BendixKing KT 86 Mode S Transponder Instruction Manual
- June 6, 2024
- BendixKing
Table of Contents
- BendixKing KT 86 Mode S Transponder
- Front Panel
- Display
- Mode Selector Knob
- Push Buttons
- Squawk code entry
- Flight ID entry
- Altitude Monitor
- ADS-B Monitor
- Warning Messages
- Fault Annunciation
- Low-Temperature Operation
- Warnings
- Faults
- Read User Manual Online (PDF format)
- Download This Manual (PDF format)
BendixKing KT 86 Mode S Transponder
Front Panel
Display
The display shows the operating mode of the transponder, the reported pressure
altitude, and the current squawk code and Flight ID. The reply indicator is
active when the transponder replies to interrogations.
The pressure altitude is displayed as a Flight Level, 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 ATC radar.
Mode Selector Knob
The knob on the right hand side controls the power to the transponder and the operating mode.
- OFF: Power is removed from the transponder.
- SBY: The transponder is on, but will not reply to any 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 configured with an automatic air/ground system will automatically switch the transponder to Ground Mode on landing or whilst taxiing. GND will be indicated on the display.
Push Buttons
- IDENT: Press the IDENT button when ATC instructs you to “Ident” or “Squawk Ident”. This activates the SPI pulse in the transponder replies for 18 seconds. IDENT will appear in the display.
- VFR: Pressing the VFR button sets the transponder to the pre-programmed conspicuity code. Pressing the button again restores the previous squawk code. Pressing the VFR button whilst in Flight ID edit changes the Flight ID to the pre-programmed ID set up during the configuration of the transponder.
- FUNC: Pressing the FUNC button provides access to the flight timer, stopwatch, Flight ID editing, ADS-B monitor (depending on installation) and altitude monitor function.
- ENT: The ENT button confirms selection or presented options.
Squawk code entry
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: VFR code in the USA
- 7000: VFR code commonly used in Europe
- 7500: Hijack code
- 7600: Loss of communications
- 7700: Emergency code
Flight Timer
The Flight Timer records the time for which the transponder has been powered
on and operating in flight mode – either ON or ALT. Press the FUNC button to
display the Flight Timer.
Stopwatch
The stopwatch can be used as a convenient timer. Press the FUNC button to
display the stopwatch. Pressing ENT will reset and start the timer. Pressing
ENT again will stop the timer
Flight ID entry
Select the Flight ID screen using the FUNC button and then edit the Flight ID
using the numeric buttons. The lower portion of the display shows the alpha
numeric characters selectable 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 an “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 30 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, entering the “space” character will end it.
Altitude Monitor
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. Press the FUNC button to display
the altitude monitor enable screen. 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.
ADS-B Monitor
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 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.
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 organisation. 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.
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.
Configuration Mode
The system is configured when it is first installed by your avionics supplier.
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 with your avionics installer
before changing the configuration.
To enter configuration mode, hold down the FUNC button whilst 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
VFR button will move back to the last menu item. Pressing FUNC advances to the
next configuration item.
When the configuration is complete, switch the transponder off. When it is
switched back on the transponder will use the new configuration.
Low-Temperature Operation
The KT 86 and KT 86G are certified to operate correctly down to -25C, but at low temperatures the display may be impaired. On a cold day you may need to wait for the cockpit to warm up to ensure normal operation. A heating element is built into the front panel to automatically raise the temperature around the display under extreme cold conditions and reduce the time before the display is fully functional. This heater may take several minutes to become effective after initial power on.
Warnings
The following warnings may appear on the transponder display.
Message | Issue Description | Action to resolve |
---|---|---|
Antenna Fault | The transponder has detected that there is a fault in the |
antenna cabling or
antenna connection.
| Check transmitter cabling and connection to antenna.
Output Power Low| The transponder has detected that it transmitted at a lower
power level than expected. This may be caused by;
a) poor antenna connection in the transponder tray,
b) poor antenna cable connections or
c) a transponder hardware fault.
| Check connection at the transponder tray and transmitter cabling.
No ADSB Position| Valid ADSB position data has not been received for either;
a) 180 seconds from system startup or
b) 2 seconds once a GPS position data has been received by the transponder.
| Check cabling to GPS and GPS antenna position and connection.
Faults
The Transponder will not continue to operate when a fault condition is present and one of the following messages appears on the display.
Message | Action to resolve |
---|---|
FPGA Fault | Call Service center |
ROM checksum failed XXXX | Call Service center |
Receiver fault or no signal | Call Service center |
Transmitter failed | Call Service center |
Squitter failure | Call Service center |
I2C Write Data | Call Service center |
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