BendixKing KT 74 User Manual

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KT 74 Pilot's Guide
KT 74 ADS-B
OUT ENABLED
MODE S
TRANSPONDER
PILOT'S GUIDE
D201308000036 Title Rev 0 Dec 2013 Page T-1
© Honeywell International Inc. Do not copy without express permission of Honeywell
KT 74 Pilot's Guide
Revision History and Instructions
Manual KT 74 ADS-B Out Enabled Mode S Transponder Pilot's
Guide
Revision 0 Summary This is a new release.
Record of Revisions
REVISION
NUMBER
U0 DEC, 2013
REVISION
DATE
Record of Revisions D201308000036
Page RR 1 Rev
© Honeywell International Inc. Do not copy without express permission of Honeywell
0 Dec 2013
KT 74 Pilot's Guide
Table of Contents
Section Page
1. Operation ................................................................................. 1-1
1.1 Introduction ...................................................................... 1-1
1.2 Front Panel Controls and Functions ................................ 1-2
1.3 Display ............................................................................. 1-2
Light Sensor .................................................................... 1-3
1.4 Mode Knob ...................................................................... 1-4
1.5 Push Buttons ................................................................... 1-5
Squawk Code Entry ......................................................... 1-6
1.6 Functions ......................................................................... 1-6
Flight Timer ...................................................................... 1-7
Stopwatch ........................................................................ 1-8
Flight ID Entry .................................................................. 1-8
Altitude Monitor ................................................................ 1-8
ADS-B Monitor ................................................................. 1-9
1.7 Warning Messages .......................................................... 1-9
1.8 Fault Annunciation ........................................................... 1-9
1.9 Configuration Mode ....................................................... 1-10
1.10 Low Temperature Operation ......................................... 1-10
2. Appendix ................................................................................. 2-1
2.1 Acronyms and Abbreviations ........................................... 2-1
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KT 74 Pilot's Guide
List of Illustrations
Figure Page
Figure 1-1: Front Panel Controls and Functions ............................. 1-2
Figure 1-2: Display .......................................................................... 1-2
Figure 1-3: Mode Knob ................................................................... 1-4
Figure 1-4: Push Buttons ................................................................ 1-5
Figure 1-5: Functions ...................................................................... 1-6
List of Tables
Table 1-1: FUNC Sequence with Squat Switch Input Enabled ....... 1-7
Table 1-2: FUNC Sequence without Squat Switch Input Enabled .. 1-7
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KT 74 Pilot's Guide
1. OPERATION
1.1 INTRODUCTION
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.
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KT 74 Pilot's Guide
1.2 FRONT PANEL CONTROLS AND FUNCTIONS
Figure 1-1: Front Panel Controls and Functions
The KT 74 has the following front panel controls and functions:
Display: See section 1.3.
Mode Knob: See section 1.4.
Push Buttons: See section 1.5.
Functions: See section 1.6.
1.3 DISPLAY
Figure 1-2: Display
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KT 74 Pilot's Guide
The display shows the following indications:
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
1.9 of this guide.
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KT 74 Pilot's Guide
The transponder is on, but will not reply to any
1.4 MODE KNOB
Figure 1-3: Mode Knob
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.
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KT 74 Pilot's Guide
button when ATC instructs you to
appear in the display.
essing the button again
during configuration of the transponder.
B monitor
See section 1.6 below.
ENT
The ENT button confirms selection or presented options.
code and as part of the data entry selections.
1.5 PUSH BUTTONS
Figure 1-4: Push Buttons
IDENT
Press the IDENT
“Ident” or “Squawk Ident”. This activates the SPI pulse in
the transponder replies for 18 seconds. IDENT will
VFR Pressing the VFR button sets the transponder to the pre-
programmed VFR code. Pr restores the previous squawk code.
Pressing the VFR button while in Flight ID editing mode
changes the Flight ID to the pre-programmed ID set up
FUNC Pressing the FUNC button provides access to the flight
timer, stopwatch, Flight ID entry, ADS­(depending on installation) and altitude monitor function.
0-7
The numeric buttons are used to change the squawk
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KT 74 Pilot's Guide
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
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.
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KT 74 Pilot's Guide
Table 1-1: FUNC Sequence with Squat Switch Input Enabled
Airborne/
Ground
GPS
INPUT
SEQUENCE
Airborne Yes PWR ON (Squawk) -> Flight Time -> Timer
-> ADS POS -> Edit Flight ID -> Alt Monitor
-> Squawk
Airborne No PWR ON (Squawk) -> Flight Time -> Timer
-> Edit Flight ID -> Alt Monitor -> Squawk
On Ground
On Ground
Yes PWR ON (Squawk) -> Flight Time -> Timer
-> ADS POS -> Edit Flight ID -> Squawk
No PWR ON (Squawk) -> Flight Time -> Timer
-> Edit Flight ID -> Squawk
Table 1-2: FUNC Sequence without Squat Switch Input Enabled
GPS
SEQUENCE
INPUT
Yes PWR ON (Squawk) -> Flight Time -> Timer ->
ADS POS -> Edit Flight ID -> Alt Monitor -> Squawk
No PWR ON (Squawk) -> Flight Time -> Timer ->
Edit Flight ID -> Alt Monitor -> Squawk
Each function is described in more detail below:
Flight Timer
Press the FUNC button once to display the 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.
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KT 74 Pilot's Guide
Stopwatch
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.
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KT 74 Pilot's Guide
ADS-B Monitor
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.
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KT 74 Pilot's Guide
with your avionics installer before changing the
1.9 CONFIGURATION MODE
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.
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KT 74 Pilot's Guide
ADS-B
Automatic Dependent SurveillanceBroadcast
ALT
Altitude
ATC
Air Traffic Control
ENT
Enter
FAA
Federal Aviation Administration
FL
Flight Level
FUNC
Function
GPS
Global Positioning System
ID
Identification
IDENT
Identify
LCD
Liquid Crystal Display
SBY
Standby
VFR
Visual Flight Rules
2. APPENDIX
2.1 ACRONYMS AND ABBREVIATIONS
Acronyms and abbreviations used in this manual are defined as follows:
TERMS DEFINITION
Copyrighted information in this manual is subject to change without notice. Bendix/King reserves the right to improve or change the products or contents of this manual, without notification of any person or agency. The contents of this pilot's guide may be downloaded, stored and reprinted for personal use provided that this copyright information is included. Commercial use is strictly prohibited. For further information contact
techsupport@bendixking.com.
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© Honeywell International Inc. Do not copy without express permission of Honeywell
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