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L3 CP-2500, Руководство по установке

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L3 CP-2500 Скачать руководство пользователя страница 42

CP-2500 

Installation Manual 

 

Page A-4  

Appendix A 

0040-17251-01 

March 15, 2018 

Revision D 

 

PIN 13 

Signal Name: 

Reserved 

Signal Type: 

--- 

Electrical Characteristics: 

--- 

Connection: 

No Connection 

Comments: 

 

 

PIN 14 

Signal Name: 

Reserved 

Signal Type: 

--- 

Electrical Characteristics: 

--- 

Connection: 

No Connection 

Comments: 

 

 

PIN 15 

Signal Name: 

Reserved 

Signal Type: 

--- 

Electrical Characteristics: 

--- 

Connection: 

No Connection 

Comments: 

 

 
 
 

Содержание CP-2500

Страница 1: ... 9080 17250 Installation Manual This manual contains installation instructions recommended flightline maintenance information and operation information for the CP 2500 Control Panel This information is supplemented and kept current by revisions service letters and service bulletins ...

Страница 2: ... your comments concerning this manual Although every effort has been made to keep it free of errors some may occur When reporting a specific problem please describe it briefly and include the manual part number the paragraph figure table number and the page number Send your comments to the address or email above Disclaimer This manual contains information that is considered relevant only at the ti...

Страница 3: ...ghtline maintenance procedures It includes periodic maintenance troubleshooting return to service checkout instructions and disposition of defective components APPENDIX A SIGNAL AND CABLE CHARACTERISTICS This appendix defines the electrical characteristics of all input and output signals APPENDIX B ENVIRONMENTAL QUALIFICATION FORM Descriptions for Warnings Cautions and Notes are used throughout th...

Страница 4: ...either downloading from the L3 Technical Publications website may require secure site access or by receiving a copy via email Send an email request to 21T21Tavionics techpubs L3T com21T21T Note Additional request for software and databases may be required Service Literature Description None Publication Description 0040 17250 01 Pilot s Guide for the CP 2500 0040 17010 01 Pilot s Guide for the Lynx...

Страница 5: ...nt Matter i thru viii Section 1 General Information 1 1 thru 1 6 Section 2 Installation 2 1 thru 2 10 Section 3 Installation Checkout 3 1 thru 3 10 Section 4 Maintenance 4 1 thru 4 2 Appendix A Signal Name and Characteristics A 1 thru A 4 Appendix B Environmental Qualification Form A 1 thru B 2 REVISION HIGHLIGHTS Revision D is a republication This republication completely replaces the existing bo...

Страница 6: ...n 1 2 1 2 1 NGT 1000 2000 2500 1 3 1 2 2 NGT 9000R 1 3 1 3 Specifications 1 4 1 4 Modifications 1 5 1 5 Configuraton Versions 1 5 1 6 Interfaces 1 5 1 7 Equipment Required Not Supplied 1 5 1 8 Installation Kit 1 6 1 9 Installation Approval and Limitations 1 6 Section 2 Installation 2 1 Introduction 2 1 2 2 Unpacking and inspecting 2 1 2 2 1 Transport and Storage Considerations 2 1 2 3 installation...

Страница 7: ...k Brightness Controls 3 9 3 3 5 Checkout Complete 3 9 Section 4 Maintenance 4 1 Introduction 4 1 4 2 Continued airworthiness 4 1 4 2 1 Periodic Maintenance 4 1 4 3 Fault Isolation 4 1 4 4 return to Service 4 1 4 4 1 Remove and Replace Procedures 4 2 4 5 Disposition Of Failed Items 4 2 Appendix A Signal Name Cable Characteristics A 1 Introduction A 1 A 1 1 RS 232 BUS A 1 A 2 Wire and Signal charact...

Страница 8: ...mensions for 9080 17250 12 2 4 Figure 2 4 P1 Mating Connector and Pin Assignments 2 6 Figure 2 5 Interconnect Wiring Diagram for NGT 1000 2000 2500 2 7 Figure 2 6 Interconnect Wiring Diagram for Lynx NGT 9000R 2 8 Figure 3 1 CP 2500 Display and Controls 3 2 List of Tables Table Page Table 1 1 CP 2500 Configurations 1 1 Table 1 2 Hardware Modifications 1 5 Table 1 3 CP 2500 Configuration Versions 1...

Страница 9: ...EAR Export Administration Regulations ESDS Electrostatic Discharge Sensitive FAA Federal Aviation Administration FCC Federal Communications Commission FIS B Flight Information System Broadcast GPS Global Positioning System i e That is ID or IDENT or IDT Identification INIT Initialization LED Light Emitting Diode LRU Line Replaceable Unit MI Michigan MSS MultiLink Surveillance System N A Not Applic...

Страница 10: ...CP 2500 Installation Manual Page viii 0040 17251 01 March 15 2018 Revision D This page intentionally blank ...

Страница 11: ...GT 9000R Release 1 1 9080 17250 02 2 1 4 inch bezel FW Rev 15 16 HW Rev 01 Compatible with NGT 1000 2000 2500 Version 1 with Release 1 3 1 52 and Version 2 with Release 1 8 or earlier Compatible with NGT 9000R Release 2 0 2 1 3 0 3 1 9080 17250 02 2 1 4 inch bezel FW Rev 17 or greater HW Rev 01 Compatible with NGT 1000 2000 2500 Version 1 with release 1 52 and Version 2 with Release 1 8 or earlier...

Страница 12: ...n be rotated and pressed to activate functions LED display and backlighting provides a sunlight readable display with smooth dimming Refer to Figure 1 1 The following are models of the Lynx MultiLink Surveillance Systems that interface with the CP 2500 NGT 1000 NGT 2000 NGT 2500 also referred to as NGT 1000 2000 2500 NGT 9000R NGT 9000R NGT 9000RD NGT 9000RD also referred to as NGT 9000R NOTES 1 W...

Страница 13: ... displays the following information Transponder Code Mismatch Message Fault Indications Fault Messages Pressure Altitude ADS B Out of Coverage indication NGT 2000 2500 only 1 2 2 NGT 9000R 1 The CP 2500 provides the following control functionality Enter Mode A Squawk Code Set Operation Mode with selections of On Alt or Sby IDENT VFR Code select Set Flight ID optional enabled during installation Ac...

Страница 14: ... environmental qualification form in Appendix B SIZE See outline drawings in installation section WEIGHT 0 5 lbs 0 23 kg CHASSIS GROUND Bonding impedance between aircraft ground and the CP 2500 Chassis must be less than 2 5 milliohms POWER REQUIREMENTS 11 0 to 33 0 Volts DC 4 Watts Max Startup 2 Watts Nominal CONNECTOR TYPE Mating Connector 15 pin sub D P N 425 015 2052 INTERFACE S RS 232 OPERATIN...

Страница 15: ...ES The electrical characteristics of all input and output signals are detailed in Appendix A 1 7 EQUIPMENT REQUIRED NOT SUPPLIED ITEM DESCRIPTION Cables and Wiring The installer will supply all system wires and cables All wires are 22 AWG as noted in the installation section Use MIL DTL 16878 or equivalent wire and use M27500 or equivalent for twisted shielded wire for installation Circuit Breaker...

Страница 16: ...x 3 8 Machine Screws 475 632 006 4 1 9 INSTALLATION APPROVAL AND LIMITATIONS The conditions and tests required for TSO approvals of this article are minimum performance standards It is the responsibility of those desiring to install this article either on or within a specific type or class of aircraft to determine the suitability of the installation The article may be installed only if further eva...

Страница 17: ... Considerations Transport of the CP 2500 should be done in accordance with standard procedures i e hand carried or transported in the original container Storage of the CP 2500 must be consistent with industry standards for avionics equipment and will perform satisfactorily after periods of storage up to 18 months The ambient temperature of the storage area should not fall below 55 C 67 F or rise a...

Страница 18: ...rcraft The electrical bond should achieve direct current DC resistance less than or equal to 5 0 m to the instrument panel for composite aircraft 2 3 1 Location The CP 2500 should be mounted in the instrument panel slightly below and in close proximity with the pilot s normal line of view with the controls within easy reach In selecting a location consider the following 1 The CP 2500 should be acc...

Страница 19: ...CP 2500 Installation Manual 0040 17251 01 Installation Page 2 3 Revision D March 15 2018 Figure 2 2 Outline Dimensions for 9080 17250 01 02 ...

Страница 20: ...CP 2500 Installation Manual Page 2 4 Installation 0040 17251 01 March 15 2018 Revision D Figure 2 3 Outline Dimensions for 9080 17250 12 ...

Страница 21: ...ing appropriate circuit breakers needed to protect aircraft wiring Manufacturer recommends a 1 0 amp circuit breaker The CP 2500 can alternately share a circuit breaker with the Lynx MSS Refer to the installation manual for the Lynx MSS for details refer to references in front section for manual part numbers All connections are made through a single 15 pin Sub D connector located at the rear of th...

Страница 22: ...CP 2500 Installation Manual Page 2 6 Installation 0040 17251 01 March 15 2018 Revision D Figure 2 4 P1 Mating Connector and Pin Assignments ...

Страница 23: ...CP 2500 Installation Manual 0040 17251 01 Installation Page 2 7 Revision D March 15 2018 Figure 2 5 Interconnect Wiring Diagram for NGT 1000 2000 2500 ...

Страница 24: ...CP 2500 Installation Manual Page 2 8 Installation 0040 17251 01 March 15 2018 Revision D Figure 2 6 Interconnect Wiring Diagram for Lynx NGT 9000R ...

Страница 25: ... be required before installation of the unit 2 The CP 2500 mounts on the backside of the instrument panel Carefully hold the CP 2500 in place behind the instrument panel 3 Secure CP 2500 to instrument panel using 4 mounting screws provided in the installation kit and mooring plate or nut plates as applicable 2 3 4 Performance Test After installation is completed complete the installation checkout ...

Страница 26: ...CP 2500 Installation Manual Page 2 10 Installation 0040 17251 01 March 15 2018 Revision D This page intentionally blank ...

Страница 27: ...n the left side of the display and the squawk code on the right side of the display as shown in Figure 3 1 The four digit squawk code may be missing when the Alt and On operational modes are on the display the code is shown in Sby mode The squawk code is removed in order to show that the Lynx MSS has a system message system failure or the GPS signal has been missing for more than two minutes Note ...

Страница 28: ...s applied the unit goes through a power on self test that lasts for 10 seconds Verify the firmware and hardware versions are correct and that the system status shows OK Note FW and HW versions are listed in the General Information section If a Failed message is shown on the display cycle power the CP 2500 If the Failed message continues replacement of the CP 2500 may be required Contact ACSS Field...

Страница 29: ...o change the CP 2500 code to the same code as the transponder 3 3 2 2 NGT 1000 2000 2500 Version 2 1 Verify that the following messages are not shown on the display If a message is observed cycle power to the Lynx MSS system If the message continues to be shown refer to the appropriate Lynx MSS Installation Manual for detailed troubleshooting information or contact ACSS Field Service GPS FAIL ADS ...

Страница 30: ... MSS system If the message continues to be shown refer to the appropriate Lynx MSS Installation Manual for detailed troubleshooting information or contact ACSS Field Service GPS FAIL ADS B OUT FAIL ADS B IN FAIL NO LRU RESPONSE incorporated in CP 2500 Firmware 15 and later FIS B FAIL XPDR FAIL TAS FAIL TAWS FAIL 2 The following messages may be seen but do not indicate a problem with the CP 2500 or...

Страница 31: ... do not indicate a problem with the CP 2500 or the Lynx MSS GPS INIT This message is removed after the GPS completes initialization STANDBY This message is seen only when the transponder STANDBY mode is activated by the remote discrete to the NGT 9000R Typically only used in dual NGT 9000R installations NO ADS B COVERAGE This message is removed once the Lynx MSS begins receiving an ADS B ground st...

Страница 32: ...to change status to Enable 5 Press the small knob again to activate self test 6 When activated the screen momentarily displays Test Started 7 The results of the test are that the ADS B Out Fail lamp flashes during the test 8 Press the M button to exit or scroll the large knob to Done and then press small knob to exit and return to normal operation 3 3 3 2 NGT 2000 2500 Version 1 with Software Rele...

Страница 33: ...are shown on the CP 2500 screen for 5 seconds each The possible fail messages are GPS Fail ADS B IN Fail ADS B OUT Fail and FIS B Fail NGT 2000 2500 only 3 3 3 4 NGT 1000 2000 2500 Version 2 with SW release 1 51 or greater 1 Press the Menu M button 2 Rotate the large knob to scroll the menu to Maintenance 4 Press small knob to display Self Tst 5 Press the small knob again to activate self test 6 W...

Страница 34: ...n 8 Rotate the large knob to scroll the menu to Maintenance 9 Press small knob to display Self Tst 10 Press the small knob again to activate self test 11 When activated the screen momentarily displays Test Started followed by Test In Progress If the optional traffic or PED display is installed each will show three targets during the test If the optional ADS B Out Fail traffic advisory and TAWS lam...

Страница 35: ...etected a fail message is flashed on the CP 2500 screen for 5 seconds The possible fail messages are NO LRU RESPONSE XPDR FAIL ADS B OUT FAIL ADS B IN FAIL FIS B FAIL GPS FAIL TAS FAIL TCAS FAIL TAWS FAIL If a degraded condition is detected a degraded message is flashed on the CP 2500 screen for 5 seconds The possible degraded messages are GPS INIT ADS B OUT DEGRADED ADS B IN DEGRADED TAS DEGRADED...

Страница 36: ...CP 2500 Installation Manual Page 3 10 Installation Checkout 0040 17251 01 March 15 2018 Revision D This page intentionally blank ...

Страница 37: ...nd secured Check that connecting cables are not cut or pinched and not in contact with other items behind the instrument panel Check the CP 2500 faceplate for cleanliness The bezel button and display glass can be cleaned with a damp lint free static free cloth If necessary clean with a soft cloth moistened with a mild solution of soap and water Care should be taken to avoid scratching the surface ...

Страница 38: ...thorization RMA Shipping Instructions will be provided with the RMA 3 If available pack components in their original shipping container If the original container is not available pack them as follows CAUTION Do not use desiccant crystals when packaging electronic assemblies Since the assembly must be packed tightly crystals in bag form cannot be used The use of loose crystals may cause unnecessary...

Страница 39: ...1 Data length 8 bits Stop Bits 1 Parity None Flow Control None Table A 1 LRU Version Release Definitions INTERFACING UNIT LRU HARDWARE VERSION RELEASE VERSION DEFINITION DISCRETE INDICATOR FROM LRU BYTE 13 VALUE NGT 1000 Version 1 Release Rel 1 SW Release 1 0 1 1 0 Appliance Rel 1 NGT 2000 2500 Version 1 Release Rel 1 SW Release 1 0 1 1 1 2 or 1 3 0 Appliance Rel 1 NGT 1000 Version 1 Release Rel 2...

Страница 40: ...stics Data bits 8 Parity none Stop bit 1 Start bit 1 Data format is ASCII Flow control is none Baud Rate 9600 bps Connection 22 AWG Wire twisted shielded pair wire Comments PIN 4 Signal Name RS232_RX Signal Type RS 232 Electrical Characteristics Data bits 8 Parity none Stop bit 1 Start bit 1 Data format is ASCII Flow control is none Baud Rate 9600 bps Connection 22 AWG Wire twisted shielded pair w...

Страница 41: ...Chassis GND Signal Type Ground panel case Electrical Characteristics Connection Airframe Ground 22 AWG Wire Comments PIN 9 Signal Name Reserved Signal Type Electrical Characteristics Connection No Connection Comments PIN 10 Signal Name Reserved Signal Type Electrical Characteristics Connection No Connection Comments PIN 11 Signal Name Reserved Signal Type Electrical Characteristics Connection No C...

Страница 42: ...Signal Name Reserved Signal Type Electrical Characteristics Connection No Connection Comments PIN 14 Signal Name Reserved Signal Type Electrical Characteristics Connection No Connection Comments PIN 15 Signal Name Reserved Signal Type Electrical Characteristics Connection No Connection Comments ...

Страница 43: ...85 C Ground Survival In Flight Loss of Cooling 4 5 5 Not Applicable Not Tested External Cooling Not Required Altitude 4 6 1 Tested to 20 000 ft Maximum Operating Altitude Decompression 4 6 2 A1F1 A2F2 8 000 ft to 20 000 ft Overpressure 4 6 3 15 000 ft Temperature Variation 5 3 1 B 5 C min Humidity 6 3 1 B Standard Humidity Environment 10 day test Operational Shocks and Crash Safety Operational Sho...

Страница 44: ... 15kHz 0 6 0 004pk pk from 15kHz to 150kHz Induced Signal Susceptibility 19 ZC For Aircraft Primary Power 400Hz Constant Frequency or DC RF Susceptibility Radiated and Conducted 20 TT Conducted Susceptibility 10KHz to 400MHz 7 5mA CW SW modulation Radiated Susceptibility 100MHz to 8GHz 5V m CW SW modulation Emission of RF Energy 21 M Interference free operation Lightning Induced Transient Suscepti...

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