure 23-11. Single Channel Ground and Airborne Radio System (SINCGARS) MENU
Fixed Frequency Sublevel
The SG LSET is used to enter the SINCGARS lockset for transmission or reception. Touching the
SG LSET touch option/display border highlights the option and the last lockset is displayed in the
scratchpad. The lockset may be changed by touching the desired number on the keypad options (1 thru
8), verifying the new lockset in the scratchpad, and touching SG LSET option. With the desired lockset
displayed in the scrathpad, the lockset is transmitted or received by touching the XMIT or RCV
option. Touching the XMIT option transmits the new radio lockset and the option is border
highlighted for 2 seconds. Touching the RCV option enables the radio to receive the lockset and the
option remains border highlighted until the lockset is received.
Touching the SG HSET touch option/display border highlights the option and the last hopset is
displayed in the scratchpad. The hopset may be changed by touching the desired number on the
keypad options (1 thru 20), verifying the new hopset in the scratchpad, and touching SG HSET option.
With the desired hopset displayed in the scratchpad, the hopset is transmitted or received by touching
the XMIT or RCV option. Touching the XMIT option transmits the new radio hopset and the option
is border highlighted for 2 seconds. Touching the RCV option enables the radio to receive the hopset
and the option remains border highlighted until the hopset is received. The XMIT and RCV options
can not be selected at the same time.
Selecting the RTN option returns the SINCGARS MENU format to the Fixed Frequency Anti-Jam
Menu format.
23.4.3 COMM Sublevel - Presets 1 Thru 20 (Anti-Jam). The Preset 1 thru 20 COMM Sublevel
(Anti-Jam) is selected by touching the COMM 1 or 2 touch option/display while on preset channel 1
thru 20 and in Have Quick or SINCGARS anti-jam mode (see figure 23-12).
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Figure 23-12. COMM Sublevel - Presets 1 to 20 (Anti-Jam)
In the Have Quick mode, this sublevel is used to change the net number, to enable or disable squelch,
cipher mode, guard receive, to select modulation type (AM or FM); or to access time receive and time
transmit.
In the SINCGARS mode, this sublevel is used to enable or disable squelch, cipher mode, guard
receive, to access master selection; to enter late net selection; to enter time; and to transmit and receive
hopsets and locksets. This sublevel, displays a 1: (selected radio) followed by H1 (Have Quick 1), H2
(Have Quick 2, or SG (SINCGARS) and the net number. In Have Quick mode, the net number (00.000
thru 99.950) is changed by touching the desired numbers on the keypad options, verifying the new net
number in the scratchpad, and touching the desired mode. The last two digits of the net number must
be 00, 25 or 50. Trailing zeros need not be entered. If invalid data is entered, an error indication is
displayed in the scratchpad. The SINCGARS net number cannot be changed at this sublevel.
SQCH (squelch) and GRCV (guard receive) are enabled or disabled by touching the respective touch
options/displays. An enabled option has a highlighted border. The AM/FM option is always border
highlighted and toggles between AM and FM. If the current frequency is available only in AM or in
FM, the AM/FM option is not displayed. While in the UHF AM mode, the cipher option cycles as
follows: CPHR (no highlighted border-cipher disabled), CPHR (border highlighted-cipher baseband
enabled), CPDP (border highlighted-cipher diphase enabled). The CPHR and CPDP options are
mutually exclusive. Continued selection of this option repeats the above cycle. CPHR (both diphase
and baseband) is available for only one radio at a time. Enabling CPHR on COMM 1 automatically
disables CPHR on COMM 2 if it was previously enabled.
Touching the AJ option returns the selected radio to the COMM fixed frequency sublevel. This
selection applies to all presets and all preset channels which now become fixed frequency.
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Touching the AJ MENU option selects the Have Quick or SINCGARS menu sublevel depending on
whether the current preset is defined as Have Quick or SINCGARS.
If the radio is in anti-jam mode but there is no valid data/waveform or time stored in the current
radio for the current preset channel, the AJ option changes to AJ NO FILL (see figure 23-13). The
AM/FM and AJ MENU options are not displayed when a NO FILL condition exists on the current
preset channel. In this condition, an A is displayed in the scratchpad and a Have Quick net number
may be entered.
Figure 23-13. AJ MENU From Have Quick COMM Sublevel
23.4.4 AJ MENU From Have Quick COMM Sublevel. Touching the AJ MENU touch option/display
while on the COMM sublevel with a Have Quick anti-jam mode selects the AJ Have Quick menu
sublevel initialized with the HQ TIME option selected and border highlighted (see figure 23-14). This
sublevel is used to transmit and receive Have Quick time. The scratchpad information is the same as
scratchpad information on the Have Quick COMM sublevel.
The HQ TIME option is used to transmit or receive Have Quick time while the radio is operating on
a Have Quick net. With the HQ TIME touch option/display border highlighted the option enables the
use of the RCV and XMIT options. Touching the RCV touch option/display border highlights the RCV
option until time is received or until 60 seconds have elapsed. Touching the XMIT touch option/
display border highlights the XMIT option for 2 seconds and time is transmitted.
Selecting the RTN option returns the format to the AJ COMM sublevel.
23.5 SINCGARS SYSTEM
The radio can be operated with SINCGARS, which provides jam resistant line-of-sight (LOS) voice
communications in the VHF band employing frequency hopping. Established communication nets
require a TOD that is coordinated and used by all net users. The system also contains encoded locksets
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Figure 23-14. AJ Have Quick Menu Sublevel
and hopsets that define the set of frequencies that will be hopped on and will not be hopped on. The
system can store multiple nets correlating to hopsets and locksets. The principle functions available for
SINCGARS control are:
a. SINCGARS mode (AJ) selection.
b. Time reception and transmission.
c. Late net entry.
d. Electronic remote fill (ERF).
e. Cue operation.
f. Coldstart.
23.5.1 AJ MENU From SINCGARS COMM Sublevel. Touching the AJ MENU touch option/display
while on the COMM sublevel with a SINCGARS anti-jam mode selects the AJ SINCGARS menu
sublevel (see figure 23-15) and may initialize with the MSTR option or LATE ENTRY option selected,
or no options selected. This sublevel is used to select MSTR (master operation), to select LATE
ENTRY (late entry operation), to enter time, and to transmit and receive hopsets and locksets.
The MSTR option is used to select master control of the net. Automatic time synchronization is
achieved by each of the net radios every time a transmission is received from the master. If the MSTR
option is border highlighted, master control of the net is enabled. If MSTR is not border highlighted,
master control of the net is disabled. The MSTR option toggles between control and no control.
The TIME option is used to enter time. Each user can enter the SINCGARS time. The time can be
used by the master to synchronize the rest of the net or to get on the net using late entry. Touching the
TIME option/display border highlights this option, a D, H, and M is displayed in the scratchpad, and
time data entry is enabled. The time may be entered in D (day), H (hour) and M (month) format by
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Figure 23-15. AJ MENU From SINCGARS COMM Sublevel
touching the desired number on the keypad options, verifying the new time in the scratchpad and
touching TIME option. Trailing zeros need not be entered. If invalid data is entered, ERROR is
displayed in the scratchpad.
The LATE ENTRY is used to gain late entry into the net. Touching the LATE ENTRY
option/display border highlights the option and enables late entry into the SINCGARS net. This
option remains border highlighted until time synchronization into the net is achieved.
Touching the ERF (Electronic Remote Fill) option selects the AJ SINCGARS ERF sublevel (see
figure 23-16). ERF allows the system to be filled electronically over the air by another net user who has
the required net data (hopsets/locksets). The net user can either provide or receive the net data. The
Figure 23-16. AJ SINCGARS ERF Sublevel
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desired hopset/lockset can be selected one at a time for either transmission or reception. The process
is repeated until all desired sets are transmitted/received. This sublevel initializes with no options
selected and displays a 1: (selected radio) in the scratchpad. This sublevel is used for SINCGARS
coldstart operation. The SINCGARS coldstart operation is used for receiving or transmitting
SINCGARS hopsets and locksets so a user can be added to the net. There is no 30 second time-out
during option selections.
The SG LSET is used to enter the SINCGARS lockset for transmission or reception. Touching the
SG LSET touch option/display border highlights the option and the last lockset is displayed in the
scratchpad. The lockset may be changed by touching the desired number on the keypad options (1 thru
8), verifying the new lockset in the scratchpad, and touching SG LSET option. With the desired lockset
displayed in the scratchpad, the lockset is transmitted or received by touching the XMIT or RCV
option. Touching the XMIT option transmits the new radio lockset and the option is border
highlighted for 2 seconds. Touching the RCV option enables the radio to receive the lockset and the
option remains border highlighted until the lockset is received.
Touching the SG HSET touch option/display border highlights the option and the last hopset is
displayed in the scratchpad. The hopset may be changed by touching the desired number on the
keypad options (1 thru 20), verifying the new hopset in the scratchpad, and touching SG HSET option.
With the desired hopset displayed in the scratchpad, the hopset is transmitted or received by touching
the XMIT or RCV option. Touching the XMIT option transmits the new radio hopset and the option
is border highlighted for 2 seconds. Touching the RCV option enables the radio to receive the hopset
and the option remains border highlighted until the hopset is received. The XMIT and RCV options
can not be selected at the same time.
Figure 23-17. Guard Transmit on Top Level CNI Format
Selecting the RTN option returns the AJ SINCGARS ERF format to the AJ SINCGARS menu
sublevel. Selecting the RTN option again returns the AJ SINCGARS menu sublevel to the COMM
sublevel that is in the SINCGARS AJ mode.
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Figure 23-18. Guard Transmit on COMM Sublevel
23.5.2
Guard Transmit on Top Level CNI Format. On the top level CNI format, placing the COMM
G XMT switch on the ACI panel to 1 or 2 selects guard transmit for that radio and GXMT replaces
the COMM touch option/display (see figure 23-17). The COMM sublevel also displays GXMT in the
scratchpad (see figure 23-18).
23.6 KY-58 - SECURE SPEECH SYSTEM
The secure speech system is used for ciphering (coding) or deciphering (decoding) audio routed
through the COMM 1 and COMM 2 receiver-transmitters. The system consists primarily of the KY-58
control panel assembly on the right console. Controls and indicators are on the KY-58 control panel
assembly and on the COMM control panel on the left console.
23.6.1 KY-58 Control Panel Assembly. The control panel assembly functions as a ciphering or
deciphering device for secure speech operation.
23.6.1.1 Ciphered Transmission. During ciphered transmissions, audio from the microphone is
routed through the COMM control panel to the KY-58 control panel assembly where it is enciphered.
The enciphered audio is routed back to the COMM control panel, then to COMM 1 or COMM 2
receiver-transmitter for transmission.
23.6.1.2 Ciphered Reception. During reception of ciphered information, the ciphered audio is
routed from the COMM 1 or COMM 2 receiver-transmitter to the COMM control panel, then to the
control panel assembly for deciphering. Deciphered audio is routed to the COMM control panel and
the headset.
23.6.1.3 Ciphered Relay Mode. During ciphered relay mode of operation, ciphered information
received on one radio is routed from the radio, through the COMM control panel to the second radio
for transmission. Ciphered information received on the first radio is also routed through the COMM
control panel to the KY-58 control panel assembly for deciphering. Deciphered audio is routed through
the COMM control panel to the headset. This enables the crewmember to hear deciphered relayed
audio in the ciphered relay mode. When cipher is selected on the COMM control panel immediately
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Figure 23-19. KY-58 Control Panel Assembly
after operating in relay plain, COMM 1 plain, or COMM 2 plain mode of operation, the crewmember
must press the transmit key for either COMM 1 or COMM 2 two times to enable ciphered relay
operations. When the relay aircraft is operating both radios within the same bandwidth, the two
frequency selections must be separated by a minimum of 10 MHz.
23.6.2 KY-58 Controls and Indicators. The only cipher control on the COMM control panel is the
RLY CIPHER/PLAIN switch (relay switch). The controls on the KY-58 control panel assembly are the
MODE select knob, unlabeled fill select knob, VOLUME control knob, and the unlabeled power select
knob (see figure 23-19).
23.6.2.1 KY-58 Mode Select Knob. The mode select knob has positions of P, C, LD, and RV. Placing
the knob to P enables plain mode of operation. Placing the knob to C enables the cipher mode of
operation. With the knob set to LD the load mode of operation is enabled. This mode is used for
loading data into the KY-58 control panel assembly. Information pertaining to the RV knob position
(receiver variable) will be supplied later.
23.6.2.2 KY-58 Fill Select Knob. The fill select knob has positions of 1 thru 6, a Z 1-5 position, and
a Z ALL position. Setting the knob to one of the six positions selects the position to be loaded with
data. Placing the knob to Z 1-5 zeroizes data in positions 1 thru 5. Placing the knob to Z ALL zeroizes
all data in positions 1 thru 6.
23.6.2.3 KY-58 Volume Control Knob. The volume control knob adjusts the volume of the KY-58
control panel assembly audio. The volume control knob should be set to full volume position during
secure voice transmission and reception.
23.6.2.4 KY-58 Power Knob. This knob has positions of ON, OFF, and TD. Placing the knob to ON
turns on power to the KY-58 control panel assembly if cipher mode has been selected. Placing the knob
to OFF removes power to the system. With the knob in TD, power is turned on for the system if cipher
mode has been selected and a time delay is selected for data processing. The knob must be in the TD
position for ciphered relay operations.
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23.6.3 KY-58 Operation. Other stations or aircraft involved in cipher or cipher relay communication
must be in either the baseband or diphase mode.
1. COMM 1 and COMM 2 radios - ON
COMM 1 and COMM 2 radios are turned on and volume adjusted with the VOL 1 and 2 COMM
control knobs on the UFCD.
2. COMM 1 and COMM 2 channels - AS DESIRED
a. COMM 1 and COMM 2 channel select knobs - ROTATE (to select desired channel).
Selected channel is displayed in COMM 1 and 2 touch option/display on the UFCD.
3. COMM 1 and COMM 2 channel frequency - SET
a. COMM 1 and COMM 2 touch option/display - TOUCH
Channel number and frequency displayed in scratchpad GRCV, SQCH, and CPHR options
appear on the option/display.
b. Channel frequency - AS DESIRED
Enter new frequency with keypad. Press the desired Comm option to enter the new frequency.
4. CPHR touch option/display - TOUCH
The CPHR touch option/display is border highlighted and a series of tones are heard for 3
seconds indicating cipher is enabled with baseband operation. Touching the CPHR touch
option/display again changes the display to CPDP with the border highlighted and enables cipher
diphase mode.
23.6.3.1 KY-58 Cipher Mode. Other stations or aircraft involved in cipher communication must have
the KY-58 fill select knob in the same position.
1. KY-58 power knob - ON
2. KY-58 MODE knob - C
3. KY-58 VOLUME knob - ADJUST TO MAX VOLUME
4. COMM switch on inboard throttle - ACTUATE
UP for COMM 1, DOWN for COMM 2. A short tone is heard in the headset.
23.6.3.2 KY-58 Relay Mode. Relay mode can operate in Plain, Cipher and ECCM mode. Other
stations or aircraft involved in cipher relay communication must have the KY-58 fill select knob in the
same position.
1. KY-58 power knob - TD
Other stations or aircraft involved in cipher relay communication must have the KY-58 power
knob in the TD position.
2. KY-58 mode knob - C
3. KY-58 volume knob - ADJUST TO MAX VOLUME
4. COMM 1 antenna select switch - AUTO
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5. Relay switch select - CIPHER
6. COMM switch on inboard throttle - ACTUATE
UP for COMM 1, DOWN for COMM 2. A short tone is heard in the headset.
NOTE
When entering the cipher relay mode from any plain mode, the Comm
1/Comm 2 transmit switch must be keyed twice; once to initialize the
KY-58 and a second time to transmit.
23.7 DIGITAL COMMUNICATION SYSTEM (DCS)
DCS provides all of the standard voice communication capabilities of earlier ARC-210 radios, plus
a digital data mode that greatly reduces pilot workload during Close Air Support (CAS) missions. It
enables the pilot to receive 9 line briefs, communicates target and mission data digitally from the
Forward Air Controller (FAC), and provides the capability to feed this information to weapon targeting
and navigation systems. Currently, this mission is handled via verbal communication and manual data
entry. A new communication control panel, incorporated with the Multifunctional Information
Distribution System (MIDS), is needed to interface with the DCS.
In the frequency range of 118.000 through 136.975 MHz, the DCS can be tuned to 8.3 KHz channels
to facilitate air traffic control communications in European air space. Tuning the radio to these
frequencies is performed via the UFCD as in any other band. In this band, however, the entered
frequency is not the actual tuned RF frequency. Refer to figure 23-20 for the convention adopted by
the International Civil Aviation Organization (ICAO).
Actual RF Frequency (MHz)
UFCD Frequency (MHz)
Channel BW (KHz)
118.0000
118.000
25
118.0000
118.005
8.3
118.0083
118.010
8.3
118.0166
118.015
8.3
118.0250
118.020
25
118.0250
118.025
25
118.2500
118.030
8.3
118.0333
118.035
8.3
118.0416
118.040
8.3
118.0450
118.045
25
118.0500
118.050
25
118.0500 thru 136.9750
118.55 thru 136.975
8.3 or 25
Figure 23-20. DCS Frequencies Conversions
23.7.1 VHF/UHF Communication System - DCS. The aircraft voice communications system consists
of an ARC-210 radio (COMM 1), a ARC-210/DCS radio (COMM 2), and KY-58 Secure Speech
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Equipment. DCS provides its own integrated secure speech encoder/decoder which allows COMM 1
and COMM 2 radios to simultaneously operate in cipher mode.
NOTE
The aircraft COMM 2 radio can also be installed with an ARC-210. In
this configuration, the KY-58 is shared between COMM 1 and COMM
2 as in earlier aircraft.
When operating the COMM 2 radio (either ARC-210 or DCS) in a band that allows selecting AM or
FM, make sure the modulation is selected before the frequency is entered. Failure to do this may not
allow the selected modulation to be accepted into memory.
23.7.1.1 ARC-210/DCS. DCS has additional capabilities which do not exist in the ARC-210. One
such capability is two-way digital data communications using Variable Message Format (VMF) for the
CAS mission. Another is storage of the cryptographic keys COMSEC communications. Finally, 8.3
KHz channel spacing is provided in the 118.00 through 136.975 MHz for Air Traffic Control (ATC)
communications required in European airspace.
23.7.1.1.1 COMM 1 and COMM 2 Volume Controls. The volume of the COMM 1 and COMM 2
radios is controlled by volume controls on the UFC.
23.7.2 DCS Communications Security (COMSEC).
23.7.2.1 Operation. During ciphered transmissions, audio from the aircrew’s microphone is routed
through the ACI panel to the DCS where it is encrypted. During reception of ciphered information, the
ciphered audio is deciphered by the DCS. The deciphered audio is routed back through the ACI panel
to the aircrew’s headset.
23.7.2.2 DDI Controls. Control of the internal DCS cryptographic functions is performed via the
DCS KEY display from the UFC. The DCS KEY display is accessed by selecting DCS on the SUPT
menu, then selecting DCSKY on the NETS (network) display. See figure 23-21. The functions
displayed are crypto keys (KEY1 thru KEY6) and TD (time delay). If one cockpit has the DCS KEY
display accessed, the other cockpit can access it by selecting only DCS on the SUPT menu.
23.7.2.2.1 TD Control. The time delay mode is enabled by selecting/boxing TD on the DCS KEY
display. A subsequent selection disables time delay and removes the box. The effect of enabling time
delay mode does not take place until CPHR or CPDP has been selected via the UFCD.
23.7.2.2.2 Crypto Key Options. There are six available crypto keys. For example, if KEY1 is loaded
with crypto key data, the option KEY1 appears on the display. If a crypto key has not been loaded with
data, that key option is not displayed. A selected crypto key is indicated with a box around the
corresponding option. Only one crypto key may be selected at a time.
The DCS KEY display initializes to the previously selected crypto key. If the last crypto key selected
has been zeroed, the system selects the next available loaded crypto key. The DCS KEY display
defaults with KEY1 selected.
If CPHR or CPDP is selected and the normal default crypto key has been zeroized, NO FILL is
displayed on the UFCD scratchpad. When the DCS KEY display is selected, NO FILL is removed from
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ORIGINAL
A1-E18GA-NFM-000
the scratchpad. If no crypto keys are loaded, no crypto key options are displayed and a NO KEYS
status appears.
If CPHR or CPDP is selected prior to entering the DCS KEY display, an additional DCS COMSEC
status check is performed upon selection of a crypto key. This check takes approximately 1.5 to 2
seconds. If the DCS COMSEC function is operational there is no change on the DCS KEY display. The
boxed option with the CIPHER ON status indicator means the selected key is valid for use and DCS
COMSEC is operational.
If the status check determines there is a problem with the COMSEC function, the selected/boxed
crypto key option is Xd and a DCSCS advisory appears. However, it is possible the DCS COMSEC
function may be operational with other loaded crypto key options. Each crypto key option would have
to be selected (in CPHR or CPDP mode) to determine if the DCS COMSEC function is inoperable.
An Xd crypto key option may still be selected. If it is selected and the COMSEC error is no longer
indicated, the X is removed. All Xd status indications are cleared upon MC power-up.
If there is a problem with the DCS/COMSEC function, the boxed crypto key variable is covered by
an X. This indicates that DCS COMSEC function is inoperable with the selected crypto key. This does
not rule out the possibility the DCS COMSEC function may be operational with the other loaded
crypto keys. Each of the other crypto keys would have to be selected while in cipher or cipher diphase
modes before it could be determined the DCS COMSEC function is completely inoperable.
When a crypto key is unavailable and the applicable COMM switch is activated, a continuous audio
tone is heard in the headset.
23.7.3 UFCD - DCS. For normal UFCD operations, refer to Part 1, Section 2, or Part 7, Section 23.
23.7.3.1 ZEROIZE Function. Zeroization of DCS and KY-58 COMSEC KEYS, as well as TRANSEC
KEYS including HQ WODs (HAVEQUICK word of day) and SINCGARS EP (electronic protection),
is accomplished using the UFCD. The selection of the ZERO option causes the display to change to
ZERO ALL ENABLE, and clears the COMSEC and TRANSEC KEYS in the radios and KY-58. Both
COMSEC and TRANSEC KEYS are also zeroized upon pilot ejection. The ZERO ALL ENABLE
option is border highlighted for two seconds, and then the option returns to displaying ZERO. While
the ZERO ALL ENABLE option is displayed, selecting any option other than ZERO ALL ENABLE
causes the option to return to ZERO.
The DCS has an internal battery which is used to maintain the COMSEC KEYS in radio memory
during aircraft power transients and when aircraft power is removed. It also provides the energy to
zeroize the radio when the pilot ejects or if the radio is removed from the aircraft.
23.7.4 Relay Mode Of Operation. During cipher relay mode of operation using a DCS and an
ARC-210, encrypted information received on one radio is routed through the ACI panel to the second
radio for transmission. The encrypted information received on the first radio is also routed through the
ACI panel to the KY-58 for deciphering. The decrypted audio is routed back to the ACI panel, then to
the aircrew’s headset.
The DCS COMSEC functions are not utilized during the cipher relay mode. In this mode the DCS
is always commanded to the plain voice mode, and all crypto relay transmissions are encrypted/
decrypted by the KY-58.
Certain constraints apply if cipher relay is selected. If COMM 2 is an ARC-210, the above constraints
do not apply.
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Figure 23-21. DCS KEY Display
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Cipher relay operation must be performed within the COMM 1 and COMM 2 relay band limitations
outlined in figure 23-22.
NOTE
With CPHR or CPDP enabled, selection of PLAIN on the
RLY
selector switch (ACI panel) does not activate plain relay mode.
REMOTE
RELAY AIRCRAFT
REMOTE
STATION
COMM 1
COMM 2
STATION
1 OR 2
2 OR 1
A
*A
*A
A
B
*B
*B
B
C
*C
*C
C
D
*D
*D
D
E
*E
*E
E
A
A
C
C
C
C
A
A
A
A
D
D
D
D
A
A
C
C
D
D
D
D
C
C
B
B
E
E
E
E
B
B
A - 30.000 MHz to 87.975 MHz
B - 118.000 MHz to 155.975 MHz
* - When the relay aircraft is operating both radios
C - 156.000 MHz to 173.975 MHz
within the same band, the two frequency selec-
D - 225.000 MHz to 399.975 MHz
tions must be separated by a minimum of 10 MHz.
E - 225.000 MHz to 399.975 MHz
NOTE: Both remote stations and the relay aircraft must have the KY-58 power knob in the TD positions.
Figure 23-22. Relay Bandwidth Limitations
23.7.5 DCS - Avionics Subsystem.
23.7.5.1 Mission Computer System. Channels 2 and 4 link the mission computer to DCS.
23.7.5.1.1 Mission Initialization. The DMD provides the capability to load the following mission
initialization files: COMM, DCS CAS, DCS NETS, and WYPT S/S. The COMM file contains the radio
presets, HAVE QUICK and SINCGARS data. The DCS CAS file contains pre-planned VMF FTXT
(free text) messages, pre-planned VMF 9-line brief messages, and an empty data file reserved for
inflight received CAS and/or FTXT messages. The DCS NETS file contains a set of network
parameters to be used for a unique network environment used in VMF message communications. The
WYPT S/S file contains a list of waypoint names for the IP (initial point) and control points that are
either entered or received in CAS 9-line briefs. See figure 23-23.
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Figure 23-23. MUMI Displays
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23.7.5.2 Status Monitoring.
23.7.5.2.1 Cautions and Advisories. DCS has the ability to trigger eight advisory messages;
COM1H(2H), COM1S(2S), COM1L(2L), BIT and DCSCS. COM1H(2H) is triggered when HAVE
QUICK time is not loaded. COM1S(2S) is triggered when SINCGARS time is not loaded. COM1L(2L)
advisory is triggered by an error in the MC to radio data loading process. BIT is triggered when a failure
is detected by BIT. DCSCS is triggered when a COMSEC failure is detected.
23.7.5.2.2 BIT Top Level Display. The top level BIT display for DCS is the same as the COM2
format. Status is indicated for DCS as COMM2. See figure 23-24.
23.7.5.2.3 COMM BIT Sub-Level Display. The COMM sub-level BIT display appears when the
COMM option on the top level BIT display is selected. The COMM BIT display for DCS is the same
as the ARC-210 with the DCS being represented as COM2.
a. DCS Option. Initiated BIT is run by selecting the COM2 option. DCS status is displayed in the
center of the page represented as COM2.
23.7.5.2.4 Software Configuration. The software configuration for the DCS is checked by selecting
CONFIG on the top level BIT display.
23.8 IDENTIFICATION FRIEND OR FOE (IFF)/COMBINED INTERROGATOR TRANSPONDER (CIT)
The AN/APX−111 CIT is a dual purpose Identification Friend or Foe (IFF) system with
transponder and interrogator capabilities. The transponder provides automatic identification of the
aircraft in which it is installed when challenged by a surface or airborne interrogator set and provides
momentary identification of position (I/P) upon request. The interrogator provides airborne target
identification capabilities.
23.8.1 IFF Transponder. The transponder system operates in Modes 1, 2, 3, 4A, 4B, C and S. Modes
1, 2, and 3 are selective identification feature (SIF) modes. Modes 4A and 4B are the crypto modes.
Mode C is the altitude reporting mode. Mode S is used in conjunction with the Civil Air Traffic Control
Surveillance System.
With the IFF Programming (IFF PROG) page: A) Mode 1, 2, and 3 codes can be automatically
programmed to change at specified times or on a time interval, B) Mode 1, 2, 3, 4, C, and S can be
automatically programmed to enable/disable when the aircraft crosses a designated waypoint in a
specified direction, and C) Mode 4 can be automatically updated on Zulu day transition. The IFF can
also be programmed during mission planning.
The IFF emergency mode automatically becomes active upon ejection or can be manually selected
with the IFF MASTER switch.
23.8.1.1 IFF on Top Level CNI UFCD Format. On the top level CNI UFCD format, IFF power
application is identified by a corner highlight in the upper left corner of the IFF option. The option
displays the current Mode 1 and Mode 3 codes regardless of whether the IFF is powered or whether the
mode is enabled. The Mode 1 code may be changed by selecting two valid numbers (first digit equal
to 0−7, second digit equal to 0−3) and selecting the IFF option. Mode 2 and Mode 3 codes may be
changed by selecting four valid numbers (each digit equal to 0−7) and selecting the IFF option.
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Figure 23-24. BIT Displays
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Figure 23-25. IFF Transponder UFCD Sublevel
23.8.1.2 IFF Transponder UFCD Sublevel. The IFF Transponder (XPOND) UFCD sublevel is
displayed by selecting the IFF option before entering any data in the scratchpad (figure 23−25). This
sublevel is used to control power to the IFF system, to enable the transponder modes, to set Mode 1,
2, and 3 codes, to select Mode 4A or 4B, to view Mode S status, to set the temporary Mode S address,
and to select the Mode S sublevel. (See 23.8.1.2.1 for Mode S operation.)
The IFF is on when the ON/OFF option is corner highlighted and displays ON. The IFF system is
off when the option is not corner highlighted and displays OFF.
The Mode 1, 2, 3/C, 4A/4B options are border highlighted when selected for enable. A mode option
without a border highlighted is not selected for enable. Modes 1, 2, 3 and C may be selected for enable
or disable when the IFF system is either on or off. The IFF must be on to select Modes 4A or 4B. Any
mode that is border highlighted with the IFF system on is immediately enabled; any mode that is
border highlighted with the IFF system off is automatically enabled when the IFF system is turned on.
Modes 1 and 2 are enabled and disabled by selecting the respective option. When neither Mode 3 nor
Mode C is enabled, selecting the Mode 3/C option results in the following sequence: both Mode 3 and
Mode C enabled − Mode 3 enabled and Mode C disabled − both Mode 3 and Mode C disabled (figure
23−26). The altitude encoding mode uses 29.92 inches Hg as a reference. When the KIV−6 is installed
and the IFF is on, Mode 4A or Mode 4B can be enabled. Selecting the Mode 4A option results in the
following sequence: Mode 4A enabled − Mode 4A disabled and legend changes to 4B − Mode 4B
enabled − Mode 4B disabled and legend changes to 4A. If the KIV−6 is not installed or the IFF is off,
the Mode 4A/4B option is not displayed.
The Mode 1 code may be changed by selecting two valid numbers (first digit equal to 0−7, second
digit equal to 0−3) and selecting the Mode 1 option. The Mode 2 and 3 codes may be changed by
selecting four valid numbers (each digit equal to 0−7) and selecting the respective Mode option.
23.8.1.2.1 Mode S Mode S is a Civil Air Traffic Control Surveillance System that can respond to
selective interrogations and provide air−to−air and air−to−ground data of aircraft ID, state, and intent
information. The carriage and operation of Mode S Elementary Surveillance functionality applies to
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ORIGINAL
A1-E18GA-NFM-000
Figure 23-26. Mode 3 and Mode C Selection
aircraft that fly Instrument Flight Rules (IFR) and Visual Flight Rules (VFR) flights in Mode S
designated airspace.
The integration of Mode S Level 2 into Navy aircraft is divided into two surveillance levels,
Elementary (EL) and Enhanced (EN). It is beneficial to air traffic control to incorporate Enhanced
Surveillance to the extent practical on all Navy aircraft and to populate Enhanced Surveillance data
parameters to the extent permitted by existing aircraft sensors. As a result of the requirements,
Elementary Mode S is incorporated via a software modification to the CIT system. The system
provides most of the functionality of Enhanced Mode S, but for flight planning purposes only
Elementary Mode S is supported.
When Elementary Surveillance is selected, the aircraft transmits the following data:
1. 24 bit aircraft address
2. Secondary Surveillance Radar (SSR) Mode 3/A
3. Aircraft Identification (call sign used in flight)
4. Transponder Capability Report
5. Altitude reporting in 100 ft intervals
6. Flight Status (airborne/on ground)
When Enhanced Surveillance is selected, the aircraft transmits the following data:
1. Elementary Surveillance data
2. Magnetic Heading
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3. Indicated Airspeed
4. Mach No.
5. Vertical Rate
6. Roll Angle
7. Track Angle Rate
8. True Track Angle
9. Ground Speed
All Mode S equipped aircraft have a permanent Mode S address which is assigned to the aircraft
BuNo. The permanent address is stored in DFIRS. A temporary Mode S address may also be used.
When available, the temporary address overrides the permanent address. Once a temporary Mode S
address has been entered, to revert back to the permanent Mode S address, it is necessary to enter the
permanent address as a temporary address.
The use of the same Mode S address in any two airborne aircraft presents
a safety of flight risk as air traffic computers cannot differentiate between
the two aircraft.
The MC requests the permanent Mode S address from DFIRS when Mode S is enabled and a
temporary Mode S address is not available. The permanent address is displayed on the Electronic
Boresight Constant (EBC) Entry sublevel when available with WonW. This is where the aircraft BuNo
and permanent address can be entered by maintainers prior to flight. Figure 23−27 demonstrates the
path to the EBC to verify the BuNo and permanent address.
NOTE
If ERROR flashing persists with attempts to enter a valid address, this
indicates a DFIRS malfunction.
The Mode S transponder transmits acquisition squitters (unsolicited transponder replies) to permit
passive acquisition by interrogators. The acquisition squitter function is disabled if Mode S is turned
off.
Prior to takeoff, the aircrew can check the availability/status of Mode S, Mode S acquisition squitter,
permanent Mode S address, temporary Mode S address, and aircraft call sign. The aircrew can enter
an A/C call sign if desired or if mission planning does not provide one. The default A/C call sign
contains VV followed by the aircraft’s BuNo.
Mode S and the acquisition squitter function in the same manner during dual and single MC
operation. In the event that power is removed from both MC1 and MC2, Mode S data ages out. The
CIT continues to provide Mode S transmissions in Level 1 mode, providing the Mode S address at a
minimum.
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ORIGINAL
A1-E18GA-NFM-000
Figure 23-27. Electronic Boresight Constant (EBC) Display with W on W
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ORIGINAL
A1-E18GA-NFM-000
Figure 23-28. XPOND Format Selection to Enable Mode S Enhanced and Squitter
1. Mode S Option on Transponder UFCD Sublevel. With the IFF system on, the Mode S
option on the UFCD Transponder (XPOND) sublevel indicates the current status of the Mode S
transponder (figure 23−28). The first line of the Mode S option indicates the selected Mode S
surveillance and acquisition squitter options. Enhanced surveillance is indicated by
EN and
Elementary surveillance byEL. AnS after the slash indicates the squitter is enabled (e.g., S−EN/S)
and a dash indicates the squitter is disabled (e.g., S−EN/−) (figure 23−29). The second and third lines
indicate the temporary Mode S address. When a mission planning input is available, those Mode S
surveillance and acquisition squitter options and the temporary address are displayed. Otherwise, the
system defaults to Enhanced surveillance and squitter enabled (S−EN/S). Regardless of the Mode S
options selected, Mode S is disabled at power up.
The first selection of the Mode S option boxes the option and enables the displayed Mode S
functions. The second selection of the Mode S option displays the Mode S UFCD sublevel (figure
23−30).
If neither the permanent nor temporary Mode S address is available, Mode S is disabled, the Mode
S option is Xd out, and the first line displaysS−. If no temporary address has been provided by
mission planning or aircrew entry, all zeroes (00000000) are displayed (figure 23−31). A new temporary
address can be entered by selecting eight valid numbers (all digits equal to 0−7 and can not contain all
7’s or all 0’s) and selecting the Mode S option.
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ORIGINAL
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Figure 23-29. Return to XPOND Format with Squitter Disabled
2. Mode S UFCD Sublevel. The Mode S sublevel is used to enable/disable the acquisition
squitter, select Enhanced or Elementary surveillance, and enter the aircraft call sign and temporary
address (figure 23−30). If the aircrew changes Mode S selections and disables Mode S, the aircrew’s
selections return when Mode S is re-enabled.
a. Temporary Mode S Address. The temporary Mode S address is displayed on the TEMP S option.
The temporary address can be provided via mission planning or aircrew entry. If a temporary address
is not available, all zeros (00000000) are displayed. A new temporary address can be entered by
selecting eight valid numbers (all digits equal to 0−7 and can not contain all 7’s or all 0’s) and selecting
the TEMP S option.
b. Mode S Surveillance Level. The Mode S Enhanced (S−EN) and Elementary (S−EL) Surveillance
level options are mutually exclusive. Selection of either option enables that option and disables the
other option. If neither option is enabled, enabling one option also enables the acquisition squitter (S
ACQ SQUIT). If both options are disabled, Mode S and the acquisition squitter are disabled.
c. Mode S Acquisition Squitter. Selecting the Mode S acquisition squitter (S ACQ SQUIT) option
toggles the squitter between enabled and disabled. When the squitter is disabled by selecting the
option, it remains disabled until enabled again by aircrew. The squitter is also disabled when Mode S
is not selected (S−EN and S−EL are deselected at the same time). Whether the squitter was disabled
by the S ACQ SQUIT option or S−EN and S−EL deselect, selecting S ACQ SQUIT enables S ACQ
SQUIT and the previous Mode S surveillance level (S−EN or S−EL). Squitter status is also displayed
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Figure 23-30. Mode S UFCD Sublevel
on the XPOND sublevel Mode S option. AnS after the slash indicates enabled (e.g., S−EN/S) and
a dash indicates disabled (e.g., S−EN/−) (figure 23−29). The SQTTR advisory is also displayed
anytime Mode S is enabled while the acquisition squitter is disabled. The SQTTR advisory is cleared
when either Mode S is disabled or the acquisition squitter is enabled.
Keep Mode S acquisition squitter enabled (boxed) when Mode S is
enabled. Disabling Mode S acquisition squitter with Mode S enabled does
not allow TCAS in nearby aircraft to acquire track.
d. Mode S Aircraft Call Sign. The Mode S aircraft (A/C) call sign is displayed on the CALL SN
option. If the A/C call sign has not been made available from the aircrew or mission planning, the
default A/C call sign is VV plus the BuNo (e.g.,VV166855). The A/C call sign may be changed by
selecting the CALL SN option which displays the A/C call sign UFCD sublevel and alphanumeric
keypad (figure 23−32). Valid A/C call signs are limited to no more than eight letters and numbers.
Leading or embedded spaces between characters in the A/C call sign are not accepted. Selecting the
CALL SN option after entering the new A/C call sign changes the call sign.
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Figure 23-31. Mode S Address Not Available on XPOND Sublevel
Figure 23-32. Mode S A/C Call Sign Sublevel
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23.8.2
IFF Interrogator. Interrogator operation is described in NTRP 3−22.2−EA−18G.
23.8.3
IFF BIT. IFF BIT status is displayed on the BIT page (figure 23−24). Initiated IFF BIT can
be performed by selecting the IFF option on the COMM sublevel of the BIT page.
23.8.4 IFF Programming (IFF PROG) Page. The IFF Programming (IFF PROG) page (figure 23-33)
allows the aircrew to program the MC to automatically change the IFF codes at specified times or on
a time interval, enable/disable IFF modes when the aircraft crosses a designated waypoint in a
specified direction, and update the Mode 4 transponder and interrogator on Zulu day transition. The
IFF PROG page is displayed by selecting the IFF/ROE PROG option on the SUPT page and then the
IFF PROG option. The IFF can also be programmed during mission planning. There is no MC backup
of this functionality. If either MC fails, this functionality is not usable.
IFF programs are always set as classified when edited on the IFF PROG page. When IFF programs
are downloaded as an initialization file, the classification is set the same as the file, whether classified
or unclassified.
23.8.4.1 Top Level IFF PROG Page. The IFF PROG page is divided into two sections. The top section
contains the time based (TIME) code information while the bottom section contains the position
(POS) group information. There are 15 distinct times and 2 positions which can be entered.
With the TIME option boxed, the MC automatically updates the selected IFF codes at the specified
time. For each specified time, transponder codes may be set for Modes 1, 2, and 3. The times are
referenced to aircraft Zulu time of day (ZTOD) in the format of hours:minutes. The first column of a
TIME data line contains the ZTOD at which the codes are updated followed by the Mode 1, 2, and 3
code columns.
With the POS option boxed, the MC automatically enables/disables the selected Modes 1, 2, 3, C,
and S transponder functions and can enable the Mode 4 transponder and interrogator functions at the
designated waypoint. Mode 4 transponder and interrogator functions can not be automatically
disabled. A POS group data line consists of the group number, the list of the modes to be affected in
this group, whether the modes are enabled/disabled, and the cardinal direction and waypoint
combination to specify the location where the modes are enabled/disabled.
With the AUTO M4 option boxed, Mode 4 for both the transponder and the interrogator switches
fromA toB when the aircraft clock passes through 00:00 Zulu time. If Mode 4 is alreadyB, this
feature has no effect.
The MC automatically disables the TIME and POS updates when Automatic Carrier Landing
(ACL) is selected. Once disabled, the desired automatic update state may be manually reselected. The
AUTO M4 feature is never automatically disabled.
When the EDIT option is selected, the IFF PROG EDIT sublevel is displayed.
23.8.4.2
IFF PROG EDIT Sublevel. The IFF PROG EDIT sublevel is used to select the time, mode
codes, position data and modes to be enabled/disabled and is displayed when the EDIT option on the
IFF PROG page is selected. The selection box indicates the currently selected data line. Selection
arrows are used to change the current selected data line. The CLEAR option clears the currently
selected data. The RETURN option returns to the IFF PROG page.
23.8.4.2.1 TIME Data. When editing a TIME data line, M1, M2, M3 and INTVL options are
displayed. When M1, M2, or M3 is selected, a UFCD format is displayed which allows aircrew to enter
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ORIGINAL
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Figure 23-33. IFF PROG EDIT Sublevel - POS Data
the Zulu time for the currently selected data line as well as input the exact code to be used in the
selected mode. The mode code is selected by entering a valid code and selecting the UFCD CODE
option. The selected mode code is displayed in the appropriate mode column on the IFF PROG page
and in the CODE option. If no mode code has been selected, the column on the IFF PROG page is
blank and the CODE option displays zeros. Time is selected by entering a valid four digit Zulu time and
selecting the UFCD TIME option. The selected time is displayed in the TIME column on the IFF
PROG page and in the TIME option. The selection arrows on the UFCD allow the aircrew to scroll
sequentially through the times entered on the IFF PROG page.
When a new time is entered, the TIME data lines are sorted in increasing time order based on
current aircraft time. The earliest later time is displayed first, followed by the remaining times in
sequential order. The selection box is moved automatically when the data line is edited. Times that are
earlier than the current aircraft time are assumed to be specified for the next Zulu day. When a TIME
data line is CLEAR’ed, the data lines are re−sorted, moving the data selection box and the newly
cleared data line to the bottom of the display.
A TIME data line is considered invalid if it contains valid code entries but does not contain a valid
time. Invalid data lines are displayed at the bottom of the display and are not used by the IFF.
When INTVL is selected, a UFCD format is displayed which allows aircrew to enter a start time and
single time interval for changing the IFF codes automatically. Start time is selected by entering a valid
four digit Zulu time and selecting the UFCD START TIME option. The selected start time is displayed
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in the START TIME option. The time interval is selected by entering a valid time interval (1 − 99
minutes) and selecting the UFCD LNGTH option. The selected time interval is displayed in the
LNGTH option.
When a start time and time interval are entered, all existing times are recomputed. The start time
is displayed in the first TIME data line with subsequent times equal to the previous time plus the time
interval. The codes currently specified for each data line are not changed.
23.8.4.2.2
POS Data When editing a POS group data line, M1, M2, M3, M4, MC, MS mode options,
ENBL/DSBL and cardinal direction options are displayed (figure 23−33). In order for group data line
to be valid, the following must occur: 1) At least one mode must be selected, 2) a direction must be
selected, 3) and a waypoint must be entered.
The mode options toggle the modes to be enabled or disabled into and out of the selected group. The
ENBL/DSBL option toggles between enabling and disabling the currently selected modes in the group.
The option affects all of the modes presently selected in the group. When the DSBL option is selected,
DSBL is displayed in the selected group and all modes listed are disabled when the aircraft reaches the
designated waypoint. When the ENBL option is selected, ENBL is displayed in the selected group and
all modes listed are enabled when the aircraft reaches the designated waypoint. Since Mode 4 can not
be automatically disabled, whenever the selected POS group data line displays DSBL, the M4 option
is Xd out. Also, if M4 is displayed in the selected POS group data line, the DSBL option is Xd out.
To designate the waypoint, one of the cardinal direction (N, S, E, W) options must be selected. The
selected cardinal direction is the direction the aircraft must pass the designated waypoint in order to
cause the selected modes to be enabled or disabled automatically. When a cardinal direction option is
selected, a UFCD format is displayed which allows aircrew to enter the designated waypoint. The
waypoint is selected by entering a valid waypoint number (0−99) and selecting the UFCD WYPT
option. The selected waypoint number is displayed in the WYPT option. The selected waypoint
number and cardinal direction are displayed in the group data line.
23.8.5 IFF Controls.
23.8.5.1 IDENT (ID) Button. The ID button is located on left side of the UFCD and is used to
manually squawk ident. Pressing the ID button enables the IFF system to transmit identification of
position for approximately 18 seconds.
23.8.5.2 Emission Control Button. The emission control button is located on the right side of the
UFCD and is labeled EMCON. Pressing the EMCON button changes the IFF, if ON, to a standby
mode so that it cannot transmit. At the same time, EMCON is displayed in the scratchpad for top level
displays or vertically in the left options for DDI displays on the UFCD. When EMCON is turned off
by pressing the button again, the IFF returns to the previous operating mode.
23.8.5.3
IFF Control Panel. The IFF control panel is located on the left hand console and contains
the MASTER switch, the MODE 4 switch, and the CRYPTO switch. The MODE 4 and CRYPTO
switches are used for Mode 4 on aircraft which have the KIV−6 installed.
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23.8.5.3.1
MASTER Switch. This switch has positions of NORM and EMERG.
NORM
IFF replies to interrogations with selected codes.
EMERG I FF replies to interrogations with emergency replies. The IFF transponder turns
on if off. This selection also zeroes the ARC−210 radios.
23.8.5.3.2
MODE 4 Switch. This switch has positions of DIS/AUD, DIS, and OFF.
DIS/AUD Enables IFF 4 caution andMODE 4 REPLY voice alert, M4 OK and IFFAI
advisories, and the Mode 4 audio tone.
DIS
Disables the Mode 4 audio tone. The IFF 4 caution andMODE 4 REPLY voice
alert, and M4 OK and IFFAI advisories are enabled.
OFF
Disables IFF 4 caution andMODE 4 REPLY voice alert, M4 OK and IFFAI
advisories, and the Mode 4 audio tone.
23.8.5.3.3
CRYPTO Switch. This switch has positions of HOLD, NORM, and ZERO. The switch is
spring−loaded to the NORM position.
HOLD
Mode 4 codes are retained after power has been turned off if HOLD has been
selected after the landing gear handle has been raised and lowered.
NORM
Mode 4 codes are available until power is turned off after the landing gear handle
has been raised and lowered.
ZERO
Mode 4 codes are zeroized (erased).
23.8.5.4 IFF Antenna Select Switch. The IFF antenna select switch is located on the ANT SEL
panel on the left console. When the switch is moved from BOTH to either UPPER or LOWER, the
selection remains in effect for only 60 seconds, at which time the IFF automatically switches to BOTH.
If the IFF switch remains in either UPPER or LOWER, a false indication of the antenna exists after
the 60 second time limit. With WonW, the time limit is not in effect and the IFF operates in accordance
with the position of the IFF antenna select switch.
UPPER
Selects upper antenna.
BOTH
Provides automatic antenna selection.
LOWER Selects lower antenna.
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23.8.6
IFF Related Cautions and Advisories. The following IFF related cautions and advisories are
described in the Warning/Caution/Advisory Displays in Part V:
• IFF 4 caution
• IFF OVRHT caution
• MODE 4 REPLY voice alert
• EBC advisory
• IFFAI advisory
• M4 OK advisory
• SQTTR advisory
23.9 COMMUNICATION-NAVIGATION-IDENTIFICATION INTERFACE
The radios, TCN, ILS, data link, radar beacon, and IFF interface with the aircrew through the
UFCD. The UFCD power and symbology are provided by the MPCD. As commands are entered into
the UFCD, the MPCD transmits those commands to the mission computer. The MC accepts those
commands and transmits them either directly to the CNI equipment if it is MUX compatible or to the
CSC if it is not. For non-MUX CNI equipment, the CSC converts the commands to analog or discrete
information and directly interfaces with the equipment. The CSC also converts standby attitude
signals used in the electronic attitude display indicator (EADI) and if the CSC fails the EADI is not
available.
23.10 COMMUNICATION-IDENTIFICATION DATA ENTRY
23.10.1
Data Entry. All data are entered using the keyboard followed by selecting the option
directly. Refer to figure 23-34 Communication-Identification Data Entry.
23.10.2 Data Entry Using the Shifted Keypad. The N-E-W-S option is provided on all UFCD data
entry displays. The shifted keypad provides the ability to enter a negative sign, a decimal point,
degrees, minutes, and seconds symbols, and North (N), East (E), West (W), and South (S) entries for
latitude and longitude entries.
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Figure 23-34. Communication-Identification Data Entry
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CHAPTER 24
Navigation Equipment
Navigation equipment consists of the following: Accurate Navigation System
(ANAV,
AN/ASN−181), which includes the Inertial Navigation System (INS) and Global Positioning System
(GPS), Instrument Carrier Landing System (ICLS, AN/ARA−63), and Data Link (D/L, RT/1379A/
ASW).
24.1 NAVIGATION CONTROLS AND INDICATORS
Navigation controls and indicators consist of the UFCD, MPCD, DDIs, HUD, INS mode switch,
course set switch, and COMM control panel. These controls and indicators are integrated in the
navigation system. MPCD and HUD symbology, and UFCD functions are described in Chapter 2.
24.1.1 UFCD Navigation Controls. The UFCD allows: ON/OFF operation of the ILS, TACAN, D/L,
and ADF; data entry for the TACAN and INS; and mode selection for the D/L.
24.1.2 Moving Map - Digital Map Set (DMS). The DMS is displayed in color on any AMPD, and the
front and rear MPCD to provide the pilot/WSO with a high resolution color map display for day/night
navigation.
24.1.2.1 MAP Option (HSI Option). The MAP option provides on/off control of the DMS map when
selected from an MPCD (MAP option is boxed when the map is ON). When MAP is selected from a
DDI, the HSI format source alternates between stroke (DDI symbol generator) and raster (DMS
mono-map) on all DDIs displaying the HSI format. The DMS map is commanded ON for the LDDI
and the MPCD when the raster HSI is selected on the DDI.
When map update is selected from the front cockpit MPCD, the TDC is assigned to the map slew
function. When map update is selected from the rear cockpit MPCD, the LDC is assigned to the map
slew function (if the LDDI is not communicating on the AVMUX, the RDC is assigned). When map
update is selected from the right or left DDI, the RDC or LDC, respectively, is assigned to the map slew
function. When map update is selected, MAP is automatically boxed. When map update is selected on
a DDI, all DDIs displaying the HSI format are driven by the DMS mono-map.
24.1.2.1.1 Moving Map Range Scales. For HSI in T UP (track up) or N UP (true north up), valid
range scale/map type combinations are as follows: 40/1:2M, 20/1:2M-ZOOM, 10/1:500K, 5/1:250K.
For HSI in DCTR (decenter), valid range scale/map type combinations are as follows: 80/1:2M,
40/1:2M-ZOOM, 20/1:500K, 10/1:250K.
Map compatible range scales are:
1. Centered (5, 10, 20, & 40 nm)
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2. Decentered (10, 20, 40, & 80 nm)
24.1.3 HSI Format. The MPCD displays TACAN, INS (also INS alignment data), D/L, and ILS
navigation symbology. The MPCD also allows selection of various TACAN, ILS, INS, and D/L
functions using the MPCD option pushbuttons. See figure 24-1.
The HSI format displayed on the MPCD is driven by the MPCD symbology overlaying the DMS
color map. The HSI format displayed on the DDI is driven by either a mono-map output from the DMS
or a DDI symbol generator. The DMS mono-map output contains the same information as the DMS
color output except for color, including cautions if they are provided with the color output. If the DMS
fails, the color map is unavailable; however, all stroke formats are available for display.
Navigation symbols and digital readouts are normally displayed on the MPCD. One of three TDC
assignment symbols can be displayed in the upper right corner of a TDC compatible display, to
indicate a TDC is assigned to the display in the front cockpit only, rear cockpit only, or both cockpits.
When a TDC is assigned to the map slew function, SLEW is displayed in the upper right corner of the
HSI display along with one of three arrows to indicate TDC assignment to the display in the front
cockpit only, rear cockpit only, or both cockpits.
24.1.3.1 HSI Option. This option returns the operator to the Top Level HSI format after the DMS
has been configured for operation. The HSI option coincides with the other HSI options found on
similar HSI formats to ensure consistency between formats. See figure 24-2.
24.1.3.2 MODE Option (HSI Format). The HSI display MODE option is located adjacent to the
center left push button of the DDI or MPCD. Selecting the MODE option enables T UP, N UP, DCTR,
MAP, and slew options to be displayed on the left side of the HSI display. At aircraft power-up/WonW,
the system initializes to map boxed (on), centered, T UP, and 40 nm scale.
24.1.3.2.1 MAP Operating Mode Option. This multifunction option combines the Chart (CHRT),
digital terrain elevation data (DTED), and controlled image base (CIB) map operating modes into a
single option. See figure 24-2.
24.1.3.3 MODE Backup. If aircraft magnetic heading or aircraft horizontal velocities become invalid,
the HSI format is limited to a centered north-up mode and the T UP and DCTR legends are removed
and selection inhibited from the HSI Mode sublevel. The N UP legend on the HSI Mode sublevel is
boxed under this condition. When aircraft magnetic heading and aircraft horizontal velocities become
valid, the HSI format is driven to the currently selected mode and the T UP, N UP and DCTR legends
are provided and processed on the HSI Mode sublevel.
NOTE
The currently selected HSI format mode option remains unchanged
when the aircraft magnetic heading or aircraft horizontal velocities
become invalid.
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Figure 24-1. Navigation Controls and Indicators (Sheet 1 of 2)
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Figure 24-1. Navigation Controls and Indicators (Sheet 2 of 2)
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Figure 24-2. TAMMAC Mode Selections
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24.1.3.3.1 MAP Modes/Data Products. Each of the map modes (CHRT, DTED, and CIB) provides
a different plan-view map/image. The actual presentation and availability of the different maps/
images are independent and mutually exclusive. Only one map mode can be selected at any one time.
The detailed images and associated area coverage for each mode are dependent on the map (theater)
data loaded in the DMS or installed on the mission card. Each plan-view map, regardless of mode,
presents an image that can support moving map capability and/or slew mode functions. When toggling
through the different modes, different map images are available providing the mode specific data is
loaded/available for that particular geographic position and scale. The map modes and their associated
data products are:
1. Chart (CHRT) mode provides a plan-view color map derived from Compressed ARC Digitized
Raster Graphics (CADRG). This chart product replaces the Compressed Aeronautical Chart (CAC)
map data currently used in the existing map (AN/ASQ-196).
2. Digital Terrain Elevation Data (DTED) mode provides a plan-view, panchromatic (gray scale),
terrain plot with slope shading.
3. Controlled Image Base (CIB) mode provides a plan-view panchromatic image derived from a
variety of mission planning, command, control, communications, and intelligence systems.
24.1.3.4 Map Data. The MDATA option is provided on the HSI/DATA sublevel format. MDATA is
boxed when selected and remains boxed until A/C, WYPT, TCN, HSI, or INS CK is selected. When
MDATA is selected, the DATA option is provided on the UFCD. When MDATA is selected on the
HSI, all DDI/MPCD/UFCD with the HSI format are driven by the DMS mono-map and the data
frames written in raster. The number of data frames is limited to 100.
24.1.3.4.1 Map Orientation Option. This option is a multifunction option that combines the Track
Up (T UP) and North Up (N UP) map orientation functions into a single option. Successive selections
of the orientation option toggles the map between these two orientations as they are mutually
exclusive. The T UP orientation is the default orientation. The DMS mono-map output contains the
same information as the DMS color output (except for color), including cautions if they are provided
with the color output. See figure 24-2.
24.1.3.5 SLEW Option (HSI Format). When map update is selected from the cockpit, the TDC is
assigned to the slew function. When map update is selected from the rear MPCD, the LDC is assigned
to the slew function (if the left DDI has malfunctioned the right designator control (RDC) is assigned).
When map update is selected from the right or left DDI the RDC or LDC, respectively, is assigned to
the map slew function. When map update is selected, MAP is automatically boxed and when selected
on a DDI, all DDIs and MPCDs displaying the HSI display are commanded to be driven by the DMS
monochromatic map.
When WYPT slew is selected from the cockpit, the TDC is assigned to the MAP Slew function for
waypoint update. When WYPT Slew is selected from the aft MPCD, the LDC is assigned to the MAP
slew function for waypoint update (if the LDDI is not communicating on the AVMUX, the RDC is
assigned). When WYPT Slew is selected from the right or left DDI, the RDC or LDC, respectively, is
assigned to the map slew function for waypoint update. When WYPT Slew is selected, MAP is
automatically boxed. When WYPT slew is selected on a DDI, all DDIs and UFCDs displaying the HSI
format are commanded to be driven by the DMS mono-map.
24.1.3.6 POS/XXX Option (HSI Format). This option is located along the top row of the HSI display
and when selected provides the POS/XXX sublevel display. This sublevel display allows the selection
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of AINS, INS, GPS, MIDS, ADC, or TCN as the position keeping source. When one of these options
is selected the top level HSI display is returned, with the appropriate selection denoted
(Ex.
POS/ADC). POS/INS is automatically selected during ground operations when INS data is valid.
Without MIDS, should the INS fail, the MC automatically begins position keeping with FCS air data
function (ADC) from the last valid INS position. MIDS is automatically selected as the aircraft
position keeping source if GPS and INS fail or become degraded. Because MIDS position keeping is
unreliable and inflight alignment is not possible when in POS/MIDS, air data position keeping
(POS/ADC) should be manually selected if POS/MIDS is displayed.
24.1.3.7 UPDT Option (HSI Format). The UPDT option is located along the top row of the HSI
display and when selected provides the UPDT sublevel display. This sublevel display allows the
selection of VEL (velocity), TCN, DSG (designation), AUTO, or MAP as the update source. Following
the selection of one of the update options, an ACPT/REJ (accept/reject) display is presented in which
the update can either be accepted or rejected. After selection of ACPT or REJ, the top level HSI
display is returned. There is no ACPT/REJ display presented when the AUTO option is selected.
Velocity update is described in the NTRP 3-22.2-EA-18G (EA-18G Classified Manual). If a previous
update has been accepted, a CANCEL option is also displayed on the UPDT sublevel to allow the
aircrew to cancel the last accepted update.
24.1.3.8 MK Option (HSI Format). This option is located along the top row of the HSI display. The
mark option is initialized to MK1 upon power up with WonW, regardless of the previous selection. A
maximum of nine mark points may be entered. If all mark points have been used and another mark
point is entered, MK1 is replaced with the new mark data.
If a waypoint/OAP is not designated and the MK option is selected, the lat/long of the current
overfly point is stored with the elevation set to zero. If a location is designated, the lat/long of the
designated location is stored. In this situation, the aircraft altitude minus the altitude above the
designated target is stored as the elevation.
24.1.3.9 DATA Option (HSI Format). The data option is located along the top row of the HSI display.
Selecting this option provides the DATA sublevel display. This display is used to enter waypoint/OAP
data, aircraft data, TACAN data, waypoint/OAP sequence data, radar and barometric altitude
warning, groundspeed data, and TOT data; and to select the INS check display. After selection of
either the WYPT, A/C, or TCN option, the UFC or SEQUFC option is used to initialize the UFCD for
data entry. The HSI option is used to return the HSI display to the top level format.
24.1.3.10 WYPT, OAP Option (HSI Format). The WYPT, OAP option is located along the right side
of the HSI. WYPT is displayed when steering is to a waypoint. OAP is displayed when steering is to
an OAP. If either the WYPT or OAP option is selected (boxed), direct great circle steering is provided
to that waypoint/OAP. TGT is displayed at this location when a target is designated.
24.1.3.10.1 Waypoint, OAP, Mark Point Selection. Along the right side of the HSI display just below
the WYPT/OAP/TGT options, there are two arrows pointing in opposite directions with a number in
between. This number indicates the current steer to waypoint/OAP/mark. The waypoint/OAP being
steered to can be incremented/decremented by selecting the appropriate arrow option, changing the
steer to number. After all of the waypoints/OAPs have cycled through (0 through 59), the mark points
can be selected for display. Marks are displayed with an M preceding the number.
24.1.3.11 WPDSG, O/S Option (HSI Format). This option is located along the right side of the HSI
display. Selecting this option designates a waypoint/OAP for weapon computations, sensor slaving,
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steering, or position updating. Selecting the WPDSG option designates the waypoint/OAP. After
designating a waypoint, the WPDSG option is removed and TGT replaces WYPT. After designating
an OAP, OAP remains boxed and O/S replaces WPDSG. When O/S is selected, the offset point is
designated, TGT replaces OAP, and O/S is removed.
24.1.3.12 SEQ # Option (HSI Format). The SEQ # option is located along the right side of the HSI
display. At power up with WonW, this option initializes to SEQ1 (unboxed). Successive actuations of
the option toggles through a display sequence in the following order: SEQ1 (boxed), SEQ2 (unboxed),
SEQ2 (boxed), SEQ3, (unboxed), SEQ3, (boxed), SEQL, (unboxed), SEQL, (boxed), and back to SEQ1
(unboxed). With the SEQ # option boxed, dashed lines are displayed connecting the waypoints of that
sequence. The dashed lines connecting the waypoints (SEQ # boxed) are displayed for all HSI range
scales and all HSI modes. The dashed lines are removed when magnetic heading is invalid, aircraft
position is invalid, or map slew is selected.
24.1.3.13 AUTO Option (HSI Format). The AUTO option is located along the bottom of the HSI
display. Selecting the AUTO option provides auto sequential steering to the first waypoint in the
selected sequence; boxing the AUTO and WYPT or OAP option (if not already boxed). Selecting the
AUTO option while boxed deselects auto sequential steering and unboxes the AUTO option. The
AUTO option is removed when:
1. The INS is in an alignment mode
2. INS heading failure occurs
3. Magnetic is invalid
4. Aircraft present position is invalid
5. Aircraft ground track is invalid
6. Selected sequence contains less than two waypoints
7. Aircraft is in auto or velocity update
8. FCS is coupled to the D/L
9. A ground point is designated
24.1.3.14 TIMEUFC Option (HSI Format). The TIMEUFC option is located along the bottom row of
the HSI display. The TIMEUFC option is removed from the HSI format during a GND or IFA GPS
alignment until the qual number is 6.2 or better, and is never displayed during a CV alignment.
Selecting this option boxes TIMEUFC and initializes the UFCD option display windows with the clock
options: DATE, ET counter, CD timer, ZTOD, and LTOD. Border highlights indicate that an option
is enabled for data entry. If an option is displayed on the HUD, the option has *HUD displayed below
it in addition to being border highlighted. The DATE, ET, ZTOD, LTOD, and CD options are mutually
exclusive; selecting one option deselects another option.
Data entry can be made for current date, current zulu or local time, or initial countdown time. No
data entry is available for the elapsed time option.
If DATE is highlighted, an M, D, and Y appear in the scratch pad and the month, day and year can
be entered on the keypad. If LTOD or ZTOD are highlighted two colons appear in the scratchpad and
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the hour, minutes and seconds can be entered on the keypad. If CD is highlighted one colon appears
in the scratchpad and minutes and seconds can be entered. Leading zeroes must be entered for the date
and time entries. Digits not entered are assumed to be zeroes, i.e., trailing zeroes need not be entered.
The time is displayed on the scratchpad as it is entered and displayed as ##:##:##. When the time
has been updated in the SDC it appears on the HUD and *HUD appears on the UFCD highlighted
option. The time display can be changed from local or zulu by selecting the appropriate option on the
UFCD and entering the appropriate time as before.
Countdown (CD) or elapsed (ET) time is selected and displayed in the same manner as local or zulu
time with the addition of START or STOP options. While CD START is displayed, the countdown
timer is counting down. The countdown timer defaults to 6 minutes on power up. If an invalid
countdown time is entered the timer sets to 59:59 and freezes. While ET START is displayed, the
elapsed timer is counting up to a maximum of 59:59.
24.1.3.15 MENU Option (HSI Format). The MENU pushbutton cycles through the airborne elec-
tronic attack (AEA), tactical (TAC), and support (SUPT) menus in the following order: AEA - TAC -
SUPT.
24.1.3.16 ACL Option (HSI Format). The ACL option is located on the left side of the HSI display.
When selected, ACL is boxed and the link 4 display appears on the left DDI.
24.1.3.17 SENSORS Option (HSI Format). Refer to NTRP 3-22.2-EA-18G (EA-18G Classified
Manual).
24.1.3.18 VEC Option (HSI Format). Refer to NTRP 3-22.2-EA-18G (EA-18G Classified Manual).
24.1.3.19 D/L Option (HSI Format). Refer to NTRP 3-22.2-EA-18G (EA-18G Classified Manual).
24.1.3.20 ILS Option (HSI Format). The ILS option is located on the left side of the HSI display.
When selected, ILS is boxed and ILS steering appears on the HUD.
24.1.3.21 TCN Option (HSI Format). The TCN option is located on the left side of the HSI display.
When selected, TCN is boxed and TACAN great circle steering appears on the HUD.
24.1.4 HSI Format on a DDI. The DDIs are capable of displaying HSI display and D/L information
by selecting the HSI or SA option on the applicable menu.
24.1.5 HUD - Navigation Information. The HUD displays basic flight symbology and steering
information for the TACAN, ILS, ACL, and INS.
24.1.6 CRS Select Switch. The CRS select switch is used to set a course to the selected waypoint,
OAP, or TACAN station. When the switch is actuated with waypoint/OAP or TACAN direct great
circle steering already selected, a course line appears through the waypoint/OAP or TACAN symbol on
the HSI display and steering information appears on the HUD. The course line rotates clockwise when
the switch is held to the right and counterclockwise when the switch is held to the left. When a course
is selected, a digital readout appears on the lower right corner of the HSI display.
24.1.7 ILS Control Panel. This panel contains two ILS controls: ILS UFC/MAN switch and the ILS
channel knob.
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24.1.7.1 ILS UFC/MAN Switch. When the switch is in the UFC position, ILS power and channel-
ization is controlled by the UFCD. With the switch in the MAN position, ILS power is enabled and ILS
channel changes are controlled by the ILS channel knob.
24.1.7.2 ILS CHANNEL Knob. This knob is used to select ILS channels when the ILS UFC/MAN
switch is set to MAN.
24.2 INERTIAL NAVIGATION SYSTEM (INS)/GLOBAL POSITIONING SYSTEM (GPS)
The INS and GPS are integrated into a single system called Accurate Navigation (ANAV). ANAV
data is provided to the MC for navigation, targeting, and weapon delivery. ANAV integrates the
Deflection of Vertical (DoV) database (also known as the Gravity Map database). The DoV database
is downloaded onto a mission card during mission planning. The continual use of DoV data along the
flight path assists in an improved navigation solution. If GPS data is unavailable, the additional DoV
data assists the ANAV system in maintaining unaided navigation performance.
24.2.1 Inertial Navigation System (INS). The INS is a self−contained, fully automatic dead
reckoning navigation system. The INS detects aircraft motion and provides acceleration, velocity,
present position, pitch, roll, and true heading.
Without good GPS satellite data, unaided INS (POS/INS) is the primary position keeping mode. In
POS/INS, the ANAV system provides navigation data by using the INS’s sensor data alone. In this
mode, the navigation data will drift in error over time. The error drift is minimized with the use of the
DOV data. POS/INS is selected by switching the INS knob to NAV after a GND or CV alignment.
If the INS shuts down abnormally (power loss), the INS knob must be set
to OFF for a minimum of 20 seconds.
NOTE
While it is acceptable to taxi with the INS off, the INS should be on,
whenever possible, to reduce accelerometer wear. It is preferable to
switch to the GYRO mode and wait for course level complete (NO
ATT disappears) before taxiing.
24.2.2 Global Positioning System (GPS). The GPS provides position, velocity, and time (PVT) data
that can be used to aid the INS or as an independent navigation sensor. The GPS receives modulated
signals through the GPS antenna from 32 high orbit satellites. Satellite data is used to determine GPS
position and velocity. GPS can be initialized with crypto keys, enabling encrypted P−code (precise)
navigation signals to be received.
With good GPS satellite data, aided INS (POS/AINS) is the primary position keeping mode. In
POS/AINS, the ANAV system provides navigation data by blending the INS sensor data with GPS
data. POS/AINS is selected by switching the INS knob to IFA after a GND or CV alignment. The
position keeping mode remains POS/AINS unless GPS satellites are lost, an INS or GPS failure occurs,
or the pilot manually chooses a different position keeping source.
GPS has four modes of operation which are displayed on the GPS page (see figure 24-3). In NAV
mode, the GPS tracks all available satellite constellations possible to provide the most accurate PVT
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solution. In Initialize (INIT) mode, the power supply is turned on, satellite tracking is not performed,
and almanac and waypoint data are loaded into the MC when initiated by the MC. In Not Ready (NOT
RDY) mode, the GPS is off or not communicating on the MUX. TEST mode is provided for ground
BIT testing.
Crypto key loading may be performed with a KYK−13 in any mode of operation.
It is important to set Zulu Time of Day (ZTOD) to aid in satellite acquisition. Local time, if desired,
should be set after takeoff. GPS is loaded with GPS precise times only once per cold start. Changing
the aircraft time or date with WonW re−initializes the GPS. An overall GPS Position Accuracy Figure
Of Merit (FOM) and Satellite (SAT) status is displayed on the GPS page to enhance the pilot’s
awareness of the overall GPS status.
24.2.3 INS Alignment Modes. INS alignment modes which can be selected using the INS knob are
CV (carrier alignment), GND (ground alignment), IFA (in−flight alignment), and GYRO (AHRS
attitude only). A Stored Heading alignment may also be selected to reduce CV/GND alignment time
if certain conditions are met.
During the first 30 seconds to 2 minutes of all alignments, NO ATT is displayed to the right of QUAL
on the HSI alignment display and the INS ATT caution is set. After the platform has leveled, NO ATT
is replaced with a quality (QUAL) number, the INS ATT caution is cleared, and the INS begins to
determine true north. The QUAL number is an estimate of present position accuracy in nm/hr CEP.
Also during the INS alignment, the GPS is initialized with WYPT 0, ZTOD, DATE, almanac and GPS
waypoints if the A/C is WonW. After initialization, the GPS is commanded to search and acquire GPS
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Figure 24-3. GPS Page
satellites. OK is displayed next to the QUAL number when a satisfactory alignment is achieved and the
INS can be switched to IFA (POS/AINS) or NAV (POS/INS). When IFA (POS/AINS) or NAV
(POS/INS) is selected, the alignment data is removed from the HSI. Also during the alignment, TIME
increments. TIME will stop incrementing and flash when the INS suspends alignment due to
premature parking brake release (GND or CV), GPS data unavailable (IFA), ship INS (SINS) data
unavailable (CV), motion detected (GND), POS ERROR caution set, or waiting for carrier data entry
or carrier heading and/or carrier velocity changes during CV Manual alignment.
24.2.3.1 CV Alignment Modes. Selecting CV provides CV alignment options of RF (radio fre-
quency), CBL (cable), and MAN (manual). With the RF or CBL alignment option selected, the aircraft
is data linked to the ship’s INS (SINS). The MAN option has no data link capability and alignment
data must be entered manually. Before selecting CV, WYPT 0, ZTOD and DATE should be entered
and the parking brake set. When CV is selected, the alignment data is displayed on the HSI page
(figure 24−4) and the UFCD displays the OPER option and the operate (alignment) frequency in the
UFCD scratchpad.
The parking brake must remain set until a satisfactory alignment is achieved (OK displayed). If the
parking brake is released before OK is displayed and the QUAL number is greater than 5, the INS
switches to GYRO mode (AHRS attitude only). If the parking brake is released with the QUAL number
less than 5, the INS switches to POS/INS mode with limited performance. A complete re−initialization
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is required to achieve a satisfactory alignment (OK displayed). This can be accomplished with either
an IFA or CV alignment.
If the INS knob is turned OFF in less than 40 seconds after selecting CV,
the system must be left off for a minimum of 20 seconds.
24.2.3.1.1 CV RF/CBL (SINS) Alignment. With the CV RF/CBL (SINS) alignment, the INS
automatically compensates for the difference between the aircraft deck position and SINS position. To
perform this alignment, the parking brake must be set and the INS knob switched to CV. The INS,
GPS and data link are turned on and alignment data is displayed on the HSI. For an RF alignment,
information is received by radio frequency and CV RF is displayed. The alignment frequency is
displayed on the UFCD scratchpad for 30 seconds after selecting CV and may be changed using the
UFCD keypad. When a cable is connected to the aircraft, information is received on the cable and CV
CBL is displayed. RF/CBL and the TIME flashes until SINS data becomes valid. If the SINS data
becomes invalid during the alignment, the TIME flashes and the INS suspends the alignment until the
SINS data becomes available again. If the SINS data remains invalid for 30 seconds, the INS
automatically switches to CV Manual alignment using the last valid SINS data the INS received. If the
SINS data becomes valid during CV Manual alignment, the INS automatically switches back to CV
SINS alignment. CV SINS alignment time is normally less than 10 minutes.
While the platform is being leveled, a total of 10 waypoints can be received. When 10 waypoints have
been received, WYPTS is displayed below the TIME. If all waypoint data is not received, NO WYPTS
is displayed below the TIME. Reception of waypoint data is not required for the alignment to proceed.
24.2.3.1.2 CV Manual Alignment. A CV Manual alignment can be selected if the data link signal is
not available or not desired, or occurs automatically if CV SINS data is invalid greater than 30 seconds.
CV Manual alignment requires entering CV data on the UFCD. To perform this alignment, the parking
brake must be set and the INS knob switched to CV. The INS, GPS and data link are turned on and
the alignment data is displayed on the HSI. Selecting the MAN option enables the CV Manual
alignment display on the HSI and UFCD (figure 24−4). MAN is boxed when selected and the STD
HDG option is removed. Carrier lat/long data (POSN), heading (CV HDG), and speed (CV SPD) are
entered through the UFCD. The INS uses this data to update present position during the alignment.
If the carrier heading changes more than 10° or carrier speed changes more than 1 knot, the aircrew
must re−enter carrier data to reinitialize the alignment. In the case where the CV SINS was invalid
greater than 30 seconds, the INS will use the last valid SINS data to complete a CV Manual alignment.
If this occurs, no carrier data entry is required. CV Manual alignment time is approximately 15
minutes.
CV MANUAL ALIGNMENT
1. Parking brake − SET
The parking brake must remain set until a satisfactory alignment is achieved (OK displayed). If the
parking brake is released before OK is displayed, the alignment must be reinitiated.
2. ATT switch − AUTO or INS
3. Enter WYPT 0, ZTOD, and DATE
4. INS knob − CV
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Figure 24-4. INS CV Alignment
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A1-E18GA-NFM-000
5. HSI MAN option − SELECT
On the UFCD
6. Enter Latitude (leading zeroes must be entered)
7. POSN option − SELECT
8. Enter Longitude (leading zeroes must be entered)
9. POSN option − SELECT
10. Enter Carrier Heading (0 to 360)
11. CHDG option − SELECT
12. Enter Carrier Speed (0 to 63)
13. CVEL option − SELECT
After alignment is complete
14. INS knob − IFA (POS/AINS). If GPS not available then INS knob − NAV (POS/INS)
24.2.3.2 Ground (GND) Alignment Mode. To perform an INS ground alignment, the parking brake
must be set, WYPT 0, ZTOD and DATE entered, and the INS knob switched to GND. The INS and
GPS are turned on and ground alignment data is displayed on the HSI (figure 24−5). If the aircraft is
taxied during the alignment, the INS will suspend the alignment as indicated by the TIME flashing.
The aircraft may be taxied without restarting the alignment if the QUAL number is less than 5.
NOTE
The most accurate alignment of the INS is achieved by changing
aircraft heading at least 70° (180° optimum) after OK is displayed
next to the QUAL number and allowing the alignment to continue. An
alignment with TIME greater than 12 minutes has little to no benefit.
The MC automatically transfers WYPT 0 to the INS to be used as aircraft present position.
This information appears on the ground alignment display. WYPT 0 position can be updated prior to
selecting GND but if an error is noticed after the alignment has begun, aircraft present position must
be corrected because WYPT 0 is transferred to the INS only once. If aircraft present position is found
to be incorrect, it must be corrected or the INS will align improperly. Refer to A/C Programming, this
chapter, to enter new aircraft position data. The INS will not restart if the position is corrected with
TIME less than 30 seconds and if the update is no more than 0.4 nm from the original position. After
30 seconds, any position update will re−start the alignment.
The parking brake may be released with TIME greater than 30 seconds; however, if the INS detects
A/C motion with the parking brake released, the INS suspends the alignment until no motion is
detected for 20 seconds, at which point the alignment will continue if the QUAL number is less than
or equal to 5 or restart if the QUAL number is greater than 5.
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Figure 24-5. INS Ground Alignment
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A1-E18GA-NFM-000
If the aircraft takes off in GND mode before the QUAL number is greater than 5, the INS switches
to GYRO mode (AHRS attitude only). If the aircraft takes off in GND mode when the QUAL number
is less than or equal to 5, the INS switches to POS/INS mode with limited performance. To complete
a partial alignment after take−off, switch the INS knob to IFA and complete the alignment.
24.2.3.3 Stored Heading (STD HDG) Alignment. A Stored Heading alignment may be performed to
reduce INS alignment time if the INS has been shut down (INS knob OFF) after a good alignment, the
parking brake set at shutdown, and no other INS mode has been selected prior to selecting OFF. The
STD HDG option is provided on the CV/GRD alignment display if available. The STD HDG option
is removed when a GRD or CV SINS alignment has progressed to the point where selecting the STD
HDG option would not reduce alignment time; or, during a CV alignment, when the MAN option is
selected.
Selecting the STD HDG option results in an alignment based on the stored heading when the INS
was shut down. To perform a Stored Heading alignment, the parking brake must be set, WYPT 0,
ZTOD, and DATE entered, the INS knob switched to CV or GND, and the STD HDG option selected
(figure 24−5). When Stored Heading alignment is entered, the INS will check if the current heading is
the same as the previous alignment’s heading. If so, the HSI alignment data will display OK next to the
QUAL number within 30 seconds for a GND alignment and within 60 seconds for a CV SINS
alignment. After OK displayed, the INS knob can be switched to IFA (POS/AINS) or NAV
(POS/INS). If the aircrew allows the alignment to continue, the QUAL number may decrease as the
alignment continues normally.
If the aircrew believes that the A/C has been moved or its shutdown heading has changed either on
the ground or with respect to the carrier deck, a Stored Heading alignment should not be attempted
even if the STD HDG option is available. If the A/C has moved, poor performance may result if a
Stored Heading alignment is achieved.
24.2.3.4 InFlight (IFA) Alignment. An IFA may be used with WonW or airborne to perform a
complete alignment or complete a partial CV/GND alignment. An IFA requires GPS satellites signal
availability. IFA should be considered a backup alignment mode to GND and CV alignments.
An IFA may be attempted after an INS failure. Select STBY with the ATT switch to verify the
accuracy of HUD attitude data by cross checking the standby instruments. If POS/MIDS is the current
position keeping mode, select POS/ADC.
NOTE
If POS/MIDS is the current position keeping mode, select POS/ADC
before commencing IFA procedures.
Select NAV master mode and radar altitude to HUD. If the IFA is being performed with WonW,
enter WYPT 0, ZTOD, and DATE. Select OFF for 20 seconds before selecting IFA. When IFA is
selected, the INS and GPS are powered and alignment data is displayed on the HSI (figure 24−6).
While waiting for the GPS to acquire good GPS satellite data, IFA RDR is displayed on the HSI and
the TIME flashes; however, the INS suspends the alignment. Once good GPS satellite data is acquired,
IFA GPS is displayed and the alignment begins. During the first 10 to 15 seconds of the alignment
while the INS platform is being leveled, NO ATT is displayed to the right of QUAL. Maintain straight
and level, unaccelerated flight to level the INS and clear the NO ATT indication. NO ATT is replaced
with the QUAL number. Select AUTO or INS with the ATT switch and the INS ATT caution will
clear. Selecting INS or AUTO replaces standby attitude reference indicator data on the HUD with INS
attitude data (the waterline symbol is replaced with a slowly flashing velocity vector which symbolizes
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a degraded vertical velocity). When the GPS horizontal position becomes valid, the POS/ADC caution
clears. The velocity vector continues to slowly flash until vertical velocity becomes valid (QUAL
number approximately 5.0). Perform one gentle 90° S−turn (less than 20° AOB and ±10° pitch) to
facilitate the alignment. Then maintain straight and level flight as much as practical. IFA takes
approximately 10 minutes. When a satisfactory alignment is achieved (OK displayed), alignment data
is removed from the HSI the position keeping mode automatically transitions to the POS/AINS.
If IFA is selected prior to the acquisition of good GPS satellite data, IFA RDR is displayed on the
HSI and the TIME flashes; however, the INS suspends the alignment. If this occurs on the ground
prior to achieving a satisfactory alignment (OK not displayed), the appropriate ground alignment
mode (i.e., GRD or CV) should be selected to allow proper alignment of the INS or wait until good GPS
satellite data is acquired. If this occurs after achieving a satisfactory alignment (OK displayed), NAV
should be selected until good GPS satellite data is acquired (SAT STATUS = GOOD on the GPS page)
and then IFA selected for POS/AINS position keeping. Although RDR IFA may flash if an IFA is
attempted without GPS satellites, APG-79 Radar does not have Position Velocity Update mode
required to support a Radar IFA.
During an IFA, if good GPS satellite data is acquired and then lost for 65 seconds or more, the INS
suspends the alignment (IFA RDR is displayed), and waits until good GPS satellite data is reacquired.
An IFA may be used to complete a partial CV/GND alignment. At takeoff with a partial alignment,
the INS platform should already be leveled (no INS ATT caution). Select IFA and the position keeping
mode automatically transitions to POS/AINS once a satisfactory alignment has been achieved (OK
displayed). Completing a partial alignment with an IFA may occur very quickly.
Present position can be provided but is not required for the alignment by performing a position
update using the UPDT option or by entering the aircraft data on the UFCD using the DATA option.
Another very good technique is to select TACAN position keeping if a stationary TACAN is available.
Velocity updates cannot be performed during an IFA. The VEL update option is displayed but returns
to the IFA alignment display when selected.
InFlight Alignment
1. ATT switch − STBY
2. If POS/MIDS is the current position keeping mode, select POS/ADC.
3. NAV master mode − SELECT
4. ALT switch − RDR
5. INS knob − OFF (20 seconds minimum)
6. If WonW, enter WYPT 0, ZTOD, and DATE
7. INS knob − IFA
8. Maintain straight and level, unaccelerated flight until NO ATT is cleared from the HSI.
9. ATT switch − AUTO or INS (VV position is degraded if flashing slowly)
10. Perform one gentle,
90° S−turn
(less than
20° AOB and ±10° pitch), then maintain
straight−and−level as much as practical.
Within approximately 10 minutes
11. HSI page − Verify transition to POS/AINS
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