Honeywell BENDIX/KING KLN 90B Installation Manual Download | Manualshive

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BENDIX/KING

KLN 90B

Page A-8

10521I05.TDC

Rev 5, April/2003

hhhh

IC designator in case of RAM failure

iiii

IC designator in case of EPROM failure

jjjj

IC designator in case of NV RAM failure

Flight Plan Data

Item designator, sequence number, waypoint identifier, latitude/ longitude, and magnetic variation
of each waypoint defined in the active flight plan are transmitted with the following format: No in-
formation shall be transmitted for waypoints beyond a fence in a flight plan when the active way-
point is before the fence. Likewise, no information shall be transmitted for waypoints after the be-
ginning of a DME arc that is part of a procedure if the active waypoint is before the last waypoint
on the arc. No information shall be transmitted for waypoints prior to the last waypoint on the DME
arc if the active waypoint is after the arc.

Item Designator

wdd w = ’w’

dd = 01 to 99

NOTE

A maximum of 32 waypoints will be transmitted.

Sequence Number

Byte

1

Bit

76543210

xlannnnn

x

= undefined

nnnnn = Sequential waypoint number, Unsigned binary

a

= 1 if waypoint is active

l

= 1 if last waypoint of flight plan

Waypoint Identifier

Byte

2

3

4

5

6

Bit

76543210 76543210 76543210 76543210 76543210

aaaaaaaa aaaaaaaa aaaaaaaa aaaaaaaa aaaaaaaa

aaaaaaaa = ASCII characters of five-character identifier

NOTE

A value of 7FH in byte 2 indicates that the waypoint

identifier is unknown and bytes 2 through 6 should

be ignored.

Latitude/Longitude

Latitude and longitude of waypoint. Packed, unsigned binary values for degrees, minutes, and
hundredths of minutes.

Byte

7

8

9

Bit

76543210

76543210

76543210

sddddddd

xxmmmmmm xhhhhhhh

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Summary of Contents for BENDIX/KING KLN 90B

Page 1: ...INSTALLATION MANUAL KLN 90B GPS RNAV MANUAL NUMBER 006 10521 0005 REVISION 5 April 2003 ...

Page 2: ...eywell International Inc Reproduction 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 ...

Page 3: ...1 3 3 UNIT TECHNICAL CHARACTERISTICS 1 5 1 4 UNITS AND ACCESSORIES SUPPLIED 1 10 1 4 1 KLN 90B GPS RECEIVER 1 10 1 4 2 GPS ANTENNA 1 11 1 4 3 KLN 90 90B INSTALLATION KITS 1 11 1 4 4 KA 91 92 INSTALLATION KIT 1 12 1 4 5 DATABASE 1 12 1 5 ACCESSORIES REQUIRED BUT NOT SUPPLIED 1 13 1 6 OPTIONAL ACCESSORIES 1 13 1 7 LICENSE REQUIREMENTS 1 19 1 8 RECOMMENDATIONS FOR IFR APPROVAL 1 19 1 9 INSTRUCTIONS F...

Page 4: ...n 2 3 2 3 6 2 Functional Pinout Descriptions 2 4 2 4 POST INSTALLATION CHECK OUT INFORMATION 2 65 2 4 1 KLN 90B RESOLVER CALIBRATION METHOD 2 65 2 4 2 POST INSTALLATION CHECKOUT PROCEDURE 2 65 2 4 3 INSTALLATION CHECK OUT 2 66 2 4 4 INTEGRATED INSTALLATION CHECK OUT 2 67 2 4 4 1 All Installations 2 67 2 4 4 2 EFIS or CDI HSI Interface 2 67 2 4 4 3 Radar Graphics Interface 2 68 2 4 4 4 Air Data Int...

Page 5: ... COAX CONNECTOR ASSEMBLY 0 to 80 ft 0 to 100 ft 2 31 2 13 KA 33 P N 071 4037 00 01 FINAL ASSEMBLY 2 33 2 14 KA 33 P N 071 4037 00 01 INSTALLATION DRAWING 2 35 2 15 CUTLER HAMMER SWITCH ANNUNCIATOR UNIT INSTALLATION DRAWING 2 37 2 16 CUTLER HAMMER SWITCH ANNUNCIATOR UNIT INTERNAL SCHEMATIC 2 39 2 17 KLN 90B INTERCONNECTION DRAWING Page 1 of 10 2 43 2 17 KLN 90B INTERCONNECTION DRAWING Page 2 of 10 ...

Page 6: ...IX A RS 232 FORMAT DEFINITIONS APPENDIX B KLN 90B SUPPLEMENTAL PROCEDURES MANUAL KLN 90B AIRPLANE FLIGHT MANUAL SUPPLEMENT KLN 90B SUPPLEMENTAL TYPE CERTIFICATE APPENDIX C GPS FAULT ERROR CODES DATABASE LOADER MESSAGES TSO APPENDIX ENVIRONMENTAL QUALIFICATION FORMS ...

Page 7: ...nformation to determine crosstrack error distance to way point ground speed track angle time to waypoint bearing to waypoint and advisory VNAV guid ance The internal data base of the KLN 90B contains information concerning airports VORs NDBs intersections and outer markers throughout the world Waypoints are stored in the data base by their ICAO identifiers The ICAO identifiers are in most cases ta...

Page 8: ...Inputs The following labels are received by the KLN 90B on the Air Data 429 receiver inputs Pins 8 and 9 of P901 TABLE 3 3 Air Data 429 Receiver Inputs LABEL OCTAL DESCRIPTION 100 SELECTED COURSE 306 NAV WPT APT LATITUDE 307 NAV WPT APT LONGITUDE 314 OR 320 TRUE HEADING MAGNETIC HEADING LABEL OCTAL DESCRIPTION 306 NAV WPT APT LATITUDE 307 NAV WPT APT LONGITUDE LABEL OCTAL DESCRIPTION 203 ALTITUDE ...

Page 9: ...4 DATA RECORD HEADER 075 ACTIVE WAYPOINT FROM TO DATA 100 SELECTED COURSE 1 113 MESSAGE CHECKSUM 114 DESIRED TRACK TRUE 115 WAYPOINT BEARING TRUE 116 CROSS TRACK DISTANCE 121 HORIZONTAL COMMAND 147 MAGNETIC VARIATION 150 GREENWICH MEAN TIME 251 DISTANCE TO GO 252 TIME TO GO 261 GPS DISCRETE WORD 275 LONG RANGE NAV STATUS 300 STATION MAGNETIC VARIATION TYPE AND CLASS 303 MESSAGE LENGTH TYPE NUMBER ...

Page 10: ...ON LATITUDE 311 PRESENT POSITION LONGITUDE 312 GROUND SPEED 313 TRACK ANGLE TRUE 314 TRUE HEADING 315 WIND SPEED 316 WIND ANGLE TRUE 321 DRIFT ANGLE 326 LATERAL DEVIATION SCALE FACTOR 351 DISTANCE TO DESTINATION VIA FLIGHT PLAN 352 TIME TO DESTINATION VIA FLIGHT PLAN 371 SPECIFIC EQUIPMENT IDENT 377 EQUIPMENT HEX ID CODE ...

Page 11: ... Kg Mounting Panel mounted with Honeywell supplied mounting rack Cooling Requirements 4 CFM cubic feet per minute provided by blower motor such as KA 33 or equivalent OPERATIONAL CHARACTERISTICS Temperature Range 40 C to 70 C Altitude Range Up to 50 000 FT Power Inputs 11 to 33 VDC at 2 5 A MAX 40 C to 70 C Panel Lighting Current Requirements 28 VDC Lighting 286 mA max 14 VDC Lighting 572 mA max 5...

Page 12: ...later as a select input LEG OBS CONTROL This pin is used as a mode programming pin on power up and later as a control input DATA LOADER IN The Data Loader RS 232 input is designed to communi cate with the dataloader RS 232 IN The RS 232 input is designed to communicate with devic es i e air data and fuel flow sensors via RS 232 format refer to Appendix A ALT ALERT ENABLED Open or tied to A C Power...

Page 13: ...s Output drive range 300 mV 150 mV full scale 30 mV per nautical mile Full scale 5 nautical mile 150 mV per nautical mile Full scale 1 nautical mile 500 mV per nautical mile Full scale 3 nautical mile Voltage at pin 22 is rela tive to voltage at pin 25 The CDI output can manually be selected to the sensitivity of one of the three sensitive modes listed below Enroute 5 1 or 3 nautical mile scale fa...

Page 14: ...S 232 output is designed to communicate with an IBM compatible personal computer ALT ALERT HIGH Inactive LOW Active can sink up to 250 mA This pin also functions as an input refer to section 2 3 6 2 X for details ALT ALERT AU DIO This output is active whenever ALT ALERT is active Signal is 1 KHz 3 5 V rms max into 500 W TSO Compliance SEE TSO APPENDIX Physical Dimensions Width 2 90 in 7 37 cm Heig...

Page 15: ...rformance standards The article may be installed only if further evaluation by the applicant documents an acceptable installation and is ap proved by the Administrator TSO Compliance SEE TSO APPENDIX Physical Dimensions Width 2 70 in 6 86 cm Height 0 70 in 1 78 cm Length 4 30 in 10 92 cm Weight 0 27 lbs 0 12 Kg Airspeed Rating 600 Kts TAS Output Impedance 50 Ohms nominal DC Voltage 5 Volts 0 5 Vol...

Page 16: ...ing the JAA AMJ 20X2 requirements PART NUMBER 14 28V LAMP 5V LAMP NIGHT VISION GOGGLE BLACK BEZEL GREY BEZEL BRNAV CAPABLE 1 UPGRADED KLN 90B s ARINC 734A CAPABLE 2 066 04031 1121 X X 066 04031 1221 X X 066 04031 1321 X X 066 04031 1421 X X 066 04031 1521 X X X 066 04031 1621 X X X 066 04031 2121 X X X 066 04031 2221 X X X 066 04031 2321 X X X 066 04031 2421 X X X 066 04031 1122 X X X 066 04031 12...

Page 17: ... Table 3 16 KLN 90B Installation Kits P N DESCRIPTION UM 0000 VENDOR NAME P N 050 03096 0000 KLN90 INSTALL CRIMP X 030 00101 0002 PANEL MOUNT PLUG J902 EA 1 TED Mfg 9 30 10 030 01157 0011 SOCKET CRMP 20G EA 50 Positronics FC6020D 14 030 01176 0000 CONN SUB D HSG 50S J901 EA 1 Positronics RD50F00000 782 0 030 01428 0006 HOOD W SPCL LCK 50P EA 1 Positronics D50000 GVLD 033 00230 0000 DATA LOADER JAC...

Page 18: ...idge is available for three separate geographic areas North American Database 071 01523 0302 Atlantic International Database 071 01523 0304 Pacific International Database 071 01523 0305 P N DESCRIPTION UM 0000 VENDOR NAME P N 050 03195 0000 KA91 INSTALL X 030 00134 0001 RIGHT ANGLE CONN COAX EA 1 TED MFG 5 30 102 047 10130 0002 BACKPLATE ANTENNA EA 1 089 06908 0012 SCREW AIRCRAFT EA 4 187 01807 00...

Page 19: ... 01791 XXXX NOTE The DME distance display is not compatible with the KLN 90B KPI 553A used with the KNR 665 Digital Gold Crown is not compatible 4 KPI 553B P N 066 3069 XX Horizontal Situation Indicator and installation kit P N 050 02167 XXXX 5 KI 525A P N 066 3046 XX Horizontal Situation Indicator and installation kit P N 050 01344 XXXX Refer to section 2 4 1 KLN 90B OBS Resolver Calibration Proc...

Page 20: ... or Commander 2000K from Lone Star Avion ics phone 817 548 7768 Laptop computers used to load the data base require the following 1 IBM compatibility 2 An available Com 1 or Com 2 serial port 3 A 3 5 high density diskette drive NOTE Not all laptops conform to the above requirements If there is uncertainty relating to this contact Honeywell Product Services by telephoning 913 782 0600 C Annunciator...

Page 21: ...ltg NAV GPS Sw Ann 031 00785 0712 or 031 00763 0712 WPT MSG Ann 031 00785 0762 or 031 00763 0762 0719 KLN 90 B or KLX 135 Ann Set 5 V ltg NAV GPS Sw Ann 031 00785 0713 or 031 00763 0713 WPT MSG Ann 031 00785 0506 or 031 00763 00506 0720 KLN 90B Approach Set for CDI or Elect Mech HSI Installations The following switch annunciators are being offered for CDI or HSI switching GPS CRS and APR switching...

Page 22: ...031 00785 0780 or 031 00785 0765 GPS APR ARM ACT Sw Ann 031 00785 0768 KLN 90A Upgrade to KLN90B Approach Set If a KLN 90A is upgraded to a KLN 90B the additional GPS CRS and GPS APR switch annunci ators are needed or KLN 90B with EFIS Approach Set Most EFIS systems will provide NAV GPS switching and WPT MSG annunciation but still require external GPS CRS and GPS APR switch annunciators NOTE The G...

Page 23: ...red for the switching of the outputs This Switch Annunciator is available in 5 V 14 V or 28 V versions as shown below LIGHTING Honeywell P N Honeywell P N 28 V 031 00763 0711 031 00785 0711 5 V 031 00763 0713 031 00785 0713 14 V 031 00763 0712 031 00785 0712 Eaton Series 584 Eaton Series 582 WPT MSG Remote Annunciators The KLN 90B contains two outputs 1 Waypoint Alert WPT and 2 Message MSG Annunci...

Page 24: ...LEG mode the flightplan legs will automatically sequence as determined by present position In OBS mode the active waypoint and inbound or outbound course will be manually selected The Remote OBS LEG Switch Annun ciator is recommended for non precision approaches to reduce pilot workload The selection of OBS or LEG may be accomplished in either of two methods Method 1 Select the Mode Page by rotati...

Page 25: ...OR IFR APPROVAL 1 Aircraft Logbook Entry 2 Aircraft Installation Requirements The following interface functions were not required for a VFR KLN 90 but are required for an IFR d KLN 90B installation TSO d Antenna The antenna must be a TSO d KA 91 P N 071 01545 0200 or KA 92 P N 071 01553 0200 If the P N of the KA 91 is not available it may be identified by the serial number as the TSO d antennas ha...

Page 26: ...lay a remote annunciator is also required in the pilots panel unless it is accomplished in an HSI CDI or EFIS display GPS CRS OBS LEG Switch Annunciator The KLN 90B may operate in either of two modes LEG or OBS In LEG mode the flightplan legs will automatically sequence as determined by present position In OBS mode the active waypoint and inbound or outbound course will be manually selected The Re...

Page 27: ...f the STC approval 4 Pilot s Guide The KLN 90B pilots guide must be placed in the aircraft in a location that is accessible to the pilot The pilot s guide is P N 006 08773 0000 and the abbreviated pilot s guide is P N 006 08774 0000 1 9 INSTRUCTIONS FOR CONTINUED AIR WORTHINESS The instructions for continued air worthiness given in the TC or STC approvals for this product supplements or supercedes...

Page 28: ...BENDIX KING KLN 90B Page 1 22 10521I05 TDC Rev 5 April 2003 ...

Page 29: ...ed While modern day individual circuit designs consume much less electrical energy watts per cubic inch dissipated within the avionics unit remains much the same due to the high density packaging techniques utilized Consequently the importance of providing cooling to the avionics stack is still with us today While each individual unit may or may not require forced air cooling the combined heat loa...

Page 30: ... 2 12 for both TNC and BMA for the 0 to 80 feet and 0 to 100 feet categories NOTE KA 91 92 nominal gain and noise figures are 26 5 dB and 2 3 dB respectively With 0 050 ice on radome gain will not decrease by more than 2 0 dB when viewing a satellite from 30 above the horizon to ze nith as compared to a no ice condition 100 to 165 ft Contact TED ECS or PIC for complete cable connector assembly NOT...

Page 31: ...e antenna itself be well bonded to the aircraft G When installing the KLN 90B antenna do not exceed 25 inch lbs of torque on the antenna mounting screws H Apply white RTV sealant around base of installed antenna Fill mounting screw holes with RTV sealant P N 016 01129 0000 or equivalent 2 3 6 ELECTRICAL INSTALLATION 2 3 6 1 General Information The KLN 90B will operate with an input voltage from 11...

Page 32: ... turned on This pin is used only for dual long range navigation installations when a KLN 90B is interfaced through ARINC 429 as system 2 D Pins 4 and 5 EFIS 429 Receiver Inputs The KLN 90B receives information from the Electronic Flight Instrument System EFIS or KA 90 display adapter in GAMA 429 format on this input bus This bus should be left open if no EFIS or adapter is connected to the KLN 90B...

Page 33: ...IVE Pin 16 is the Approach Active annunciator output This output is tied to a remote annunciator lamp When the line is pulled low the annunciator lamp will illumi nate The annunciator will be on whenever the unit is in the approach mode For more complete information refer the KLN 90B Pilots Guide P N 006 08773 0000 L Pin 17 APPROACH ARM Pin 17 is the Approach Arm annunciator output This output is ...

Page 34: ...rawing for the correct method of connecting these pins and connecting to the aircraft dimmer bus S Pin 30 Approach Arm Select Pin 30 is used as a mode programming pin on power up and later as a select input If the installation is not certified for approach the external switch annun ciator is not required This function can be eliminated by connecting the AP PROACH ARM SELECT pin 30 to the APPROACH ...

Page 35: ...mpling at powerup If pin 38 is grounded it is configured as an input All pilot selectable altitude alert functions of the KLN 90B will be disabled This option should be considered if another altitude preselector is already installed in the air craft If pin 38 is open or connected to drive an alerting device it is configured as an output Altitude alert functions will be selectable through the KLN 9...

Page 36: ...BENDIX KING KLN 90B Page 2 8 10521I05 TDC Rev 5 April 2003 ...

Page 37: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 9 FIGURE 2 1 KLN 90B CONNECTOR PIN FUNCTIONS ...

Page 38: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 11 FIGURE 2 2 KLN 90B CRIMPING AND INSERTION EXTRACTION TOOLS ...

Page 39: ...BENDIX KING KLN 90B Page 2 12 10521I05 TDC Rev 5 April 2003 ...

Page 40: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 13 FIGURE 2 3 KLN 90B INSTALLATION DRAWING DWG NO 155 05818 0000 R AB ...

Page 41: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 15 FIGURE 2 4 KA 91 OUTLINE DWG NO 071 01545 0200 R 4 ...

Page 42: ...BENDIX KING KLN 90B Page 2 16 10521I05 TDC Rev 5 April 2003 ...

Page 43: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 17 FIGURE 2 5 KA 91 INSTALLATION DRAWING DWG NO 155 05999 0000 R 5 ...

Page 44: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 19 FIGURE 2 6 KA 91 BACKPLATE OUTLINE DWG NO 047 10130 0000 0002 R 2 ...

Page 45: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 21 FIGURE 2 7 KA 92 OUTLINE DRAWING DWG NO 071 01553 0200 R AB ...

Page 46: ...BENDIX KING KLN 90B Page 2 22 10521I05 TDC Rev 5 April 2003 ...

Page 47: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 23 FIGURE 2 8 KA 92 INSTALLATION DRAWING DWG NO 155 06019 0000 R 2 ...

Page 48: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 25 FIGURE 2 9 KA 92 BACKPLATE OUTLINE DWG NO 047 10735 0000 0002 R 1 ...

Page 49: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 27 FIGURE 2 10 KA 91 92 TNC ANTENNA COAX CONNECTOR ASSEMBLY RG142B U OR RG400 0 TO 40 FT P N 030 00134 0000 R 3 030 00134 0001 R 0 ...

Page 50: ...BENDIX KING KLN 90B Page 2 28 10521I05 TDC Rev 5 April 2003 ...

Page 51: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 29 FIGURE 2 11 KA 91 92 BMA ANTENNA COAX CONNECTOR ASSEMBLY RG142 B U OR RG400 0 TO 40 FT DWG NO 030 00101 0002 R 9 ...

Page 52: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 31 FIGURE 2 12 KA 91 92 TNC ANTENNA COAX CONNECTOR ASSEMBLY 0 TO 80 FT 0 TO 100 FT FOR CABLE P N S 024 00071 0000 R 0 024 00072 0000 R 0 ...

Page 53: ...BENDIX KING KLN 90B Page 2 32 10521I05 TDC Rev 5 April 2003 ...

Page 54: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 33 FIGURE 2 13 KA 33 P N 071 4037 00 01 FINAL ASSEMBLY DWG NO 300 03256 0000 R AA ...

Page 55: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 35 FIGURE 2 14 KA 33 P N 071 4037 00 01 OUTLINE AND MOUNTING DWG NO 155 05574 0000 R 5 ...

Page 56: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 37 FIGURE 2 15 CUTLER HAMMER SWITCH ANNUNCIATOR MOUNTING ...

Page 57: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 39 FIGURE 2 16 CUTLER HAMMER SWITCH ANNUNCIATOR INTERNAL SCHEMATIC SHEET 1 OF 2 ...

Page 58: ...BENDIX KING KLN 90B Page 2 40 10521I05 TDC Rev 5 April 2003 ...

Page 59: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 41 FIGURE 2 16 CUTLER HAMMER SWITCH ANNUNCIATOR INTERNAL SCHEMATIC SHEET 2 OF 2 ...

Page 60: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 43 FIGURE 2 17 KLN 90B INTERCONNECT DRAWING DWG NO 155 06021 0000 R AC SHEET 1 OF 10 ...

Page 61: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 45 FIGURE 2 17 KLN 90B INTERCONNECT DRAWING DWG NO 155 06021 0000 R AC SHEET 2 OF 10 ...

Page 62: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 47 FIGURE 2 17 KLN 90B INTERCONNECT DRAWING DWG NO 155 06021 0000 R AC SHEET 3 OF 10 ...

Page 63: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 49 FIGURE 2 17 KLN 90B INTERCONNECT DRAWING DWG NO 155 06021 0000 R AC SHEET 4 OF 10 ...

Page 64: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 51 FIGURE 2 17 KLN 90B INTERCONNECT DRAWING DWG NO 155 06021 0000 R AC SHEET 5 OF 10 ...

Page 65: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 53 FIGURE 2 17 KLN 90B INTERCONNECT DRAWING DWG NO 155 06021 0000 R AC SHEET 6 OF 10 ...

Page 66: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 55 FIGURE 2 17 KLN 90B INTERCONNECT DRAWING DWG NO 155 06021 0000 R AC SHEET 7 OF 10 ...

Page 67: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 57 FIGURE 2 17 KLN 90B INTERCONNECT DRAWING DWG NO 155 06021 0000 R AC SHEET 8 OF 10 ...

Page 68: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 59 FIGURE 2 17 KLN 90B INTERCONNECT DRAWING DWG NO 155 06021 0000 R AC SHEET 9 OF 10 ...

Page 69: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 61 FIGURE 2 17 KLN 90B INTERCONNECT DRAWING DWG NO 155 06021 0000 R AC SHEET 10 OF 10 ...

Page 70: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page 2 63 FIGURE 2 18 KLN 90B DATALOADER PC INTERFACE DRAWING ...

Page 71: ...en If the OBS angle on the KLN 90B agrees with the selected course on the external indicator then no calibration is necessary 10 If the two values do not agree then the KLN 90B will need to be calibrated This is done by pressing the left cursor button and adjusting the value next to OBS CAL A value of 100 is the default setting and represents no correction It is possible to make adjustments of up ...

Page 72: ...on for the installation location accurate to within 60 nautical miles Display the Set 2 Page Verify that the date and time are correct to within 10 minutes and update if necessary If the date is off by a large amount and the date cannot be set back to the correct year make the receiver blind to the satellites by disconnecting the coax setting the date while on the bench with no antenna covering th...

Page 73: ...put Output signals that can be connected to the KLN 90B It should be clearly determined which of the signals are in tended to be used in any given installation and then only the paragraphs pertaining to those signals should be performed 2 4 4 1 All Installations Perform all steps defined in Paragraph 2 4 3 and leave the system energized with a valid GPS signal being received 2 4 4 2 EFIS or CDI HS...

Page 74: ...nd that proper baro has been entered Verify that there is no interference between the KLN 90B transponder and any other loads on the encoding altimeter output Remove power from each of the loads on the encoder to verify that the remaining equipment still performs properly If interference exists one or more of the units are not diode isolated and isolation diodes will need to be added to the aircra...

Page 75: ...e 2 18 Set the KLN 90B to the Set 0 page Put the 1 diskette into the PC Cycle the power of the PC and follow the menu driven instructions NOTE The KLN 90B database may be updated using a PC with the KLN 90B mounted in an aircraft or via a KCC 90 ref figure 2 18 2 4 4 12 ALT ALERT ALT ALERT AUDIO Upon approval of the self test page five 5 beeps will be issued on the audio output and five 5 sonalert...

Page 76: ... mode However the KLN 90B will test the roll steering while on the system test page and activate all the outputs The Roll Steering will be valid and active until you ap prove the page While on this page you can engage the flight director and observe the com mand bars change from 0 degrees to 5 degrees right and back to 0 degrees This will validate the drivers and wiring so you will feel confident ...

Page 77: ...03 10521I05 TDC Page 3 1 SECTION III OPERATION 3 1 GENERAL INFORMATION For an explanation of the operating controls of the KLN 90B GPS RNAV refer to the KLN 90B pilots guide P N 006 08773 0000 or the aircraft s flight manual supplement ...

Page 78: ...BENDIX KING KLN 90B Page 3 2 10521I05 TDC Rev 5 April 2003 ...

Page 79: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page A 1 APPENDIX A RS 232 FORMAT DEFINITIONS ...

Page 80: ...BENDIX KING KLN 90B Page A 2 10521I05 TDC Rev 5 April 2003 THIS PAGE RESERVED ...

Page 81: ...ormal operations the RS 232 input will be connected to a fuel sensor and or air data In installations where the RS 232 input is not connected to a fuel sensor and air data it will be looped back to RS 232 output However in test mode the RS 232 input and output can be connected to a PC to read or write from or to a memory location or port The RS 232 output provides navigation and self test data in ...

Page 82: ... self test data navigation data RS 232 I O Fuel Sensor Air Data ELT and or moving map and or PC Fuel data and air data navigation data self test data RS 232 I O Fuel Sensor Air Data Fuel data and air data navigation data self test data RS 232 I O Fuel Sensor Fuel data RS 232 PC memory port read write request memory port read write response O I ...

Page 83: ...hs of minutes B s ddd mmhh10 present longitude s sign E for east W for west ddd degrees mm minutes hh hundredths of minutes C ddd 3 track magnetic dashed if groundspeed 2KT ddd degrees D ddd 3 ground speed ddd knots E ddddd 5 distance to active waypoint ddddd nm 10 G sdddd 5 cross track error s sign R for aircraft position right of course L for aircraft position left of course dddd nm 100 I dddd 4...

Page 84: ...ired track bearing to active waypoint and magnetic variation in leg and OBS modes The following definitions are used TK angle of the course that the aircraft is flying relative to true north DTK angle of the course line at the point nearest the present position relative to true north RAD true radial from the active waypoint to the present position angle is measured at the waypoint MSC angle of the...

Page 85: ...32 Data a5 RS 232 Data Error a6 RS 232 Output Error a7 1 b0 Data Loader Error b1 ARINC 429 Output Fail b2 EFIS RCVR Failure b3 RDRG RCVR Failure b4 Air Data Fail b5 WPT Annunciator OCD FAIL b6 MSG Annunciator OCD FAIL b7 1 c0 Approach ACTV OCD FAIL c1 Approach ARM OCD FAIL c2 NAV SUPER Flag Failure c3 unused c4 unused c5 unused c6 unused c7 1 d0 unused d1 unused d2 unused d3 unused d4 unused d5 un...

Page 86: ... the arc No information shall be transmitted for waypoints prior to the last waypoint on the DME arc if the active waypoint is after the arc Item Designator wdd w w dd 01 to 99 NOTE A maximum of 32 waypoints will be transmitted Sequence Number Byte 1 Bit 76543210 xlannnnn x undefined nnnnn Sequential waypoint number Unsigned binary a 1 if waypoint is active l 1 if last waypoint of flight plan Wayp...

Page 87: ...st longitude s 1 West longitude x Undefined dddddddd Longitude degrees mmmmmm Longitude minutes hhhhhhh Longitude hundredths of minutes Magnetic Variation Byte 14 15 Bit 76543210 76543210 nnnnnnnn nnnnnnnn nnnnnnnnnnnnnnnn Magnetic variation at waypoint Two s complement binary in sixteenths of degrees Easterly variation is positive NOTE A value of 7FH in byte 14 indicates that magnetic variation i...

Page 88: ...g Checksum Break each decimal value into its BCD representation Using BCD arithmetic sum the 4 BCD val ues and convert the low order BCD digit to an ASCII coded numeric digit Example The checksum for a value of 432 would be 9 39H 8 11 Fuel Flow Rate units hour ASCII coded decimal format as for Fuel Remaining 12 Fuel Flow Rate Checksum Sum of fuel flow bytes computed as for Fuel Remaining 13 ETX AS...

Page 89: ...ytes computed as for Total Fuel Remaining 31 36 Total Fuel Used ASCII coded decimal format as for Total Fuel Remaining 37 Total Fuel Used Checksum Sum of Total Fuel Used bytes computed as for Total Fuel Remaining 38 43 Engine One Fuel Used ASCII coded decimal format as for Total Fuel Remaining 44 Engine One Fuel Used Checksum Sum of Left Engine Fuel Used bytes computed as for Total Fuel Remaining ...

Page 90: ...I coded decimal format with a sign character Example 1 A PALT of 34500 feet would be sent as 00543 30H 30H 35H 34 33H 2BH 70 pressure altitude checksum Sum for PALT bytes excluding the sign character Example The sum for 850 feet would be 3 33H 71 76 density altitude DALT feet ASCII coded decimal format with a sign character as for PALT 77 density altitude checksum Sum for DALT bytes excluding the ...

Page 91: ...D A 121 byte ASCII string shall be transmitted Bytes 1 through 107 shall be the same as Format C except that bytes 3 through 9 shall be filled with asterisks if total fuel remaining is not available and consequently must be entered through the KLN 90B The remaining bytes shall be defined as follows If valid data for a particular data item is received both on this bus and on an ARINC 429 input the ...

Page 92: ...BENDIX KING KLN 90B Page A 14 10521I05 TDC Rev 5 April 2003 ...

Page 93: ...X KING KLN 90B Rev 5 April 2003 10521I05 TDC Page B 1 APPENDIX B Includes the following KLN 90B SUPPLEMENTAL PROCEDURES MANUAL KLN 90B AIRPLANE FLIGHT MANUAL SUPPLEMENT KLN 90B SUPPLEMENTAL TYPE CERTIFICATE ...

Page 94: ...BENDIX KING KLN 90B Page B 2 10521I05 TDC Rev 5 April 2003 THIS PAGE RESERVED ...

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Page 133: ...BENDIX KING KLN 90B Rev 5 April 2003 10521I05 TDC Page C 1 APPENDIX C GPS FAULT ERROR CODES AND MESSAGES ...

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Page 135: ...800 and an 0008 are both detected they will be displayed as an 0808 So if you see an error code displayed that does not exist in the table check to see if it is a combination of 2 or more error codes GPS Rec error Codes Definition Suggested Action RCVR Hardware Error 0002 ROM Failure The ROM failed self test Bad ROM Read Only Memory Return for service RCVR Hardware Error 0004 RAM Failure The RAM f...

Page 136: ...e GPS Substitute the GPS unit RCVR Hardware Error 0100 BBP Timeout The 1 mS baseband pro cessing timer failed self test It could be one of the following in the order of prob ability 1 The 5 volt supply to the antenna could be shorted out in the coax This disables the oscillator in the GPS 2 The flex cable between the Receiver Board and Main Board may have come out of the socket in the GPS 3 Bad TC...

Page 137: ...r Microprocessor on the Receiver Board RCVR Hardware Error 2000 BBP Underflow The baseband process ing loop detected an error in the 1 mS pro cessing loop It could be one of the following in the order of prob ability 1 The flex cable between the Receiver Board and Main Board may have come out of the socket in the GPS 2 Bad TCXO MMIC or ASIC on the Receiver Board RCVR Hardware Error 8000 BBP Overfl...

Page 138: ...LN 90B 2 EEPROM Fail ure Icxxxx Indicates a detected EEPROM failure in ei ther the GPS unit or the database cartridge If the xxxx field is 1xxx indicates a failure in the processor in the KLN 90 A B GPS unit 03xx 04xx indicates a failure in the processor in the KLN 90 A B database cartridge NAV Superflag Failure Indicates an internal test of the NAV Super flag output failed When the flag is suppos...

Page 139: ... and connection for problems 2 Verify that 5 volts is present at the antenna end of the coax 3 Substitute the receiver to check for sensitivity 4 Substitute the antenna to check for sensitivity No RS 232 Data There is no RS 232 data at the RS 232 input port The Air Data Fuel Flow source is not providing RS 232 data to the GPS If no source of RS 232 is interfaced the receiver input must be jumpered...

Page 140: ...error __ These are error codes that are detected in the GPS receiver Refer to the GPS Fault Error Code table RAIM not avail able Approach mode inhibited Predict RAIM on OTH 3 or STA 5 This is a calculated pre diction of RAIM avail ability The message appears when integrity monitoring RAIM is predicted to not be available at either the FAF or MAP The GPS will not allow the unit to go into APR ACTV ...

Page 141: ...iring of the data loader cable and aircraft harness Check sum error Indicates an error on the database diskettes Try an old cycle If the old cycle diskette works contact AlliedSignal Navigation Services for a re placement diskette Disk compatibility problem This indicates a prob lem with the diskette Verify that Windows is not running and that you booted the computer from the database diskette Try...

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