Honeywell Bendix/King KRA 405B Installation Manual Download Page 22

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KRA 405B RADAR ALTIMETER INSTALLATION MANUAL

Page 1-10

006-10536-0010 Rev. 10

Oct/2005

RADAR ALTIMETER INDICATOR - Honeywell KNI 415 or KNI 416

TABLE 1-1 KNI 415/416 INDICATOR AVAILABILITY

RADAR ALTIMETER ANTENNAS (2 each)

Honeywell KA 54A, Part Number 071-1501-00 (White)

Part Number 071-01501-0100 (Black)

Gaskets are included with a new antenna. They may be ordered

separately as P/N 187-01753-0000.

NOTE:

The KA 54 Radar Altimeter Antenna is compatible with the

KRA 405B and may be used in retrofit situations. However,

this antenna is no longer available from the factory.

KRA 405B INSTALLATION KIT

P/N 050-03365-00XX which includes the following:

UNIT

PART NUMBER

FACEPLATE

PANEL LIGHTING

KNI 415

066-3031-00

BLACK

5 VOLT

KNI 415

066-3031-01

BLACK

28 VOLT

KNI 415

066-3031-02

GRAY

5 VOLT

KNI 415

066-3031-03

GRAY

28 VOLT

KNI 415

066-3031-04

BLACK

NIGHT VISION

KNI 416

066-3044-00

BLACK

5 VOLT

KNI 416

066-3044-01

BLACK

28 VOLT

KNI 416

066-3044-02

GRAY

5 VOLT

KNI 416

066-3044-03

GRAY

28 VOLT

KNI 416

066-3044-04

BLACK

NIGHT VISION

PART NUMBER

DESCRIPTION

UM -00

-01

-02

-03

VENDOR PART NUMBER

030-02077-0000

41 Pin Conn Solder

EA 1

CANNON KPT06B2041S

030-02077-0004

41 Pin Conn Crimp

EA 0

CANNON KPSE06F20-41S

057-05944-0017

TSO KIT LABEL

EA 1

N.A.

057-05944-0018

TSO KIT LABEL

EA 0

N.A.

057-05944-0019

TSO KIT LABEL

EA 0

N.A.

057-05944-0020

TSO KIT LABEL

EA 0

N.A.

071-04003-0000

Mounting Rack

EA 1

Summary of Contents for Bendix/King KRA 405B

Page 1: ...INSTALLATION MANUAL KRA 405B RADAR ALTIMETER MANUAL NUMBER 006 10536 0010 REVISION 10 OCTOBER 2005 ...

Page 2: ... 1999 2001 2003 2005 Honeywell International Inc REPRODUCTION OF THIS PUBLICATION OR ANY PORTION THEREOF BY ANY MEANS WITHOUT THE EXPRESS WRITTEN PERMISSION OF HONEYWELL IS PROHIBITED EXCEPT TO THE EXTENT REQUIRED FOR INSTALLATION OR MAINTENANCE OF THE RECIPIENT S EQUIPMENT FOR FURTHER INFORMATION CONTACT THE MANAGER TECHNICAL PUBLICATIONS HONEYWELL ONE TECHNOLOGY CENTER 23500 WEST 105th STREET OL...

Page 3: ...GHLIGHTS 006 10536 0010 Rev 10 Oct 2005 This is a full reprint of the KRA 405B Installation Manual Discard the previous manual revision in its entirety Specific changes to content are denoted by change bars Revision highlight s include the updating the environmental qualification forms to revision AF ...

Page 4: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page RH 2 006 10536 0010 Rev 10 Oct 2005 THIS PAGE IS RESERVED ...

Page 5: ...M COMPONENTS 1 9 A RADAR ALTIMETER Receiver Transmitter 1 9 B RADAR ALTIMETER INDICATOR Honeywell KNI 415 or KNI 416 1 10 C RADAR ALTIMETER ANTENNAS 2 each 1 10 D KRA 405B INSTALLATION KIT 1 10 E KNI 415 416 INDICATOR INSTALLATION KIT 1 11 F KA 54A RADAR ALTIMETER ANTENNA INSTALLATION KIT 1 11 1 5 ACCESSORIES REQUIRED BUT NOT SUPPLIED 1 11 1 6 OPTIONAL ACCESSORIES RECOMMENDED BUT NOT SUPPLIED 1 12...

Page 6: ... INSTALLATION 2 10 E IMPLEMENTING THE ANTENNA INSTALLATION 2 12 F ANTENNA CABLES 2 13 G WIRING HARNESS 2 14 H CONFIGURATION MODULE INSTALLATION 2 14 2 6 POST INSTALLATION 2 15 A POST INSTALLATION CALIBRATION 2 15 B GENERAL 2 17 C KRA 405B RADAR ALTIMETER POST INSTALLATION TEST PROCEDURE 2 17 D TEST PROCEDURE 2 20 2 7 REMOVAL AND REPLACEMENT 2 22 A KRA 405B RECEIVER TRANSMITTER 2 22 B KNI 415 416 I...

Page 7: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page TC 3 006 10536 0010 Rev 10 Oct 2005 ITEM PAGE D APPROACH 3 3 E PUSH TO TEST MODE 3 3 3 3 SELF TEST DIAGNOSTICS 3 4 TSO APPENDIX ...

Page 8: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page TC 4 006 10536 0010 Rev 10 Oct 2005 THIS PAGE IS RESERVED ...

Page 9: ...9 FIGURE 2 8 KA 54 ANTENNA OUTLINE AND MOUNTING DRAWING 2 33 FIGURE 2 9 UBC TYPE AD 43013 1 AND COMANT TYPE 01 34 04531 2 35 FIGURE 2 10 DORNE MARGOLIN TYPE DMPN 3 4 A ANTENNA 2 37 FIGURE 2 11 KA 54A ANTENNA 2 39 FIGURE 2 12 HONEYWELL GT 7003586 SENSOR SYSTEMS TYPE S67 2002 4 ANTENNA 2 41 FIGURE 2 13 TNC COAX CONNECTOR ASSEMBLY RG 393 U 2 43 FIGURE 2 14 CONNECTOR PIN LOCATIONS 2 44 FIGURE 2 15 KRA...

Page 10: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page TC 6 006 10536 0010 Rev 10 Oct 2005 THIS PAGE IS RESERVED ...

Page 11: ...B RADAR ALTIMETER INSTALLATION MANUAL Page TC 7 006 10536 0010 Rev 10 Oct 2005 ITEM PAGE TABLE 1 1 KNI 415 416 INDICATOR AVAILABILITY 1 10 TABLE 1 2 CABLE INSTALLATIONS 1 11 TABLE 2 1 TSO CERTIFIED ANTENNAS 2 9 ...

Page 12: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page TC 8 006 10536 0010 Rev 10 Oct 2005 THIS PAGE IS RESERVED ...

Page 13: ...0 Configuration Module optional The system is positioned as a replacement for the KRA 405 Radar Altimeter System The preferred configurations utilize the following components COMPONENT UNIT PART NUMBER CHARACTERISTIC RADAR ALTIMETER KRA 405B 066 01153 0101 STANDARD KRA 405B 066 01153 0202 ARINC 552A KRA 405B 066 01153 2001 4001 ENHANCED DIGITAL AC CURACY CONTROLLER DISPLAY KNI 415 066 3031 00 5 VO...

Page 14: ...de information to the flight control system during the approach The KRA 405B Radar Altimeter P N 066 01153 0202 in addition to providing an ARINC 552A output for Auxiliary Out 2 has the ability to take a DH input from an EFIS or KNI 415 416 and generate an audio signal refer to section 1 3 C KRA 405B RECEIVER TRANSMITTER for tone generator circuit specifications The KRA 405B Radar Altimeter P N 06...

Page 15: ...s for KRA 405 and KRA 405B are not compatible 1 2 ACRONYMS AND ABBREVIATIONS ACRONYM MEANING AGL Above Ground Level ARINC Aeronautical Radio Incorporated EUROCAE The European Organization for Civil Aviation Electronics FAA Federal Aviation Administration FCC Federal Communications Commission FTZ Fernmeldetechischeszentralamt German Hz Hertz IF Intermediate Frequency kHz kilohertz GHz Gigahertz MHz...

Page 16: ...PHYSICAL CHARACTERISTICS Length Width Height See FIGURE 2 6 KRA 405B INSTALLATION DRAWING WEIGHT KRA 405B With Mtg rack optional See FIGURE 2 6 KRA 405B INSTALLATION DRAWING POWER REQUIREMENTS Nominal Current Maximum Current 27 5 Vdc 20 at 850 mA 18 Vdc 1 2 Amperes emergency ALTITUDE RANGE Tracked 20 to 2 500 feet 6 1 to 762 0 m ALTITUDE TRIPS selectable Adjustment Range 1 2 and 3 Con figuration M...

Page 17: ... mV m Zero feet 0 000 volts Auxiliary Out 2 0202 20 to 480 feet 6 1 to 146 3 m 20 mV ft 65 62 mV m 480 to 2 500 feet 146 3 to 762 m 10 x logn e h 20 500 10 x logn e h 6 1 152 4 m Zero ft 0 400 volts Analog Altitude 20 to 500 feet 6 1 to 152 4 m 20 mV ft 65 62 mV m 500 to 2 500 feet 152 4 to 762 m 3 mV ft 9 84 mV m Zero ft 0 400 volts Arinc 429 Out Shall meet all ARINC 429 electrical specifications...

Page 18: ...TER OUTPUT cont FM Deviation P P 100 MHz Type of Service Continuous WARNING SYSTEM FCS Warn Normal Operation 18 to 32 Vdc at less than 250 mA Warn Condition Less than 10 μA Altimeter Valid Normal Operation 18 to 32 Vdc at less than 250 mA Warn Condition Less than 10 μA Rad_Alt Valid Normal Operation 18 to 32 Vdc at less than 250 mA Warn Condition Less than 10 μA ALTITUDE TRIPS Tripped Locked R T 0...

Page 19: ...ac 10 120 mA Panel Lamp Power 5 volt units 5 Vdc 10 or 5 Vac 10 575 mA ALTITUDE RANGE DISPLAYED 20 to 2 000 feet 6 1 to 609 60 m ALTITUDE ACCURACY 0 to 500 ft 4 feet 1 22 m or 4 whichever is great er 500 to 2 000 ft 5 DECISION HEIGHT Altitude Range pilot adjustable 0 to 2 000 feet 0 to 609 60 m Accuracy 5 feet 1 27 m or 5 whichever is greater EXTERNAL DECISION HEIGHT OUTPUT Isolated pair of relay ...

Page 20: ...idth Height WEIGHT 2 required See FIGURE 2 11 KA 54A ANTENNA ALTITUDE 60 000 ft 18 281 m OPERATIONAL TEMPERATURE RANGE 54 C TO 85 C BEAMWIDTH E Plane 45 min H Plane 40 min SIDELOBES Greater than 40 dB down VSWR 4240 4360 MHz 1 5 1 Maximum GAIN 10 dBi above isotopic POLARIZATION Linear POWER HANDLING 1 watt average 10 watts peak CROSS COUPLING 20 in spacing 88 dB max 36 in spacing 95 dB max INPUT I...

Page 21: ...atible Honeywell KRA 405B P N 066 01153 2001 4001 Enhanced accuracy below 100 feet TSO COMPLIANCE C87 ETSO 2C87 DO 138 Env Cat AAAAAX PHYSICAL CHARACTERISTICS See FIGURE 2 8 KA 54 ANTENNA OUTLINE AND MOUNT ING DRAWING Length Width Height WEIGHT 2 required See FIGURE 2 8 KA 54 ANTENNA OUTLINE AND MOUNT ING DRAWING ALTITUDE 55 000 feet 16 764 m OPERATIONAL TEMPERATURE RANGE 54 C to 71 C BEAMWIDTH E ...

Page 22: ... which includes the following UNIT PART NUMBER FACEPLATE PANEL LIGHTING KNI 415 066 3031 00 BLACK 5 VOLT KNI 415 066 3031 01 BLACK 28 VOLT KNI 415 066 3031 02 GRAY 5 VOLT KNI 415 066 3031 03 GRAY 28 VOLT KNI 415 066 3031 04 BLACK NIGHT VISION KNI 416 066 3044 00 BLACK 5 VOLT KNI 416 066 3044 01 BLACK 28 VOLT KNI 416 066 3044 02 GRAY 5 VOLT KNI 416 066 3044 03 GRAY 28 VOLT KNI 416 066 3044 04 BLACK...

Page 23: ...OR PART NUMBER 030 02210 0012 Connector EA 1 ITT CANNON KPS306F14 19SY 057 02029 0008 Connector Label EA 1 057 02029 0009 Connector Label EA 1 073 00044 0001 Plate Mooring EA 1 073 00045 0000 Plate Adapter Blk EA 1 073 00045 0001 Plate Adapter Gry EA 1 089 05115 0012 FHP 6 32x3 4 Blk Scr EA 4 089 06461 0012 FHP 6 32x3 4 Gry Scr EA 4 PART NUMBER DESCRIPTION UM QTY VENDOR PART NUMBER 030 00108 0000 ...

Page 24: ...e Part No Part No Part No Part No Part No RG 393 024 00075 0000 030 00108 0004 TED 5 10 43 2 N A TED 5 30 14 1 RG 142 024 00002 0000 030 00134 0000 TED 5 10 30 030 00134 0001 TED 5 30 102 ECS 311601 024 00072 0000 N A ECS CTS 922 N A ECS CTR 922 ECS 311201 024 00071 0000 N A ECS CTS 122 N A ECS CTR 122 Cable Type CONNECTOR STRAIGHT TNC CONNECTOR RIGHT ANGLE TNC CONNECTOR 75 DEG ANGLE TNC PIC S4419...

Page 25: ... current software and the CM 2000 is required order P N 050 03311 0002 which contains the items listed below XX Highest Revision NOTE For CM 2000 Configuration Modules used in ART 2000 Weather Radar and KRA 405B Radar Altimeter Installations and CM 2000 configuration modules that have never been pro grammed or may have a default program for a different unit a write to initialization must be perfor...

Page 26: ...R CONTINUED AIRWORTHINESS 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 ...

Page 27: ...e applicant documents an acceptable installation 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 incurred 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 trans...

Page 28: ...ling to the equipment will lead to increased avionics maintenance costs and may also void the Honeywell warranty 2 4 CONFIGURABLE PARAMETERS The installer may alter some of the operational characteristics of the KRA 405B by installing a CM 2000 Configuration Module that has been programmed with customized preferences These characteristics are the threshold altitudes for the three Altitude Trip Poi...

Page 29: ...meter that is to be adjusted FIGURE 2 1 KRA 405B DEFAULT TRIP POINT SETTINGS Press the Enter key to display the Editing Window for the selected Trip Point The window should be similar to the following figure FIGURE 2 2 KRA 405B TRIP POINT EDITING WINDOW Enter an integer value between 0 and 2500 at the blinking cursor Press the Enter key to accept the value ...

Page 30: ...03 or 02 03 software and 2001 4001 version units with 01 03 or higher soft ware may provide slight negative values of altitude when the aircraft is taxiing or at rest This is normal oper ation as the altitude calculation may vary around zero at plus and minus the system accuracy All other unit and software configurations will clamp negative calculation results to zero feet and never go negative Th...

Page 31: ...acceptable with zero feet displayed at rest either do not install the configuration module or keep the default 0 feet value for the Zero Foot Offset The Zero Feet Offset has the following limitations 1 Zero Feet Offset must be a positive value 2 Zero Feet Offset must be less than 200 feet Note that alti tude values less than 20 feet shall be reported as 20 feet 3 Zero Feet Offset must be in whole ...

Page 32: ... data to the Configuration Module This must be completed before the module is installed For operational procedures refer to KPA 900 Operator s Guide Part Number 006 05392 00XX XX Latest Revision D DH AUDIO OUTPUT The KRA 405B 066 01153 0202 provides an audio output which some operators prefer to the visual indication of Decision Height The audio output is intended to be connected to an audio panel...

Page 33: ...s 2 Using four 4 6 32 screws secure the mounting tray in the position selected The fluted knob on the mounting tray should face in a direction to provide easy access 3 Slide the KRA 405B R T into the rack Secure the unit in place by hooking the triangular keeper over the front lip of the unit and tightening the fluted knob b For shock mounted units perform the following steps 1 Mark punch then dri...

Page 34: ...it is no different than the operation of a unit in a single radar al timeter installation 3 Zero Feet Calibration The KRA 405B Receiver Transmitter DOES NOT require an AID The KRA 405B R T has provisions to calibrate to zero 0 feet during installation such that the radar altitude is 0 feet when the aircraft is taxiing or stationary on the ground Re fer to section 2 6 A POST INSTALLATION CALIBRATIO...

Page 35: ...d to transmit the signal and the other is used to receive the reflected signal In order to meet the requirements of TSO C87 ETSO 2C87 the KRA 405B Radar Altimeter System must use TSO certified antennas with the characteristics listed in 1 3 TECHNICAL CHARACTERISTICS Recommended antennas are listed in TABLE 2 1 TSO CERTIFIED ANTENNAS below NOTE Variances between the S67 2002 and S67 2002 4 are depi...

Page 36: ...chnologies 455 Commack Road Deer Park NY 11729 4591 Telephone 631 595 3275 D PLANNING THE ANTENNA INSTALLATION Many factors are important when planning an optimum antenna installation for use with a radar altimeter system Careful planning and attention to detail are absolutely necessary Failure to install the antennas correctly will cause degradation in system performance Antennas should be mounte...

Page 37: ...er may not stow above 2500 feet if the leakage between the antennas is too great Antennas should not be separated by a distance greater than the antenna height above the terrain at touchdown If the antennas are separated by more than this distance sufficient terrain area is not illuminated for ground level operation The antennas should be mounted closer than the antenna height above the terrain bu...

Page 38: ...her as long as they remain on the same longitudinal axis If a side by side dual installation is chosen the transmit an tennas from the two units should be next to each other and the receive antennas should be next to each other see FIGURE 2 7 DUAL RADAR ALTIMETER SYSTEM TYPICAL ANTENNA INSTALLATIONS E IMPLEMENTING THE ANTENNA INSTALLATION NOTE Antenna and airframe surfaces must be free of paint or...

Page 39: ...s should be lashed securely but not to the point of cutting or distorting the cable insulation Cutting the coax shield causes an altitude return and affects system opera tion Tighten all antenna coax connectors slightly more than finger tight CAUTION DO NOT PAINT ANTENNA OPERATION AND OR ACCURACY MAY SUF FER AND MAY CAUSE UNIT TO LOCK ON TO ERRONEOUS ALTITUDES F ANTENNA CABLES After the location o...

Page 40: ...fied on the interconnect diagram Leave slack in cables to allow for free sway of the equipment After installation of the cables in the aircraft and before in stallation of the equipment a check should be made to ensure that the aircraft power is applied only to the pins specified H CONFIGURATION MODULE INSTALLATION The KRA 405B interfaces to the CM 2000 Configuration Module The configuration modul...

Page 41: ... antennas must be installed The KRA 405B antennas and coaxes must be mounted and routed in the final configuration to be representative of the normal flight conditions 2 The calibration must be accomplished outside of the hanger with no obstacles surrounding or underneath the aircraft Ex traneous reflections may cause an incorrect calibration 3 Allow a minimum of three minutes of warm up time befo...

Page 42: ...grammed into the configuration module this will be an indication of the negative value of the zero feet offset plus or minus the system tolerance of two or three feet Note that the analog indicators may not allow quantifiable negative indications A KRA 405B with software 01 04 02 04 or higher contain enhancements to the calibration routine 1 When the calibration is in process the KRA 405B will out...

Page 43: ...ill exist In order to determine whether an altimeter installation problem does exist the tests in Paragraphs 2 6 C KRA 405B RADAR ALTIMETER POST INSTALLATION TEST PROCEDURE and D TEST PROCEDURE can take the place of a flight test Agencies that install many altimeter systems including other manufacturer s equipment will find these test procedures quite helpful For the majority of installation probl...

Page 44: ...wer b Adjust the DH knob on the indicator to set the DH bug to 25 feet c Depress the test button on the indicator The altitude indicated should be 50 5 feet and the DH lamp should be out d Slowly advance the DH bug until the DH lamp lights The bug should be set at 50 5 feet at this time Continue increasing the DH bug setting The DH lamp should stay lit e Release the test button The indicated altit...

Page 45: ...r at the R T by exchanging the antenna coaxes cables at the R T Repeat Step f If the pointer still does not stow disconnect the an tenna cable from the R T unit s receiver port upper connector and terminate the receiver port with a 50 ohm load Load the transmitter antenna into the RF absorb er The indicator pointer should stow behind the mask Repeat this test for the transmitter port lower port an...

Page 46: ...estions in 2 5 KRA 405B SYSTEM INSTALLATION pertaining to the cables D TEST PROCEDURE KRA 405B Radar Altimeter Post Installation Test Procedures using 1000 Foot Delay Line 1 Purpose of Test This test simulates an actual altitude of 1000 feet AGL with various return signal strengths Low power output poor coax cables poor connectors and poor R T performance can be found using this method 2 Required ...

Page 47: ...vement while adjusting the variable attenua tor in Step c indicates a possible problem in the an tenna coax Connect the test equipment directly to the R T trans mitter port and connect to the receiver port via the 6 foot test cable Try Step c again Pointer movement while adjusting the variable attenuator indicates a possible R T problem The R T should be bench tested to insure proper opera tion e ...

Page 48: ... The test voltage range is from 0 to 25 volts with 0 volts corresponding to 0 feet and 25 volts correspond ing to 2500 feet Slowly run the test voltage from 0 to 25 volts and back down to 0 volts Confirm that the altimeter indicates a corresponding change in altitude 0 feet to 2500 feet and back to 0 feet and that the DH Lamp illuminates at the appropriate time c Remove the low from the ALTITUDE T...

Page 49: ...hten the fluted retaining screw clamp located on the front of the mounting rack until secure 2 Align unit with mounting holes and secure with 4 6 32 screws b Re attach mating cable to Cannon connector P4051 on the front of the unit c Re attach mating coaxial cables to XMIT P4052 and RCVR P4053 TNC connectors on the front of the unit B KNI 415 416 INDICATOR refer to FIGURE 2 5 KNI 415 416 INSTALLAT...

Page 50: ...al cable from antenna TNC connector b Remove the fasteners attaching the antenna to the air frame The number and pattern will vary depending on antenna type consult proper antenna mounting drawing for details 2 Re installation a Align antenna with panel mounting holes and secure with fasteners The number and pattern will vary depending on antenna type consult proper antenna mounting draw ing for d...

Page 51: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 25 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 5 KNI 415 416 INSTALLATION DRAWING Dwg No 155 05160 0000 R 1 ...

Page 52: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 27 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 6 KRA 405B INSTALLATION DRAWING Dwg No 155 06030 0000 R 0 ...

Page 53: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 29 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 7 DUAL RADAR ALTIMETER SYSTEM TYPICAL ANTENNA INSTALLATIONS Page 1 of 2 ...

Page 54: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 31 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 7 DUAL RADAR ALTIMETER SYSTEM TYPICAL ANTENNA INSTALLATIONS Page 2 of 2 ...

Page 55: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 33 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 8 KA 54 ANTENNA OUTLINE AND MOUNTING DRAWING DORNE MARGOLIN INC TYPE DMPN 3 3 A Dwg No 155 05159 0000 R 1 ...

Page 56: ...A 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 35 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 9 UBC TYPE AD 43013 1 AND COMANT TYPE 01 34 04531 ANTENNA OUTLINE AND MOUNTING DRAWING Dwg No 155 05166 0000 R 0 ...

Page 57: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 37 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 10 DORNE MARGOLIN TYPE DMPN 3 4 A ANTENNA OUTLINE AND MOUNTING DIAGRAM Dwg No 155 05167 0000 R 2 ...

Page 58: ...R ALTIMETER INSTALLATION MANUAL Page 2 39 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 11 KA 54A ANTENNA SENSOR SYSTEMS TYPE S67 2002 DORNE AND MARGOLIN TYPE DMPN 19 2 1 OUTLINE AND MOUNTING DRAWING P N 071 01501 0000 R AE ...

Page 59: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 41 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 12 HONEYWELL GT 7003586 SENSOR SYSTEMS TYPE S67 2002 4 ANTENNA OUTLINE AND MOUNTING DRAWING ...

Page 60: ...adar Altimeter System depends upon the VSWR of the antenna cable Therefore extreme care must be ex ercised in assembling the TNC connector to the RG 393 U cable Strict adherence to the above instructions will ensure a good VSWR of the antenna cables FIGURE 2 13 TNC COAX CONNECTOR ASSEMBLY RG 393 U P N 030 00108 0004 ...

Page 61: ... ALTIMETER INSTALLATION MANUAL Page 2 44 006 10536 0010 Rev 10 Oct 2005 KRA 405B MATING CONNECTOR P4051 P N 030 02077 0000 KRA 415 416 MATING CONNECTOR P4151 P4161 P N 030 02210 0001 FIGURE 2 14 CONNECTOR PIN LOCATIONS ...

Page 62: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 45 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 15 KRA 405B TEST EQUIPMENT SETUP ...

Page 63: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 46 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 16 EXTERNAL SONALERT W 15 SECOND DH AUDIO FADER ...

Page 64: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 47 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 17 KRA 405B RADAR ALTIMETER SYSTEM INTERCONNECT Dwg No 155 01645 0000 R AD ...

Page 65: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 2 49 006 10536 0010 Rev 10 Oct 2005 FIGURE 2 18 CM 2000 CONFIGURATION MODULE MOUNTING DRAWING Dwg No 155 06016 0000 R 2 ...

Page 66: ...eet each mark represents 5 feet from 200 to 500 feet each mark represents 20 feet and from 500 to 2000 feet each mark represents 100 feet Indicator Needle The AGL altitude in feet is displayed beneath this needle Needle will be clockwise behind mask when above 2000 feet Flag Indicates invalid altitude information is being displayed or self test button is depressed Self Test Button This button is u...

Page 67: ...a tor to set the DH bug to 25 feet 3 Depress the TEST button The indicated altitude should be 50 5 feet and the flag should come into view The DH lamp should be out 4 With the TEST button depressed slowly increase the DH bug until the DH lamp lights The bug should be 50 5 feet The lamp should be lit at all altitudes above 50 feet 5 Release the TEST switch The warning flag should move out of view a...

Page 68: ...n the approach plans are reviewed prior to beginning the actual approach the pilot should set the DH bug to the decision height altitude and check altimeter operation When decision height is reached the DH Lamp lights to alert the pilot that a decision should be made The DH Lamp may then be turned off by pressing the lamp in E PUSH TO TEST MODE 1 To check altimeter operation depress the TEST butto...

Page 69: ...ted altitude is cor rect Indicator Failure Radar Altime ter System failures may not be indicated by a flag Repair is required DH Lamp fails to light Indicator Failure The decision height will not be annunciated Repair is required The altimeter indicates 100 feet The system s receiver transmit ter is inoperative Repair is re quired The altimeter indicates 200 feet Configuration module failure Re pa...

Page 70: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 3 5 006 10536 0010 Rev 10 Oct 2005 FIGURE 3 1 KNI 415 CONTROL FUNCTIONS ...

Page 71: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page 3 6 006 10536 0010 Rev 10 Oct 2005 FIGURE 3 2 KNI 416 CONTROL FUNCTIONS ...

Page 72: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page AppE 1 006 10536 0010 Rev 10 Oct 2005 TSO APPENDIX ENVIRONMENTAL QUALIFICATION FORMS ...

Page 73: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page AppE 2 006 10536 0010 Rev 10 Oct 2005 THIS PAGE IS RESERVED ...

Page 74: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page AppE 3 006 10536 0010 Rev 10 Oct 2005 ...

Page 75: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page AppE 4 006 10536 0010 Rev 10 Oct 2005 ...

Page 76: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page AppE 5 006 10536 0010 Rev 10 Oct 2005 ...

Page 77: ...N KRA 405B RADAR ALTIMETER INSTALLATION MANUAL Page AppE 6 006 10536 0010 Rev 10 Oct 2005 THIS PAGE IS RESERVED ...

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