Honeywell BENDIX/KING KLN 94- Manuals

Honeywell BENDIX/KING KLN 94– User Manual in PDF format online.

Manuals:

User Manual

User Manual Honeywell BENDIX/KING KLN 94

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Summary

Page 2 - WARNING; COPYRIGHT NOTICE

WARNING Prior to export of this document, review for export license requirement is needed. COPYRIGHT NOTICE 2000, 2003 Honeywell International, Inc. Reproduction of this publication or any portion thereof by any means without the expressed written permission of Honeywell is prohibited. For further i...

Page 6 - THIS PAGE IS RESERVED

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL RH-4 THIS PAGE IS RESERVED

Page 11 - EQUIPMENT DESCRIPTION

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 1-1 SECTION I GENERAL INFORMATION 1.1 INTRODUCTION This manual contains information relative to the physical, mechanical, and electrical characteristics of the BENDIX/KING KLN 94 Global Positioning System (GPS) Receiver. General installation procedures are...

Page 22 - NOTE

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 1-12 NAV/GPS Switch/Annunciator Installations where the outputs from KLN 94 and an existing navigation system are switched between a common indicator or HSI may require some type of annunciation. A NAV/GPS switch/annunciator is available that provides both...

Page 23 - Section II

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 1-13 1.6.3 NAV/GPS Switching Installations in which the outputs from a KLN 94 and an existing navigation system are being switched onto a common indicator will require some remote relay switching that is controlled by the NAV/GPS switch/annunciator. 1.6.4 ...

Page 25 - Appendix D

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-1 SECTION II INSTALLATION 2.1 GENERAL INFORMATION This section contains general suggestions and information to consider before installation of the KLN 94 GPS RNAV. Close adherence to these suggestions will assure optimum performance from the equipment. N...

Page 29 - Pin 5 is a spare RS 232 input.

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-5 2.3.6.2 Functional Pinout Descriptions This section gives a brief description of some of the inputs and outputs of the KLN 89/89B. It is provided so the installer can determine what specific wiring needs to be done to the aircraft in which the unit is ...

Page 38 - FIGURE 2-4 CRIMPING AND INSERTION/EXTRACTION TOOLS

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-14 FIGURE 2-4 CRIMPING AND INSERTION/EXTRACTION TOOLS

Page 41 - THIS PAGE IS RESERVED.

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-18 THIS PAGE IS RESERVED.

Page 42 - FIGURE 2-7 KA 91 INSTALLATION DRAWING

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-19 FIGURE 2-7 KA 91 INSTALLATION DRAWING Dwg. No. 155-05999-0000 Rev. 5

Page 46 - NOTES; Antennas to be bulk packaged as per good commercial practice.

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-25 NOTES 1. For best performance, electrical bond between aircraft and antenna should be less than 10 milliohms measured from TNC connector to aircraft skin. 2. Antenna to be mounted with four 8-32 x 3/4 inch long Pan Head phillips stainless steel screws...

Page 48 - FIGURE 2-10 KA 92 INSTALLATION DRAWING

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-27 FIGURE 2-10 KA 92 INSTALLATION DRAWING Dwg. No. 155-06019-0000 Rev. 2

Page 49 - FIGURE 2-11 KA 92 BACKPLATE OUTLINE

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-29 FIGURE 2-11 KA 92 BACKPLATE OUTLINE Dwg. No. 047-10735-0000 Rev. 1

Page 52 - (RG142 B/U or RG400 - 0 to 40 FEET)

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-33 FIGURE 2-13 KA91/92 BMA ANTENNA COAX/CONNECTOR ASSEMBLY (RG142 B/U or RG400 - 0 to 40 FEET)

Page 58 - FIGURE 2-18 CUTLER-HAMMER SWITCH / ANNUNCIATOR INTERNAL SCHEMATIC

B KLN 94 Rev. 4, Dec/2002 10599I04.CDL Page 2-43 FIGURE 2-18 CUTLER-HAMMER SWITCH / ANNUNCIATOR INTERNAL SCHEMATIC Sheet 1 of 2

Page 61 - FIGURE 2-19 KLN 94 SERIAL RECEIVERS & TRANSMITTERS INTERCONNECT

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-47 FIGURE 2-19 KLN 94 SERIAL RECEIVERS & TRANSMITTERS INTERCONNECT Dwg. No. 155-01732-0000 Rev. B

Page 63 - FIGURE 2-21 KLN 94 DEVIATION & FLAGS INTERCONNECT

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-51 FIGURE 2-21 KLN 94 DEVIATION & FLAGS INTERCONNECT Dwg. No. 155-01732-0002 Rev.-

Page 64 - FIGURE 2-22 KLN 94 OBS RESOLVER INTERCONNECT

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-53 FIGURE 2-22 KLN 94 OBS RESOLVER INTERCONNECT Dwg. No. 155-01732-0003 Rev.- Sheet 1 of 2

Page 65 - Sheet 2 of 2

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-55 FIGURE 2-23 KLN 94 INTERCONNECT Dwg. No. 155-01732-0003 Rev.- Sheet 2 of 2

Page 68 - FIGURE 2-26 KLN 94 PC LOADER & ANTENNA INTERCONNECT

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-61 FIGURE 2-26 KLN 94 PC LOADER & ANTENNA INTERCONNECT Dwg. No. 155-01732-0006 Rev.-

Page 69 - FIGURE 2-27 KLN 94 DATA LOADER / PC INTERFACE

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-63 FIGURE 2-27 KLN 94 DATA LOADER / PC INTERFACE

Page 70 - FIGURE 2-28 KLN 94 QUICKTUNE INTERCONNECT

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-65 FIGURE 2-28 KLN 94 QUICKTUNE INTERCONNECT Dwg. No. 155-01732-0007 Rev.-

Page 77 - POST INSTALLATION CHECKOUT PROCEDURE; is via the front panel controls.

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-73 B. Configuring the KLN 94 to operate with KFC 225 (attitude-based flight control system): 1. Select MNT 8 page.2. Push CRSR button. The cursor will appear over the second line.3. Select “Bank Angle” and push CRSR again. The screen should look like: C....

Page 79 - SW REVISION 0X0X

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-75 If the interference is from the radiating VHF COMM, an optional notch filter (i.e. the KA 198 P/N 071-01565-0000 or TED Mfg 4-70-54) will need to be installed. The recommended location for the inline filter should be as close to the VHF RT as practica...

Page 81 - Interface

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-77 2.4.4.6 Moving Map Interface If the KLN 94 is interfaced to a moving map display, verify operation by moving the aircraft out to an open location to acquire a satellite position. Enter an active flightplan or active waypoint to develop a presentation ...

Page 82 - Diskette Update; The KLN 94 database may be updated using a PC with the KLN 94 mounted; The Attitude Gyro is fully erected and stabilized.

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-78 Diskette Update Connect the laptop via the PC loader kit PN 050-03612-0000 (ref figure 2-26 ). Turn on the KLN 94 to the SET 3 page. Insert the 3.5" Database diskette into the PC. Cycle the power of the PC and follow the menu driven instructions. ...

Page 85 - TABLE 2-1 GPS RECEIVER ERROR CODES

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-81 RCVR HardwareError: 0100 BBP Timeout: The 1 mS baseband processing timer has failed self-test. It could be one of the following, in the order of probability: 1. The 5 volt supply to the antenna could be shorted out in the coax. This disables the oscil...

Page 87 - TABLE 2-2 GPS PAGE MESSAGES

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 2-83 TABLE 2-2 GPS PAGE MESSAGES GPS Page Messages Definition Suggested Action RAIM not available Cross check position This means there are not enough satellites available to compute integrity (RAIM). 1. The satellites are blocked from view by obstructions...

Page 89 - GENERAL INFORMATION

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page 3-1 SECTION III OPERATION 3.1 GENERAL INFORMATION For an explanation of the operating controls of the KLN 94 GPS RNAV refer to the KLN 94 Pilot’s Guide (P/N 006-18207-0000) or the aircraft’s flight manual supplement.

Page 101 - RS232 OUTPUT DATA ITEM DEFINITIONS

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page A-11 Data Protocol Data shall be sent in blocks having the following format: Any data which is invalid or exceeds the data format will be filled with dashes. RS232 OUTPUT DATA ITEM DEFINITIONS There are two RS232 output data item definitions, as represente...

Page 110 - FLIGHT MANUAL SUPPLEMENT PROCEDURE

B KLN 94 Rev. 4, Jan/2003 10599I04.CDL Page B-2 FLIGHT MANUAL SUPPLEMENT PROCEDURE For the installation of the KLN 94 GPS to be FAA approved for enroute and approach IFR operation, it is necessary for the installer to create a flight manual supplement that is unique for the installation and to submi...

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