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BENDIX/KING

KT 73

Rev 0, October/2002

10563I00.JA

Page 3-17

NOTE:

The KT 73 will accept altitude from a Gillham source
between the range of -1000 ft. to 62749 ft.  The KT
73 will accept altitude from an ARINC/GAMA 429 or
RS-232 source in the range of -1025 ft. to 62749 ft.
All other altitude values are considered invalid.

DISPLAY BRIGHTNESS ADJUSTMENT:

(a)

The display brightness is adjustable in the TEST mode.

(b)

Eight carets are provided below the alpha-numeric display characters to indicate 
the brightness setting (relative to the photocell reading).

(c)

Maximum brightness is indicated by all 8 carets being illuminated.

(d)

Minimum brightness is indicated by no carets being illuminated.

(e)

The factory default setting is indicated by 4 carets being illuminated.

(f)

To adjust the display brightness, place the unit into TEST mode and rotate knob 
either clockwise or counterclockwise to adjust the brightness up or down, respec-
tively.

INTERNAL EEPROM AND REMOTE CONFIGURATION MODULE:

(a)

The KT 73 has the capability to utilize a configuration module if installed.

(b)

The presence of the external configuration module is indicated by + 5 volts being 
present on Pin 2 of connector JKT73-2.

GAS DISCHARGE DISPLAY:

(a)

The brightness of the display is determined by the photocell relative to the pro-
grammed brightness level.

(b)

The illuminance is a function of the PHOTO_CEL voltage provided to the microcon-
troller from the photocell.

(c)

When going from bright to dim, an approximate 6 

±

 0.5 second time constant is 

used.

(d)

When going from bright to dim, 63% of the change will take place in each time con-
stant period.

3.3.3

BUILT IN TEST EQUIPMENT (BITE)

FAULT ANNUNCIATION:

Built In Test Equipment (BITE) failure parameters are monitored by a time averaging process to 
ensure that transient events, typical of the aircraft environment, are not the cause of fault annun-
ciation. 

The following list the fault annunciation parameters during STANDBY, GROUND, ON, and ALTI-
TUDE modes.

Critical faults are defined as faults that may cause the transponder to behave in an undetermined 
manner.  The following are critical and non-critical faults.

Impress Tryout

Preliminary - Subject To Change Without Notice

Содержание KT73

Страница 1: ...INSTALLATION MANUAL KT 73 MODE S TRANSPONDER MANUAL NUMBER 006 10563 0000 REVISION 0 OCTOBER 2002 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 2: ...uction of this publication or any portion thereof by any means without the express written permission of Honeywell is prohibited For further information contact the manager Technical Publications Honeywell One Technology Center 23500 West 105th Street Olathe KS 66061 telephone 913 782 0400 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 3: ...N HISTORY KT 73 Installation Manual Part Number 006 10563 XXXX For each revision add delete or replace pages as indicated REVISION Rev 0 October 2002 ITEM ACTION New manual No previous manual revision exists Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 4: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page RH 2 THIS PAGE IS RESERVED Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 5: ...4 2 KT 73 INSTALLATION KIT 1 6 1 5 ACCESSORIES REQUIRED BUT NOT SUPPLIED 1 7 1 6 LICENSING REQUIREMENTS 1 8 1 7 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 1 8 SECTION II INSTALLATION PARAGRAPH PAGE 2 1 GENERAL INFORMATION 2 1 2 2 UNPACKING AND INSPECTING EQUIPMENT 2 1 2 3 EQUIPMENT INSTALLATION 2 1 2 3 1 GENERAL 2 1 2 3 2 AVIONICS COOLING REQUIREMENTS FOR PANEL MOUNTED EQUIPMENT 2 2 2 3 3 KT 73 INTE...

Страница 6: ...ING 2 27 2 7 SINGLE KT 73 WITH ADLP OR ADS B INTERCONNECTION DRAWING 2 29 2 8 SINGLE KT 73 WITH SERIAL ALTITUDE INPUTS INTERCONNECTION DRAWING 2 31 2 9 DUAL KT 73 BASIC INTERCONNECTION DRAWING 2 33 2 10 DUAL KT 73 WITH SERIAL ALTITUDE INPUTS INTERCONNECTION DRAWING 2 37 2 11 RF CONNECTOR DRAWING 2 43 2 12 ACCEPTABLE CABLE CONNECTIONS DRAWING 2 45 2 13 CABLE CONNECTOR DRAWING 2 47 2 14 TYPE N AND C...

Страница 7: ...ODE 3 10 3 7 KT 73 GROUND MODE 3 10 3 8 KT 73 ON MODE 3 11 3 9 KT 73 ALTITUDE MODE 3 12 3 10 KT 73 FLIGHT ID MODE 3 13 3 11 KT 73 TEST MODE 3 13 TABLES TABLE PAGE 2 1 INSPECTION CHECK PROCEDURE 2 51 2 2 RAMP TESTS 2 53 3 1 BITE FAULT CODES 3 18 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 8: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page TC 4 THIS PAGE IS RESERVED Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 9: ...n handle include Uplink Formats 0 and 11 and Downlink Formats 0 4 5 11 16 17 and 18 The KT 73 also provides Mode C or altitude reporting information When the KT 73 is operated in the ALT Mode and used in conjunction with an encoding altimeter the flight level altitude is displayed in addition to the 4096 code and the altitude information is transmitted to the ground in response to Mode C interroga...

Страница 10: ...d for display from the front panel When the KT 73 receives Mode A interrogations from the ground radar facility it will transmit a coded group of pulses which consist of a four digit identification number that has been assigned by the Air Traffic Controller This code is entered into the KT 73 by the pilot and is transmitted back to the ground as a Mode A reply This coded information is presented o...

Страница 11: ...O DOC 9688 AN 952 RTCA DO 160D ICAO ANNEX 10 AMENDMENT 71 RTCA DO 178B RTCA DO 239 RTCA DO 260 EUROCAE ED 102 EUROCAE ED 14D EUROCAE ED 73A MOUNTING PANEL MOUNTED TEMPERATURE 20 C TO 55 C Canadian cold soak tested to 35 C ALTITUDE RANGE 51 500 FT COOLING NO FORCED AIR COOLING REQUIRED BUT RECOMMENDED VIBRATION DO 160D CATEGORY S CURVES B M CATEGORY R CURVE G ZONE 2 SHOCK RIGID MOUNTING 6 G OPERATI...

Страница 12: ... if the interrogation has nominal pulse characteristics A The MTL for ATCRBS and ATCRBS Mode S All Call interrogations will be 73 dBm 4 dB B The MTL for Mode S interrogations will be 74 dBm 3 dB C The reply ratio will be at least 99 for all Mode S interrogations between MTL 3 dB and 21 dBm and at least 90 for ATCRBS and ATCRBS Mode S All Call in terrogations between MTL and 21 dBm D The variation ...

Страница 13: ...ort Mode S downlink formats A 50 Mode S replies in a 1 second interval B 18 Mode S replies in a 100 ms interval C 8 Mode S replies in a 25 ms interval D 4 Mode S replies in a 1 6 ms interval The transponder will have the capability of generating the following reply rates for long Mode S downlink formats A At least 16 of the 50 Mode S replies in any 1 second interval B At least 6 of the 18 Mode S r...

Страница 14: ...0101 0002 PANEL MOUNT PLUG EA 1 00 030 01094 0002 CONNECTOR 12 24 P EA 1 00 030 01096 0000 KEY POLARIZER EA 1 00 030 01107 0024 CONNECTOR TERM 24T EA 1 00 030 01407 0000 CONTACT FEMALE EA 7 00 030 03454 0002 CONN RECT RECPT EA 1 00 057 05944 0024 KT 73 INSTALL KIT EA 1 00 089 02013 0037 NUT FLAT 6 32 EA 3 00 089 02147 0022 NUT LOCK 6 32 EA 2 00 089 02353 0001 NUT CLIP 6 32 EA 6 00 089 05903 0007 S...

Страница 15: ...t See Figure 2 12 Sheet 2 of 2 Honeywell PART NUMBER DESCRIPTION QUANTITY 030 00101 0002 Connector Coax 1 024 00051 0060 Cable Coax 11 ft 030 00005 0000 Connector Coax Mod Type BNC 1 Honeywell PART NUMBER DESCRIPTION QUANTITY 030 00102 0001 Connector Type Unit 1 024 00072 0000 Cable Coax 25 ft 030 00435 0000 Connector Antenna 1 Honeywell PART NUMBER DESCRIPTION QUANTITY 030 00101 0002 Connector Ty...

Страница 16: ...uirements as required 1 7 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS The instructions for continued airworthiness given in the TC or STC approvals for this product sup plements or supersedes the instructions for continued airworthiness in this manual Most Honeywell products are designed and manufactured to allow on condition maintenance On condition maintenance is described as follows There are no p...

Страница 17: ... contain information pertaining to the initial installation of the KT 73 Mode S Transponder including instructions concerning the location and mounting of the supporting an tenna The equipment should be installed in the aircraft in a manner consistent with acceptable workman ship and engineering practices and in accordance with the instructions set forth in this publication To ensure that the syst...

Страница 18: ...2 3 3 KT 73 INTERCONNECTION AND CABLE HARNESS FABRICATION 2 3 3 1 General The KT 73 Mode S Transponder receives primary power from the aircraft power source Power connections voltage requirements and circuit breaker requirements are shown on the intercon nect diagrams Figures 2 5 through 2 10 The length of the wires to parallel pins should be approximately the same length so that the best distribu...

Страница 19: ...recautions should be taken to ensure each segment of the shielded lead be grounded at only one point A ground connection of not more than two inches in length should be used The preceding discussion does not apply to coaxial and quadraxial cable 6 Avoid routing cabling near high noise and high power sources 7 Do not route the transponder antenna coax near ADF sense or loop antenna cables NOTE The ...

Страница 20: ... RS232 ALT TX This line is programmable as a Gillham altitude input or as the transmit line of an RS 232 port used to report altitude As a Gillham input HIGH voltage 18 5 VDC or resistance to ground 100KΩ Per ARINC 572 Attachment 4 input is an active LOW pulse where LOW voltage 2 0 volts or resistance to ground 15 KΩ Pin 9 9 V SUPPRESSION IN This line is a 9V Suppression Input Voltage 5 will suppr...

Страница 21: ...programmable as a Gillham altitude input as defined for pin 8 or as the transmit line reserved for a future interface Pin L GILLHAM ALTITUDE C2 RS485 TX A This line is programmable as a Gillham altitude input as defined for pin 8 or as the transmit line reserved for a future interface Pin M GILLHAM ALTITUDE A1 This line is programmable as a Gillham altitude input as defined for pin 8 Pin N TIS 429...

Страница 22: ...mit at 1090 MHz 1 00 MHz External Connector JKT73 4 Pin A AUDIO INHIBIT Mutes audio with input of 3 0 V DC or 10 ohms Input 100 K ohms will not mute This input is designed for installations including an EGPWS system In that case the Audio Out discrete of the EGPWS must be connected to this pin Pin B AIRCRAFT GROUND This pin provides an internal connection to chassis and may be used as the third wi...

Страница 23: ...for antenna cables see Figure 2 12 the lengths of the cables from the KT 73 transponder mounting tray connector to other system units are not critical because unit interfaces are designed with high impedance inputs low impedance outputs and low noise susceptibility characteristics Forced air cooling is recommended but is not a requirement Outline drawing Figure 2 4 shows transponder and mounting t...

Страница 24: ...the unit and confirm the front lobe of the hold down device is in a vertical position This can be accomplished by using a 3 32 inch Allen wrench through the front plate 2 3 5 3 Transponder 1 Slide the transponder into the tray until the front lobe touches the mounting tray 2 Turn the Allen wrench clockwise until the rear lobe engages the mounting tray slot Continue turning the wrench clockwise unt...

Страница 25: ...on 3 2 2 3 5 5 Antenna For L band blade antenna outline drawing installation procedures and mounting dimensions re fer to the manufacturer s instructions 2 3 6 MOLEX CONNECTOR ASSEMBLY PROCEDURE The KT 73 uses a special connector that mates directly with the printed circuit board inside the unit see Figure 2 1 Assemble the connector using the following procedure 2 3 6 1 Solderless Contact Terminal...

Страница 26: ...x contact ejector tool HT 1884 Honeywell P N 047 05099 0001 under the contact on the mating side of the connector By turning the connector upside down one can see the blade slide to the stop 2 When the ejector is positioned against the stop the locking key of the contact is raised allowing the contact to be removed by pulling moderately on the lead 3 Neither the contact or position is damaged by r...

Страница 27: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 11 FIGURE 2 1 CRIMPING TOOLS MOLEX Sheet 1 of 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 28: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 12 FIGURE 2 1 CRIMPING TOOLS MOLEX Sheet 2 of 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 29: ...close and the ratchet releases Straighten the terminal if necessary then release the plier grips and remove the crimped terminal CRIMPING PRESSURE ADJUSTMENT If too much or too little pressure is needed to release the crimper s ratchet pawl at the end of the crimp stroke the ratchet can be easily adjusted A spanner wrench provided with the tool can be used to loosen the lock nut and rotate the key...

Страница 30: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 14 THIS PAGE IS RESERVED Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 31: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 15 FIGURE 2 2 CRIMPING TOOLS POSITRONIC Sheet 1 of 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 32: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 16 FIGURE 2 2 CRIMPING TOOLS POSITRONIC Sheet 2 of 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 33: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 17 FIGURE 2 2 CRIMPING TOOLS POSITRONIC Sheet 3 of 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 34: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 18 THIS PAGE IS RESERVED Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 35: ...EXTERNAL STANDBY 11 I 11 33 V DC 12 I 11 33 V DC A O AIRCRAFT GROUND B I GILLHAM ALTITUDE B4 RS232 GPS RX C I GILLHAM ALTITUDE B2 RS232 GPS TX D I GILLHAM ALTITUDE C1 ARINC 429 RX 0B E I GILLHAM ALTITUDE B1 ARINC 429 RX 0A F I EXTERNAL IDENT H I GILLHAM ALTITUDE C4 RS485 RX B J I GILLHAM ALTITUDE A4 RS485 RX A K I GILLHAM ALTITUDE A2 RS485 TX B L I GILLHAM ALTITUDE C2 RS485 TX A M I GILLHAM ALTITU...

Страница 36: ... 3 O AUDIO HI 4 O 5 V DC 5 O AUDIO LO 6 I AUDIO INHIBIT A O SERIAL DATA OUT B I SERIAL DATA IN C O SERIAL CLOCK D O AIRCRAFT GROUND E I ARINC429 RX 1A RS232 RX F I O ARINC429 RX 1B RS232 TX Antenna Connector JKT73 3 Pin I O Description 1 I O RF RX TX PORT FIGURE 2 3 KT 73 Pinout Diagrams Sheet 2 of 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 37: ...nector JKT73 4 Front View Pin I O Description A I AUDIO INHIBIT B O AIRCRAFT GROUND C I ARINC429 RX 1A RS232 RX D I O ARINC429 RX 1B RS232 TX E O AUDIO HI F O AUDIO LO FIGURE 2 3 KT 73 Pinout Diagrams Sheet 3 of 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 38: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 22 THIS PAGE IS RESERVED Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 39: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 23 FIGURE 2 4 KT 73 INSTALLATION DRAWING Dwg 155 06046 0000 Rev D Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 40: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 24 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 41: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 25 FIGURE 2 5 SINGLE KT 73 BASIC INTERCONNECTION DRAWING Dwg 155 01689 0001 Rev Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 42: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 26 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 43: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 27 FIGURE 2 6 SINGLE KT 73 WITH TIS INTERCONNECTION DRAWING Dwg 155 01689 0002 Rev Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 44: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 28 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 45: ...DIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 29 FIGURE 2 7 SINGLE KT 73 WITH ADLP OR ADS B INTERCONNECTION DRAWING Dwg 155 01689 0003 Rev Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 46: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 30 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 47: ...ING KT 73 Rev 0 October 2002 10563I00 JA Page 2 31 FIGURE 2 8 SINGLE KT 73 WITH SERIAL ALTITUDE INPUTS INTERCONNECTION DRAWING Dwg 155 01689 0004 Rev Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 48: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 32 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 49: ...NDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 33 FIGURE 2 9 DUAL KT 73 BASIC INTERCONNECTION DRAWING Dwg 155 01689 0005 Rev Sheet 1 of 2 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 50: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 34 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 51: ...NDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 35 FIGURE 2 9 DUAL KT 73 BASIC INTERCONNECTION DRAWING Dwg 155 01689 0005 Rev Sheet 2 of 2 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 52: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 36 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 53: ... 73 Rev 0 October 2002 10563I00 JA Page 2 37 FIGURE 2 10 DUAL KT 73 WITH SERIAL ALTITUDE INPUTS INTERCONNECTION DRAWING Dwg 155 01689 0006 Rev Sheet 1 of 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 54: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 38 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 55: ... 73 Rev 0 October 2002 10563I00 JA Page 2 39 FIGURE 2 10 DUAL KT 73 WITH SERIAL ALTITUDE INPUTS INTERCONNECTION DRAWING Dwg 155 01689 0006 Rev Sheet 2 of 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 56: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 40 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 57: ... 73 Rev 0 October 2002 10563I00 JA Page 2 41 FIGURE 2 10 DUAL KT 73 WITH SERIAL ALTITUDE INPUTS INTERCONNECTION DRAWING Dwg 155 01689 0006 Rev Sheet 3 of 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 58: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 42 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 59: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 43 FIGURE 2 11 RF CONNECTOR DRAWING Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 60: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 44 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 61: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 45 FIGURE 2 12 ACCEPTABLE CABLE CONNECTIONS DRAWING Sheet 1 of 2 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 62: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 46 FIGURE 2 12 ACCEPTABLE CABLE CONNECTIONS DRAWING Sheet 2 of 2 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 63: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 47 FIGURE 2 13 CABLE CONNECTOR DRAWING Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 64: ... JA Page 2 48 FIGURE 2 14 TYPE N AND C CONNECTOR ASSEMBLY DRAWING PART NUMBER SIZE DIMENSION RG U CABLE A B C D 024 00075 0000 393 9 32 1 8 5 32 3 64 024 00051 0060 400 9 32 1 8 5 32 3 64 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 65: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 49 FIGURE 2 15 BNC CONNECTOR ASSEMBLY DRAWING Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 66: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 50 THIS PAGE IS RESERVED Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 67: ...rfaces 2 4 1 2 Post Installation Checkout Operation 1 General Installation of the transponder system requires three stages of testing to ensure the proper operation of the Mode S transponder Initially prior to the installation of the transponder and antenna a system interwiring check should be performed This check verifies that the aircraft and all transponder interconnections are correct be fore ...

Страница 68: ...erformed on the ground a Pretest Setup Check KT 73 system source power as follows 1 Confirm that aircraft 11 33V dc is operational 2 Confirm that the aircraft panel background lighting power source is op erational by adjusting the cockpit dimmer switch for proper cockpit panel illumination b Operate appropriate aircraft circuit breakers and switches to apply power to the system as follows 1 Apply ...

Страница 69: ... The Aircraft Address may be verified when the KT 73 is first powered on See Section 3 2 1 for details 2 Reply Frequency Verify that the reply frequency is 1090 1 MHz 2 4 1 3 Ramp Test Per AC 20 131A This test requires the use of a Mode S Ramp Tester Specific instructions for operating the ramp tester are contained in the applicable operator s manual In systems with dual transponders and altitude ...

Страница 70: ...de S All Call interrogation Proper reply address Invalid Mode S Address Verifies that the transponder does not reply to Mode S interrogations that contain invalid addresses No reply Ident Verifies Ident function is operating Reply with SPI present in ATCRBS Mode A only Reply with SPI absent Mode S UF 0 Verifies that the transponder replies to a Mode S UF 0 interrogation with the correct altitude a...

Страница 71: ...ction If the system includes the ADS B function use the following procedure requires a KLN 94 or KLN 900 1 Place the KT 73 in the Test Mode see 3 3 1 When the unit is in TST Test mode 2 After performing the self test sequence the KT 73 should display TEST OK The KT 73 will issue the audio message TEST OK 3 Switch the KLN 94 off 4 Momentarily switch the KT 73 to ON then back to the TST mode 5 The K...

Страница 72: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 2 56 THIS PAGE IS RESERVED Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 73: ...ng the aircraft engine s FIGURE 3 1 KT 73 FRONT PANEL 3 2 PROGRAMMING MODE NOTE While in the programming mode the KT 73 will not transmit RF energy The programming mode is entered using the following procedure 1 Place the unit in Standby mode 2 Select 0000 ident code 3 Simultaneously depress the IDT and VFR buttons for a minimum of 2 seconds To select the programming mode menu rotate the cursor CR...

Страница 74: ...2 use the fol lowing procedure 1 Rotate the CRSR knob to move across the major headings 2 Press the IDT button to select a particular heading option 3 Rotate the cursor CRSR knob to cycle between choices For example when ALT SRC is selected as the major heading option the CRSR knob is rotated to cycle between the following choices 429 706 RS 232 Gillham If the RS 232 sub menu option is selected th...

Страница 75: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 3 3 FIGURE 3 2 KT 73 CONFIGURATION MENU Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 76: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA Page 3 4 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 77: ...A C ADDR When the unit is in the A C ADDR Aircraft Address program menu a The aircraft address is programmable see section 2 3 5 4 for address information b The aircraft address consists of 8 octal digits FIGURE 3 3 KT 73 FIRST 4 OCTAL DIGITS OF THE AIRCRAFT ADDRESS FIGURE 3 4 KT 73 LAST 4 OCTAL DIGITS OF THE AIRCRAFT ADDRESS Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 78: ... c 150 to 300 d 300 to 600 e 600 to 1200 f to 1200 FIGURE 3 5 KT 73 LOWER AND UPPER MAXIMUM AIRSPEED ALT SRC The ALT SRC altitude source is programmable to the following a ARINC 429 706 b RS 232 Shadin 8800M Shadin 8800G Shadin 8800T c Gillham NOTE If a Trancal RS 232 altitude source is used refer to the manufacturer s data to configure it as 8800M 8800G or 8800T Impress Tryout Preliminary Subject...

Страница 79: ...d ADS B JKT73 1 Pin B GPS RX e ADLP and ADS B JKT73 1 Pin B GPS RX f Non XPDR JKT73 1 Pin B GPS RX g None AUTO GND The KT 73 has AUTO GND Automatic Ground Programming capability when enabled a Enable b Inhibit NOTE Automatic Grounding refers to external discrete be ing connected to the landing gear strut switch where applicable AIR VOL Air Volume includes one of the following audio power levels wh...

Страница 80: ...he KT 73 s ADS B Emitter Categories are configurable to one of the following a Category set A code 0 No ADS B Emitter Category Information 1 Light 15 500 lbs 2 Small 15 500 to 75 000 lbs 3 Large 75 000 to 300 000 lbs 4 High Vortex Large aircraft such as B 757 5 Heavy 300 000 lbs 6 High Performance 5g acceleration and 400 knots 7 Rotorcraft b Category set B code 0 No ADS B Emitter Category Informat...

Страница 81: ...e select switch see the display below The following modes are available a OFF b SBY Standby c GND Ground d ON On e ALT Altitude f FLT ID Flight ID g TST Test OFF The unit is not energized When the unit is in the OFF mode the Backlighting will be illuminated if either the 14 VDC or 28 VDC lighting bus has power applied When the unit is powered up switched from the OFF position to another mode the f...

Страница 82: ... any interrogation b SBY will be annunciated in the Altitude window c The 4096 code will be displayed in the Ident window d The unit will enter the next selected mode within 5 seconds of coming out of the STANDBY mode GND see below FIGURE 3 7 KT 73 GROUND MODE NOTE This feature is controlled by the AUTOGND feature of the installation menu Impress Tryout Preliminary Subject To Change Without Notice...

Страница 83: ...f coming out of the GROUND mode i Altitude reporting will be enabled ON see below FIGURE 3 8 KT 73 ON MODE When the unit is in the ON mode a The transmission of altitude information will be inhibited 1 The ATCRBS framing pulses in ATCRBS Mode C replies will be retained 2 All ZEROs will be transmitted in the altitude field of the Mode S replies b The altitude window will be blank c The 4096 code wi...

Страница 84: ...aming pulses if the derived altitude is invalid altitude not available in response to an accepted Mode C interrogation e The unit will transmit zeros in each of the 13 bits of the AC field if the derived alti tude is invalid altitude not available in response to an accepted Mode S interroga tion f The unit will display altitude information according to Altitude Display parameters see listing in se...

Страница 85: ...e FLT ID nomenclature will be displayed d The ability to modify the Flight ID will be provided only if Flight ID is not received from the ADLP source e The unit will not transmit f An asterisk will be displayed for characters that are not alphanumeric OR a space for Flight ID received from an ADLP NOTE Spaces will be removed from Flight ID when entered from the front panel TST see below FIGURE 3 1...

Страница 86: ...primary fault and YY repre sents the secondary fault The audio message TRANSPONDER TEST FAIL is issued if any critical fault exists f If more than one fault is detected by BITE the ident window will cycle through de tected fault codes g If BITE determines that a fault is not active the ident window will display only the active faults h If BITE determines that all faults are cleared TEST is display...

Страница 87: ...of 18 1 seconds b Ground Mode Depressing the IDT momentary contact switch while in the GROUND mode 1 will cause the special position identification pulse SPI to be reflected in the Flight Status field of Mode S downlink format 4 AND 5 replies to discretely addressed Mode S interroga tions for a period of 18 1 seconds 2 will cause the unit to display the IDT nomenclature for a period of 18 1 second...

Страница 88: ...r the code is displayed REPLY If the unit is replying to a valid Mode S interrogation the reply nomenclature R will be illuminated twice per second If the unit is replying to ATCRBS interrogations the reply nomenclature R will be illuminated once per second ALTITUDE DISPLAY a When in the ALTITUDE mode when an altitude source is available and when the derived altitude is valid the KT 73 will displa...

Страница 89: ... 73 has the capability to utilize a configuration module if installed b The presence of the external configuration module is indicated by 5 volts being present on Pin 2 of connector JKT73 2 GAS DISCHARGE DISPLAY a The brightness of the display is determined by the photocell relative to the pro grammed brightness level b The illuminance is a function of the PHOTO_CEL voltage provided to the microco...

Страница 90: ...Hardware 3 RAM Initial Verification 04 Critical Hardware 3 RAM Verification 05 Critical Hardware 3 3 3V 06 Critical Hardware 3 5V 07 Critical Hardware 3 6V 08 Critical Hardware 3 12V 09 Critical Hardware 3 65V 10 Critical Hardware 3 95V 11 Critical Hardware 3 12V 12 Critical Hardware 3 90V 13 Critical Hardware 3 5V 14 Critical Hardware 3 Suppression 15 Critical Hardware 3 ATCRBS Tx Data 16 Critica...

Страница 91: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA TSO 1 TSO APPENDIX ENVIRONMENTAL QUALIFICATION FORMS Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 92: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA TSO 2 THIS PAGE IS RESERVED Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 93: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA TSO 3 Impress Tryout Preliminary Subject To Change Without Notice ...

Страница 94: ...BENDIX KING KT 73 Rev 0 October 2002 10563I00 JA TSO 4 THIS PAGE IS RESERVED Impress Tryout Preliminary Subject To Change Without Notice ...

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