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Congratulations on choosing the KT 74 ADS-B Out Enabled Mode S
Transponder. At BendixKing we are committed to providing you with
the most reliable and advanced technology that will meet your
transponder needs. The KT 74 meets the Global Mandates for
Automatic Dependent Surveillance – Broadcast (ADS-B) out* and
more.
*When coupled with approved GPS source, STC and install kit
required.
Additional KT 74 Benefits:
• Push button operation
• New sleek design
• Most affordable Mode S Transponder with ADS-B Out
• Low power consumption
• Stopwatch and timer
• Altitude monitor
• Built-in altitude repeater instead of a second altitude encoder
• TIS-A Traffic output
The feature-rich KT 74 brings the value, simplicity, reliability and
affordability into the cockpit that BendixKing has been trusted for
since 1959.
The KT 74 is certified to ETSO C112d Class 1 Mode S level 2els,
ETSO C166b Class B1S, FAA TSO C112D and TSO C166B.
•Active Mode: the Active Mode indicator shows the mode
that is currently set on the Mode Knob. See section 1.4.
•Pressure Altitude: The reported pressure altitude is
displayed as a Flight Level (FL), which is the pressure
altitude in hundreds of feet. When non-standard atmospheric
conditions apply, this may not match the altimeter indicated
altitude, but will be correctly displayed by the Air Traffic
Control (ATC) radar.
•Squawk Code: The current squawk code selected by the
Numeric Buttons. See Squawk Code Entry in section 1.5
•Flight ID: The aircraft call sign entered on your flight plan.
See Flight ID Entry in section 1.6
•IDENT Indicator: The IDENT Indicator shows when IDENT
mode is active. See section 1.5.
•Reply Indicator: The Reply Indicator is active when the
transponder replies to interrogations.
•Deviation Pointer: When altitude monitoring is in use, a
small deviation pointer appears adjacent to the altitude
display on the transponder. See Altitude Monitor in section
1.6.
• Warning message: See section 1.7
• Fault Annunciation: See section 1.8.
Light Sensor
If connected to a lighting bus, the KT 74 will adjust the brightness of
the front panel lighting based upon the lighting bus input. If no
lighting bus input is detected, the KT 74 will automatically control the
front panel lighting based on the ambient light sensor. The dim point
for the Liquid Crystal Display (LCD) backlight illumination can be
adjusted by using the configuration mode as described in section
The mode knob to the right of the display controls the power to the
transponder and the operating mode. The mode knob has the
selections that follow:
OFF
Power is removed from the transponder.
SBY
interrogations.
ON
The transponder will respond to all interrogations, but
altitude reporting is suppressed.
ALT
The transponder will respond to all interrogations.
When airborne, the transponder should always be set to ALT unless
otherwise directed by Air Traffic Control. Aircraft installations that
include a gear squat switch or other method of air/ground
determination will automatically select surface reporting mode on
landing or when taxiing. The mode indicator will read GND.
Press any of the numeric buttons (0 through 7) to change the
squawk code. A new squawk code is set when the fourth digit is
entered. If the code entry is not completed within 7 seconds, the
changes are ignored and the previous code restored.
Some standard squawk codes are listed below:
• 1200
• 7000
• 7500
• 7600
• 7700
VFR code in the USA
VFR code commonly used in Europe
Hijack code
Loss of communications
Emergency code
1.6 FUNCTIONS
Figure 1-5: Functions
The different KT 74 functions are accessed using the FUNC button.
The functions displayed vary depending on whether the aircraft is
airborne or is on the ground (squat switch or other method of
air/ground determination installed) and has the GPS input enabled or
not as shown in the following tables.
Press the FUNC button twice to display the stopwatch. The
stopwatch can be used as a convenient timer. Pressing ENT will
reset and start the timer. Pressing ENT again will stop the timer.
Flight ID Entry
Press the FUNC button three times to display the Flight ID entry
screen. The edit the Flight ID using the numeric buttons. The lower
portion of the display shows the alpha numeric characters selected
through multiple presses of the numeric buttons. When the correct
character is shown in the flight ID section of the screen, press the
ENT button to accept and advance to the next digit. The flight ID is
terminated with a “space” character located on the 7 button. When
ENT is pressed on the end space, the new Flight ID will replace the
previous value. If a button is not pressed for 7 seconds, the changes
are ignored and the previous code restored.
The Flight ID should correspond to the aircraft call sign entered on
your flight plan. If no flight plan is active, the aircraft registration
should be used as your Flight ID. Use only letters and digits. If the
Flight ID is less than 8 characters long, enter the “space” character
(7 button) to end it.
Altitude Monitor
Press the FUNC button four times to display the Altitude Monitor
enable screen. The Altitude Monitor activates an audio annunciator
or annunciator light (depending on installation) when the aircraft
pressure altitude differs from the selected altitude by more than 200
feet. Pressing ENT toggles the altitude monitor at the current
altitude.
When altitude monitoring is in use, a small deviation pointer appears
adjacent to the altitude display on the transponder.
Press the FUNC button five times to display the Altitude Monitor
screen The ADS-B Monitor is only available on installations that
include an ADS-B position source. The ADS-B Monitor provides a
display of the position information that is being transmitted in ADS-B
position reports. This can provide confirmation that the correct
information is being transmitted, particularly where the Global
Positioning System (GPS) source is remote from the transponder.
In the event that valid position information is NOT available from the
GPS, the latitude and longitude display will be replaced by dashes. If
no valid latitude and longitude is shown, then ADS-B position
information is NOT being transmitted.
Loss of ADS-B position information will also result in a WARNING
message being displayed.
1.7 WARNING MESSAGES
If the transponder detects a problem, the screen will indicate
WARNING and a brief statement of the problem. Depending on the
nature of the problem, your transponder may not be replying to
interrogations. Note the message on the screen and pass that
information to your avionics maintenance organization. The
WARNING message should clear when the event has cleared. Press
ENT to clear the message at any time; if the fault is still present the
message may reappear.
1.8 FAULT ANNUNCIATION
If the transponder detects an internal failure, the screen will indicate
FAULT and a brief statement of the problem. No replies will be made
to interrogations when a fault is detected.
Some FAULT indications can be recovered by switching the
transponder off and back on again, although in all cases a FAULT
code implies that there is a fault with the transponder or the
installation. Note the FAULT message at the bottom of the screen
and pass that information to your avionics maintenance organization.
The system is configured when it is first installed by your avionics
installer. Configuration items include the Mode S aircraft address,
the interface to the other aircraft systems, the aircraft category, and
the pre-programmed values for VFR squawk code. To view or
change these settings you must use Configuration Mode.
Do not use Configuration Mode in flight. Check
configuration.
To enter configuration mode, hold down the FUNC button while
switching on the transponder. Configuration items can be changed
using the numeric buttons (6 for down, 7 for up) and the ENT button
to accept the selection. Pressing the 2 button will move back to the
last menu item. Pressing FUNC advances to the next configuration
item.
When configuration is complete; switch the transponder off. When it
is switched back on the transponder will use the new configuration.
1.10 LOW TEMPERATURE OPERATION
The KT 74 is certified to operate down to -25°C; however under cold
operating conditions, the display update rate may be slowed but
functional. The KT 74 incorporates an integral heating element in the
front panel to automatically raise the temperature around the display.
During cold operating conditions, a warm up period of 5 minutes
minimum is suggested.
Acronyms and abbreviations used in this manual are defined as
follows:
TERMS DEFINITION
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