Honeywell KTR2280 User Manual

SYSTEM INSTALLATION

MANUAL (Preliminary)

KTR 2280

MULTI-MODE

DIGITAL RADIO (MMDR)

MANUAL NUMBER 006-10654-0000

Revision 0 AUGUST, 2006

This document contains technical data and is subject to U.S. export regulations. These commodities, technology, or software were exported from the United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited.

Honeywell - Confidential

THIS DOCUMENT AND ALL INFORMATION AND EXPRESSION CONTAINED HEREIN ARE THE PROPERTY OF HONEYWELL INTERNATIONAL INC., ARE PROVIDED IN CONFIDENCE, AND MAY BE USED BY PERSONS REQUIRED BY 14 CFR 21.50 TO COMPLY WITH ANY OF THE TERMS OF THESE INSTRUCTIONS. EXCEPT AS SET FORTH ABOVE, NO PERSON MAY, IN WHOLE OR IN PART, USE, DUPLICATE OR DISCLOSE THIS INFORMATION FOR ANY PURPOSE WITHOUT THE PRIOR WRITTEN PERMISSION OF HONEYWELL INTERNATIONAL INC.

n KTR 2280 Preliminary H 08/17/06

Honeywell Materials License Agreement

The documents and information contained herein ("the Materials") are the proprietary data of Honeywell International Inc. and Honeywell Intellectual Properties Inc. (collectively "Honeywell"). These Materials are provided for the exclusive use of Honeywell Service Centers; Honeywell-authorized repair facilities; operators of Honeywell aerospace products subject to an applicable product support agreement, their wholly owned-subsidiaries or a formally designated third party service provider thereunder; and direct recipients of Materials from Honeywell's Aerospace Technical Publication Distribution. The terms and conditions of this License Agreement govern your use of these Materials, except to the extent that any terms and conditions of another applicable agreement with Honeywell regarding the operation, maintenance, or repair of Honeywell aerospace products conflict with the terms and conditions of this License Agreement, in which case the terms and conditions of the other agreement will govern. However, this License Agreement will govern in the event of a conflict between its terms and conditions and those of a purchase order or acknowledgement.

1. License Grant - If you are a party to an applicable product support agreement, a Honeywell Service

Center agreement, or an authorized repair facility agreement, Honeywell hereby grants you a limited, non-exclusive license to use these Materials to operate, maintain, or repair Honeywell aerospace products only in accordance with that agreement.

If you are a direct recipient of these Materials from Honeywell's Aerospace Technical Publication Distribution and are not a party to an agreement related to the operation, maintenance or repair of Honeywell aerospace products, Honeywell hereby grants you a limited, non-exclusive license to use these Materials to maintain or repair the subject Honeywell aerospace products only at the facility to which these Materials have been shipped ("the Licensed Facility"). Transfer of the Materials to another facility owned by you is permitted only if the original Licensed Facility retains no copies of the Materials and you provide prior written notice to Honeywell.

2. Rights In Materials - Honeywell retains all rights in these Materials and in any copies thereof that are not expressly granted to you, including all rights in patents, copyrights, trademarks, and trade secrets. No license to use any Honeywell trademarks or patents is granted under this License Agreement.

3. Confidentiality - You acknowledge that these Materials contain information that is confidential and proprietary to Honeywell. You agree to take all reasonable efforts to maintain the confidentiality of these Materials.

4. Assignment And Transfer - This License Agreement may be assigned to a formally designated service designee to the extent allowed under an applicable product support agreement or transferred to a subsequent owner or operator of an aircraft containing the subject Honeywell aerospace products. However, the recipient of any such assignment or transfer must assume all of your obligations under this License Agreement. No assignment or transfer shall relieve any party of any obligation that such party then has hereunder.

5. Copies of Materials - Unless you have the express written permission of Honeywell, you may not make or permit making of copies of the Materials. Notwithstanding the foregoing, you may make copies of only portions of the Material for your internal use. You agree to return the Materials and any copies thereof to Honeywell upon the request of Honeywell.

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page MLA-1

n KTR 2280 Preliminary H 08/17/06

6. Term - This License Agreement is effective until terminated as set forth herein. This License Agreement will terminate immediately, without notice from Honeywell, if you fail to comply with any provision of this License Agreement or will terminate simultaneously with the termination or expiration of your applicable product support agreement, authorized repair facility agreement, or your formal designation as a third party service provider. Upon termination of this License Agreement, you will return these Materials to Honeywell without retaining any copies and will have one of your authorized officers certify that all Materials have been returned with no copies retained.

7. Remedies - Honeywell reserves the right to pursue all available remedies and damages resulting from a breach of this License Agreement.

8. Limitation of Liability - IN NO EVENT WILL HONEYWELL BE LIABLE FOR ANY INCIDENTAL DAMAGES, CONSEQUENTIAL DAMAGES, SPECIAL DAMAGES, INDIRECT DAMAGES, LOSS OF PROFITS, LOSS OF REVENUES, OR LOSS OF USE, EVEN IF INFORMED OF THE POSSIBILITY OF SUCH DAMAGES. TO THE EXTENT PERMITTED BY APPLICABLE LAW, THESE LIMITATIONS AND EXCLUSIONS WILL APPLY REGARDLESS OF WHETHER LIABILITY ARISES FROM BREACH OF CONTRACT, WARRANTY, TORT (INCLUDING BUT NOT LIMITED TO NEGLIGENCE), BY OPERATION OF LAW, OR OTHERWISE.

9. Controlling Law - This License shall be governed and construed in accordance with the laws of the State of New York without regard to the conflicts of laws provisions thereof. This license sets forth the entire agreement between you and Honeywell and may only be modified by a writing duly executed by the duly authorized representatives of the parties.

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page MLA-2

n KTR 2280 Preliminary H 08/17/06

REVISION HIGHLIGHTS

KTR 2280 Preliminary H 08/17/06

Part Number Rev Date Description

006-10654-0000 0 Aug/2006 Initial Release

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page RH-1

n KTR 2280 Preliminary H 08/17/06

REVISION HIGHLIGHTS

Part Number Rev Date Description

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page RH-2

n KTR 2280 Preliminary H 08/17/06

TABLE OF CONTENTS

SECTION 1

GENERAL INFORMATION

1.1 INTRODUCTION ......................................................................................................... 1-1

1.2 EQUIPMENT DESCRIPTION...................................................................................... 1-1

1.3 TECHNICAL CHARACTERISTICS............................................................................. 1-2

1.3.1 KTR 2280 TECHNICAL CHARACTERISTICS ............................................................ 1-2

1.3.2 KA 44B ADF ANTENNA TECHNICAL CHARACTERISTICS...................................... 1-3

1.4 UNITS AND ACCESSORIES SUPPLIED ................................................................... 1-3

1.4.1 CONFIGURATIONS AVAILABLE................................................................................ 1-3

1.4.2 KTR 2280 INSTALLATION KIT ................................................................................... 1-3

1.5 ACCESSORIES REQUIRED, BUT NOT SUPPLIED.................................................. 1-5

1.6 LICENSING REQUIREMENTS ................................................................................... 1-6

1.7 CONTINUED AIRWORTHINESS INSTRUCTIONS .................................................... 1-6

1.7.1 EQUIPMENT ............................................................................................................... 1-6

1.7.2 WIRES/COAX CABLES............................................................................................... 1-7

1.8 ANTENNA RF EXPOSURE ........................................................................................ 1-7

SECTION 2

INSTALLATION

2.1 GENERAL INFORMATION......................................................................................... 2-1

2.2 UNPACKING AND INSPECTING EQUIPMENT ......................................................... 2-1

2.3 EQUIPMENT INSTALLATION .................................................................................... 2-1

2.3.1 AVIONICS COOLING REQUIREMENTS .................................................................... 2-1

2.3.2 EQUIPMENT LOCATION ............................................................................................ 2-1

2.3.2.1 MOUNTING TRAY LOCATION(S) .............................................................................. 2-2

2.3.2.2 ANTENNA(S)...............................................................................................................2-2

2.3.3 KTR 2280 MECHANICAL INSTALLATION ................................................................. 2-3

2.3.4 ANTENNA MECHANICAL INSTALLATION ................................................................2-3

2.3.4.1 VHF COM TRANSMITTER/RECEIVER ANTENNA .................................................... 2-3

2.3.4.2 NAVIGATION ANTENNAS ..........................................................................................2-4

2.3.4.3 KA 44B ADF ANTENNA .............................................................................................. 2-5

2.3.5 ELECTRICAL INSTALLATION .................................................................................... 2-6

2.3.5.1 KTR 2280 INTERCONNECTION AND CABLE HARNESS FABRICATION................ 2-6

2.3.5.2 PRIMARY POWER AND CIRCUIT BREAKER REQUIREMENTS ............................. 2-7

2.3.5.3 CONNECTOR PIN FUNCTIONAL DESCRIPTIONS................................................... 2-8

2.3.5.4 CRIMP TOOL INFORMATION .................................................................................. 2-11

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page TOC-1

n KTR 2280 Preliminary H 08/17/06

TABLE OF CONTENTS

2.4 POST-INSTALLATION CHECKS ............................................................................. 2-29

2.4.1 KTR 2280 MMDR SYSTEM CHECKOUT ................................................................. 2-29

2.4.1.1 INSPECTION............................................................................................................. 2-29

2.4.1.2 POST-INSTALLATION CHECKOUT/OPERATION................................................... 2-30

SECTION 3

OPERATION

3.1 GENERAL ................................................................................................................... 3-1

3.2 RADIO TUNING WINDOW.......................................................................................... 3-1

3.2.1 VHF COM TUNING SUB-WINDOW ............................................................................ 3-2

3.2.1.1 ACTIVE FREQUENCY ................................................................................................ 3-2

3.2.1.2 VOLUME CONTROL INDICATION/SCALE ................................................................ 3-3

3.2.1.3 SOFT KEY IDENTIFIER/SOFT KEY SWAP IDENTIFIER........................................... 3-3

3.2.1.4 SQUELCH INHIBIT ANNUNCIATOR .......................................................................... 3-3

3.2.1.5 TRANSMIT/RECEIVE ANNUNCIATOR ...................................................................... 3-3

3.2.1.6 STANDBY FREQUENCY ............................................................................................ 3-3

3.2.1.7 STUCK MICROPHONE ANNUNCIATION .................................................................. 3-3

3.2.2 COM DETAIL WINDOW .............................................................................................. 3-4

3.2.3 VHF NAV TUNING SUB-WINDOW ............................................................................. 3-4

3.2.3.1 ACTIVE FREQUENCY ................................................................................................ 3-5

3.2.3.2 VOLUME CONTROL INDICATION/SCALE ................................................................ 3-5

3.2.3.3 SOFT KEY IDENTIFIER/SOFT KEY SWAP IDENTIFIER........................................... 3-5

3.2.3.4 DME ASSOCIATION/HOLD ANNUNCIATOR............................................................. 3-5

3.2.3.5 MORSE CODE ID ANNUNCIATOR ............................................................................ 3-5

3.2.3.6 STANDBY FREQUENCY/VOR BEARING .................................................................. 3-5

3.2.4 NAV DETAIL WINDOW ............................................................................................... 3-6

3.2.5 DME DETAIL WINDOW .............................................................................................. 3-6

3.2.6 ADF TUNING SUB-WINDOW ..................................................................................... 3-7

3.2.6.1 ADF FREQUENCY ......................................................................................................3-7

3.2.6.2 VOLUME CONTROL INDICATION/SCALE ................................................................ 3-7

3.2.6.3 SOFT KEY IDENTIFIER.............................................................................................. 3-7

3.2.6.4 ADF MODE..................................................................................................................3-7

3.2.7 ADF DETAIL WINDOW ............................................................................................... 3-8

3.3 KTR 2280 OPERATION .............................................................................................. 3-8

3.3.1 VHF COM CONTROLS ............................................................................................. 3-10

3.3.1.1 DETAIL BUTTON ...................................................................................................... 3-10

3.3.1.2 COM BUTTON........................................................................................................... 3-10

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page TOC-2

n KTR 2280 Preliminary H 08/17/06

TABLE OF CONTENTS

3.3.1.3 TUNING SELECT (SEL) CONTROL ........................................................................ 3-10

3.3.1.4 FREQUENCY SWAP................................................................................................. 3-10

3.3.2 VHF NAV CONTROLS .............................................................................................. 3-11

3.3.2.1 DETAIL BUTTON ...................................................................................................... 3-11

3.3.2.2 NAV BUTTON............................................................................................................ 3-11

3.3.2.3 TUNING SELECT (SEL) CONTROL ........................................................................ 3-11

3.3.2.4 FREQUENCY SWAP................................................................................................. 3-11

3.3.2.5 VOL/SQ/ID KNOB...................................................................................................... 3-12

3.3.2.6 NAV DETAIL WINDOW SOFT KEYS........................................................................ 3-12

3.3.2.7 DME DETAIL WINDOW SOFT KEYS ....................................................................... 3-12

3.3.3 ADF CONTROLS....................................................................................................... 3-12

3.3.3.1 DETAIL BUTTON ...................................................................................................... 3-12

3.3.3.2 ADF DETAIL WINDOW SOFT KEYS ........................................................................ 3-12

APPENDIX A

ENVIRONMENTAL QUALIFICATION FORMS

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page TOC-3

n KTR 2280 Preliminary H 08/17/06

TABLE OF CONTENTS

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page TOC-4

n KTR 2280 Preliminary H 08/17/06

LIST OF FIGURES

FIGURE 2-1 MAIN CONNECTOR - J1 ............................................................................. 2-8

FIGURE 2-2 KA 44/44B PIN LOCATION DIAGRAM ...................................................... 2-10

FIGURE 2-3 KTR 2280 INSTALLATION DRAWING ...................................................... 2-13

FIGURE 2-4 KTR 2280 BAR CLAMP ASSEMBLY DRAWING....................................... 2-21

FIGURE 2-5 KA 44B OUTLINE AND MOUNTING DRAWING (-0000)........................... 2-23

FIGURE 2-6 KA 44B OUTLINE AND MOUNTING DRAWING (-0010)........................... 2-25

FIGURE 2-7 KA 44B ANTENNA CABLE ASSEMBLY (-0020) .......................................2-27

FIGURE 3-1 RADIO TUNING WINDOW .......................................................................... 3-2

FIGURE 3-2 VHF COM TUNING SUB-WINDOW............................................................. 3-2

FIGURE 3-3 STUCK MICROPHONE ANNUNCIATION ................................................... 3-3

FIGURE 3-4 VHF COM DETAIL WINDOW ...................................................................... 3-4

FIGURE 3-5 VHF NAV TUNING SUB-WINDOW.............................................................. 3-4

FIGURE 3-6 VHF NAV BEARING DISPLAY .................................................................... 3-5

FIGURE 3-7 VHF NAV DETAIL WINDOW ....................................................................... 3-6

FIGURE 3-8 DME DETAIL WINDOW ............................................................................... 3-6

FIGURE 3-9 ADF TUNING SUB-WINDOW ...................................................................... 3-7

FIGURE 3-10 DUAL ADF DETAIL WINDOW ..................................................................... 3-8

FIGURE 3-11 KMC 2210 PFD CONTROLLER................................................................... 3-8

FIGURE 3-12 KDU 1080 DISPLAY UNIT BEZEL SOFT KEYS.......................................... 3-9

FIGURE 3-13 KMC 2220 MF CONTROLLER..................................................................... 3-9

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page LOF-1

n KTR 2280 Preliminary H 08/17/06

LIST OF FIGURES

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page LOF-2

n KTR 2280 Preliminary H 08/17/06

LIST OF TABLES

TABLE 1-1 KXP 2290 TECHNICAL CHARACTERISTICS............................................. 1-2

TABLE 2-1 J1 PIN FUNCTION LIST .............................................................................2-8

TABLE 2-2 ANTENNA CONNECTORS AND DESCRIPTIONS ..................................... 2-9

TABLE 2-3 KA 44B PIN FUNCTION LIST .................................................................... 2-10

TABLE 2-4 SIZE 22 HIGH DENSITY D-SUB CONTACT TOOLS ................................ 2-11

TABLE 2-5 INSPECTION/CHECK PROCEDURE........................................................ 2-29

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page LOT-1

n KTR 2280 Preliminary H 08/17/06

LIST OF TABLES

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page LOT-2

n KTR 2280 Preliminary H 08/17/06

SECTION 1

GENERAL INFORMATION

1.1 INTRODUCTION

This manual contains information relative to the physical, mechanical, and electrical characteristics of the Honeywell KTR 2280 Multi-Mode Digital Radio (MMDR). Installation and check out procedures are also included. Information relative to the maintenance, alignment, and procurement of the replacement parts may be found in the KTR 2280 Maintenance/Overhaul Manual, P/N 006-15654-XXXX. The only current KTR 2280 installation option is as a part of the APEX system. For additional information relating to the APEX system, refer to the APEX System Manual 006-10667-XXXX or applicable Engineering Bulletin (EB). This manual, the Apex System Manual, and the applicable EB define the recommended installation for the KTR 2280. Final design of the installation and airworthiness approval is incumbent upon the installer and their respective certification authority.

1.2 EQUIPMENT DESCRIPTION

The KTR 2280 APEX MMDR Transceiver is a blind, panel mount integrated transceiver containing one transmitter and four receivers. The KTR 2280 operates at a nominal voltage of 27.5 VDC. The KTR 2280 is controlled by APEX LRU's which send control information to the KTR 2280 via ARINC 429. Some outputs from the KTR 2280 are in digital formats and sent to other LRU's via ARINC 429. Other outputs are more traditional analog outputs.

The transmitter is a 2280 channel, 16 Watt COM transmitter capable of 8.33 kHz channel spacing operation. The four receivers include one 200 channel NAV receiver, one 40 channel glideslope receiver, one COM receiver, and one ADF receiver. The COM receivers have 2280 channels and are capable of 8.33 kHz channel spacing. The ADF tunes frequencies from 190 kHz to 1799 kHz and 2180 kHz to 2189 kHz. The KTR 2280 has no user interface and is completely controlled by other components of the APEX system via ARINC 429.

The KTR 2280 contains BIT (Built In Test) equipment so that the operational health of the unit is constantly monitored. When a critical fault is detected, the unit notifies the APEX system. The unit stores detected failures in non-volatile memory for later review. The unit also has a temperature sensor and a timer so that faults can be time stamped and temperature data can be collected and stored.

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page 1-1

n KTR 2280 Preliminary H 08/17/06

1.3 TECHNICAL CHARACTERISTICS

1.3.1 KTR 2280 TECHNICAL CHARACTERISTICS

SPECIFICATION

CHARACTERISTIC

TSO COMPLIANCE COM TRANSMIT: COM RECEIVE: VOR: LOC: GS: ADF: STUCK MICROPHONE:

SOFTWARE CERTIFICATION

TSO C37d, ETSO 2C37e TSO C38d, ETSO 2C38e TSO C40c, ETSO 2C40c TSO C36e, ETSO 2C36f TSO C34e, ETSO 2C34f TSO C41D, ETSO 2C41b TSO C41D, ETSO 2C41b

RTCA/DO-178B SOFTWARE LEVEL “C”

CATEGORY:

ENVIRONMENTAL

SEE APPENDIX A

CATEGORIES:

PHYSICAL DIMENSIONS: SEE FIGURE 2-3 KTR 2280 INSTALLATION

DRAWING

WEIGHT: SEE FIGURE 2-3 KTR 2280 INSTALLATION

DRAWING

MOUNTING: BLIND, RACK MOUNT BEHIND PANEL

TEMPERATURE: SEE APPENDIX A

ALTITUDE: SEE APPENDIX A

COOLING: INTERNAL FAN & EXTERNAL RACK MOUNTED

FAN

POWER INPUT: 16-33 VOLTS

POWER REQUIREMENTS RECEIVE (NOMINAL): RECEIVE (MAXIMUM): TRANSMIT (NOMINAL): TRANSMIT (MAXIMUM):

TABLE 1-1 KXP 2290 TECHNICAL CHARACTERISTICS

27.5 V @ 0.76A

27.5 V @ 1.02A

27.5 V @ 4.33A

27.5 V @ 6.11A

Rev. 0, Aug/2006 ©Honeywell International Inc. Do not print without express permission of Honeywell Page 1-2

n KTR 2280 Preliminary H 08/17/06

1.3.2 KA 44B ADF ANTENNA TECHNICAL CHARACTERISTICS

SPECIFICATION

CHARACTERISTIC

TSO COMPLIANCE: SEE APPENDIX A

ENVIRONMENTAL

SEE APPENDIX A

SPECIFICATIONS:

PHYSICAL DIMENSIONS: SEE FIGURE 2-5 KA 44B OUTLINE AND

MOUNTING DRAWING (-0000)/FIGURE 2-6 KA 44B OUTLINE AND MOUNTING DRAWING (-0010)

WEIGHT: SEE FIGURE 2-5 KA 44B OUTLINE AND

MOUNTING DRAWING (-0000)/FIGURE 2-6 KA 44B OUTLINE AND MOUNTING DRAWING (-0010)

POWER REQUIREMENTS: 8.5 +/-0.5 VDC at 100mA max (supplied by

KTR 2280)

1.4 UNITS AND ACCESSORIES SUPPLIED

1.4.1 CONFIGURATIONS AVAILABLE

P/N 069-01037-0101 is the only version of the KTR 2280 that is currently available.

1.4.2 KTR 2280 INSTALLATION KIT

NOTE: The following installation kit information is presented at the revision existing at the

time of this publication. Future revisions to these kits may occur. Use the latest revision of the kit as provided by Honeywell.

The KTR 2280 MMDR installation kit P/N 050-03721-0000 contains the following parts:

PN DESCRIPTION REV

----------------------------------------------------------------------050-03721-0000 INSTALL KIT KTR 2280 B

------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000

------------------------------------------------------------------------------------------------J1 030-03296-0000 HI DENSITY SUBD44P EA 1.00 J101 030-00101-0002 PANEL MOUNT PLUG EA 1.00 J102 030-00101-0002 PANEL MOUNT PLUG EA 1.00 J103 030-00101-0002 PANEL MOUNT PLUG EA 1.00 J104 030-00101-0002 PANEL MOUNT PLUG EA 1.00 J501 148-05199-0003 FAN 25X25X15MM, 4.06CFM, 55MM TEF WIRE, WITH CONN EA 1.00 001-01299-0000 INSTRUCTION FOR HARNESS ASSEMBLY PARTS RF .00 J1 030-03296-0000 HI DENSITY SUBD44P EA 1.00

n KTR 2280 Preliminary H 08/17/06

PN DESCRIPTION REV

----------------------------------------------------------------------050-03721-0000 INSTALL KIT KTR 2280 B

------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000

------------------------------------------------------------------------------------------------ 030-01458-0000 CONTACT, SOCKET, SIZE 22 EA 44.00 047-11179-0002 STRAIN RELIEF CLAMP MED EA 1.00 047-11310-0004 RACK, W/FINISH EA 1.00 057-05944-0073 KTR 2280 KIT TSO LABEL EA 1.00 073-01140-0003 BACKPLATE W/HARDWARE EA 1.00 073-01141-0002 CONNECTOR HOOD SUB D 25 90 DEG W/FINISH EA 1.00 073-01142-0002 CONN HOOD COVER W/FINISH EA 1.00 076-03189-0001 SCREW 100DEG FHP 2-56 X 3/8 SPECIAL EA 5.00 088-03559-0001 FAN GUARD EA 1.00 089-05874-0014 SCR PHP 2-56X7/8 EA 4.00 089-05878-0005 SCR PHP 4-40 X 5/16 EA 1.00 089-05903-0004 SCR PHP 4-40X1/4 EA 3.00 089-06008-0004 SCR FHP 4-40X1/4 EA 2.00 089-08252-0030 WASHER EA 8.00 090-00019-0007 RING RTNR .438 EA 4.00 091-00464-0002 CABLE TIE, 5.62 INCH EA 1.00 155-03009-0001 CABLE ASSY, POWER, KTR2280 FAN EA 1.00 155-06081-0000 INSTALL DRAWING MMDR KTR 2280 RF .00 200-10452-0001 BAR CLAMP ASSEMBLY -15 EA 1.00

Shield braids must be clamped to the connector backshell using bar clamp assembly P/N 200-10452-0001 which contains the following parts. See FIGURE 2-3 KTR 2280

INSTALLATION DRAWING and FIGURE 2-4 KTR 2280 BAR CLAMP ASSEMBLY DRAWING for additional information.

PN DESCRIPTION REV

----------------------------------------------------------------------200-10452-0001 BAR CLAMP ASSEMBLY -15 -

------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0001

------------------------------------------------------------------------------------------------REF1 300-10452-0000 BAR CLAMP ASSEMBLY KMC 2220 RF .00 047-11178-0002 BACKSHELL BAR CLAMP MED EA 1.00 076-03190-0001 SCREW PHP 4-40 X 7/16 SPECIAL EA 2.00 187-01943-0002 BACKSHELL GASKET MEDIUM EA 1.00

n KTR 2280 Preliminary H 08/17/06

The KA 44B antenna installation kit P/N 050-01756-0020 contains the following parts:

PN DESCRIPTION REV

----------------------------------------------------------------------050-01756-0020 INSTALL KIT 48 FT MMDR KA 44B SO-160D A

------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0020

------------------------------------------------------------------------------------------------ 030-00101-0000 PANEL MNT PLUG EA 1.00 057-02259-0000 ANT MTG TEMPLATE EA 1.00 057-05944-0074 KA 44B KIT TSO LABEL EA 1.00 076-01042-0001 FERRULE W/F EA 1.00 090-00019-0007 RING RTNR .438 EA 1.00 091-00031-0005 NY CA CLAMP .312 EA 1.00 200-02586-0020 ANT CBL ASSY 48FT KA 44B DO-160D EA 1.00

The KA 44B antenna cable assembly P/N 200-02586-0020 contains the following parts:

PN DESCRIPTION REV

----------------------------------------------------------------------200-02586-0020 ANT CBL ASSY 48FT KA 44B DO-160D E

------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0020

------------------------------------------------------------------------------------------------ 025-00001-0000 WIRE, HOOKUP, PTFE, 26 (7/34)AWG SPC, BLK IN 8.20 025-05120-0000 WIRE, TIN PLTD CU SHLD, 5-24 (19/36)AWG TPC COND IN 578.00 026-00029-0000 WIRE, CU, 22AWG, TINNED IN 3.00 030-01157-0011 SOCKET CRMP 20G EA 9.00 030-01171-0000 CONN SUB-D HSG 9S (FEMALE PINS) EA 1.00 030-02351-0000 HOOD/LVR ASSY ST E EA 1.00 150-00024-0010 TUBING SHRINK 10G IN 2.00 150-00049-0010 SHRINK TUBING WHT IN .75 150-00052-0010 SHRNK TUBING WHT IN 4.50 300-02586-0020 ANTENNA CABLE INTERCONNECT KA 44B DO-160D RF .00 53001150-1 50 OHM QUADRAXIAL CABLE FT 48.17

1.5 ACCESSORIES REQUIRED, BUT NOT SUPPLIED

A. Broadband Communications Antenna (50 ohms) B. VHF Navigation Antenna (50 ohms) C. Glideslope Antenna D. Antenna Splitter(s) E. ADF Antenna (representative type KA 44B)

The KA 44B, P/N 071-1234-XX, is a low profile ADF Antenna which contains both loop and sense antennas, preamplifiers, and modulators which combine the antenna signals into a single RF signal which is output to the KTR 2280 via a quadaxial cable of non-critical length. The KA 44B is available in four versions. KA 44B antenna P/N 071-1234-00/03 includes a mounting plate. KA 44B P/N 071-1234-01 includes a grounding ring. KA 44B P/N 071-1234-02 has no mounting plate and has the QE adjust accessible vertically.

n KTR 2280 Preliminary H 08/17/06

1.6 LICENSING REQUIREMENTS

The KTR 2280 meets CFR Title 47, Part 15 and Part 2 (FCC Approvals) for all radio equipment. For non-US registered aircraft, follow applicable licensing requirements as required.

The Federal Communications Commission requires that the operator of the transmitter of this equipment hold a restricted radio telephone operators permit (FCC Form 605) or higher class license. A permit may be obtained by a U.S. citizen from the nearest field office of the FCC; no examination is required. An Aircraft Station License is required for this equipment. Forms (FCC Form 605, New Aircraft Station License, or FCC Form 405A, Renewal of Aircraft Station License) can be obtained from the nearest FCC Field Office. This equipment has been type accepted by the FCC and entered on their list of type accepted equipment as Honeywell KTR 2280 and must be identified as Honeywell KTR 2280 on FCC Form 605, Aircraft Radio Station License Application.

CAUTION: THE VHF TRANSMITTER IN THIS EQUIPMENT IS GUARANTEED TO

MEET FEDERAL COMMUNICATIONS COMMISSION ACCEPTANCE OVER THE OPERATING TEMPERATURE RANGE ONLY WHEN A HONEYWELL CRYSTAL IS USED IN THE STABILIZED MASTER OSCILLATOR. USE OF OTHER THAN HONEYWELL CRYSTALS IS CONSIDERED AN UNAUTHORIZED MODIFICATION, AND WILL VOID THE WARRANTY.

1.7 CONTINUED AIRWORTHINESS INSTRUCTIONS

1.7.1 EQUIPMENT

The instructions for continued airworthiness given in the TC or STC approvals for this product supplements 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 periodic service requirements necessary to maintain continued airworthiness. No maintenance is required until the equipment does not properly perform its intended function. When service is required, a complete performance test should be accomplished following any repair action. Consult the appropriate unit Maintenance/Overhaul Manual for complete performance test information.

14 CFR Part 25.1529 Instructions for Continued Airworthiness is met per the following instructions:

A. The removal of the equipment is on the condition of failure. There is no re-

quired maintenance

n KTR 2280 Preliminary H 08/17/06

1.7.2 WIRES/COAX CABLES

During on-condition or regularly scheduled maintenance, inspect the wires and coax cables following the guidelines listed in AC 43.13-1B Chapter 11, 12 as necessary.

1.8 ANTENNA RF EXPOSURE

WARNING: TO MINIMIZE RF EXPOSURE TO PERSONNEL, INSTALL THE

ANTENNA GENERALLY AWAY FROM AREAS WHERE PEOPLE ARE LOCATED. IN SITUATIONS WHERE A PERSON WOULD BE DIRECTLY EXPOSED TO ANTENNA RADIATION, SUCH AS IN A COMPOSITE AIRCRAFT, A MINIMUM SEPARATION OF 1.97 FT (60 CM) IS GENERALLY REQUIRED BETWEEN ANY PART OF THE ANTENNA AND ANY LOCATION WHERE A PERSON MAY BE PERMANENTLY SEATED IN THE AIRCRAFT. LESSER SEPARATION IS ACCEPTABLE IN AN AIRCRAFT WHERE METAL SKIN SHIELDS THE OCCUPANTS FROM THE ANTENNA.

n KTR 2280 Preliminary H 08/17/06

This Page Intentionally Left Blank

n KTR 2280 Preliminary H 08/17/06

SECTION 2

INSTALLATION

2.1 GENERAL INFORMATION

This section contains general suggestions and information to consider before installation of the KXP 2290. Close adherence to these suggestions will assure optimum performance from the equipment.

NOTE: The conditions and test required for the TSO/ETSO and MOPS approval of this

article are minimum performance standards. It is the responsibility of those installing this article either on or with a specified type or class of aircraft to determine that the aircraft installation conditions are within the TSO/ETSO and MOPS standards. These articles must have separate approval for installation in an aircraft. Any features in this equipment outside the requirements of this applicable TSO/ETSO and MOPS must be evaluated and approved as part of the installation approval. The article may be installed only if further evaluation by the applicant confirms that the installation is acceptable and is approved by the Administrator.

2.2 UNPACKING AND INSPECTING EQUIPMENT

Exercise extreme care when unpacking the equipment. Make a visual inspection of the unit for evidence of damage during shipment. If a claim for damage is to be made, save the shipping container to substantiate the claim. The claim should be promptly filed with the transportation company. It would be advisable to retain the container and packing material after all equipment has been removed, in the event that equipment storage or reshipment should become necessary.

2.3 EQUIPMENT INSTALLATION

2.3.1 AVIONICS COOLING REQUIREMENTS

The unit is cooled by a fan internal to the unit and one attached to the rear rack assembly plate, the latter being a part of the installation (see FIGURE 2-3 KTR 2280

INSTALLATION DRAWING). During installation, do not block any holes in the unit

cover(s) which would restrict air flow.

2.3.2 EQUIPMENT LOCATION

The following paragraphs contain information pertaining to the initial installation of the KTR 2280 MMDR, including instructions concerning the location and mounting of the supporting antenna(s).

+ 51 hidden pages