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22 Apr 2019

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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL

ASPIRE-400

Table INTRO-2. List of Acronyms and Abbreviations (Continued)

Term

Full Term

PSAC

Plan for Software Aspects of Certification

PSC

Power Supply Card

PSCP

Project Specific Certification Plan

PSP

Partnership for Safety Plan

PSSA

Preliminary System Safety Assessment

PSU

Power Supply Unit

RAN

Radio Access Network

Radio Frequency

RTCA

Radio Technical Commission for Aeronautics

SAE

Society of Automotive Engineers

SAS

Software Accomplishment Summary

SATCOM

Satellite Communications

SATDATA

Satellite Data

SATVOICE

Satellite Voice

service bulletin

SBB

Swift Broad Band

SBD

Short Burst Data

SCI

Software Configuration Index

SCM

SDU Configuration Module

SCMP

Software Configuration Management Plan

SDIM

System Description and Installation Manual

SDU

Satellite Data Unit

SEU

Single Event Upset

SIP

Serial Interface Protocol

SITA

Société Internationale de Télécommunications Aéronautiques

SOI

Stage of Involvement

SSA

System Safety Assessment

STC

Supplemental Type Certificate

Software

DRAFT

3rd rvw Draft as of:

29 January, 2020

Содержание 90402651-000

Страница 1: ...imate consignee or end user s either in their original form or after being incorporated into other items without first obtaining approval from the U S government or as otherwise authorized by U S law and regulations ECCN 7E994 Export Control Legal Notice Part Number Model 90404514 000 ASPIRE 400 HPA 90402651 000 ASPIRE 400 SDU 90402652 000 ASPIRE 400 SCM System Description Installation and Mainten...

Страница 2: ...d those of a purchase order or acknowledgement Your access or use of the Materials represents your acceptance of the terms of this License Agreement 1 License Grant If you are a party to an applicable written agreement with Honeywell relating to the repair or maintenance of the subject Honeywell Product subject to your compliance with the terms and conditions of this License Agreement Honeywell he...

Страница 3: ...rty then has hereunder Otherwise neither this License Agreement nor any rights licenses or privileges granted under this License Agreement nor any of its duties or obligations hereunder nor any interest or proceeds in and to the Materials shall be assignable or transferable in insolvency proceedings by merger by operation of law by purchase by change of control or otherwise by you without Honeywel...

Страница 4: ...the License Agreement and merges all prior discussions and negotiations among them This License Agreement may be modified only by a duly authorized representative of Honeywell Safety Advisory WARNING BEFORE THE MATERIALS CALLED OUT IN THIS PUBLICATION ARE USED KNOW THE HANDLING STORAGE AND DISPOSAL PRECAUTIONS RECOMMENDED BY THE MANUFACTURER OR SUPPLIER FAILURE TO OBEY THE MANUFACTURERS OR SUPPLIE...

Страница 5: ...YSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Copyright Notice Copyright 2019 Honeywell International Inc All rights reserved Honeywell is a registered trademark of Honeywell International Inc All other marks are owned by their respective companies D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 6: ...national Inc Do not copy without express permission of Honeywell Page T 6 22 Apr 2019 23 15 49 Blank Page SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 7: ...O HOLDERS OF ASPIRE 400 SDIM ATA NO 23 15 49 PUB NO D201902000020 ISSUED FOR USE IN SUPPORT OF THE FOLLOWING Table TI 1 shows the applicable components Table TI 1 Applicable Components Component PN Nomenclature 90404514 000 ASPIRE 400 HPA 90402651 000 ASPIRE 400 SDU 90402652 000 ASPIRE 400 SCM Revision History This is an INITIAL release of ASPIRE 400 SDIM ATA NO 23 15 49 D R A F T 3rd rvw Draft as...

Страница 8: ...l International Inc Do not copy without express permission of Honeywell Page TI 2 22 Apr 2019 23 15 49 Blank Page SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 9: ... 400 RECORD OF REVISIONS For each revision write the revision number revision date date put in the manual and your initials in the applicable column NOTE Refer to the Revision History in the TRANSMITTAL INFORMATION section for revision data Revision Number Revision Date Date Put in Manual By Revision Number Revision Date Date Put in Manual By D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 10: ...l International Inc Do not copy without express permission of Honeywell Page RR 2 22 Apr 2019 23 15 49 Blank Page SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 11: ...For each temporary revision put the applicable data in the record columns on this page Definition of Status column A TR may be active incorporated or deleted Active is entered by the holder of the manual Incorporated means a TR has been incorporated into the manual and includes the revision number of the manual when the TR was incorporated Deleted means a TR has been replaced by another TR a TR nu...

Страница 12: ...l International Inc Do not copy without express permission of Honeywell Page RTR 2 22 Apr 2019 23 15 49 Blank Page SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 13: ...xpress permission of Honeywell Page SBL 1 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 SERVICE BULLETIN LIST Service Bulletin Revision Number Title Modification Date Put In Manual D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 14: ...l International Inc Do not copy without express permission of Honeywell Page SBL 2 22 Apr 2019 23 15 49 Blank Page SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 15: ...22 Apr 2019 TOC 10 22 Apr 2019 TOC 11 22 Apr 2019 TOC 12 22 Apr 2019 Introduction INTRO 1 22 Apr 2019 INTRO 2 22 Apr 2019 INTRO 3 22 Apr 2019 INTRO 4 22 Apr 2019 INTRO 5 22 Apr 2019 INTRO 6 22 Apr 2019 INTRO 7 22 Apr 2019 INTRO 8 22 Apr 2019 INTRO 9 22 Apr 2019 INTRO 10 22 Apr 2019 Section 1 SYSTEM DESCRIPTION 1 1 22 Apr 2019 1 2 22 Apr 2019 1 3 22 Apr 2019 1 4 22 Apr 2019 1 5 22 Apr 2019 1 6 22 A...

Страница 16: ... Apr 2019 2 24 22 Apr 2019 2 25 22 Apr 2019 2 26 22 Apr 2019 2 27 22 Apr 2019 2 28 22 Apr 2019 2 29 22 Apr 2019 2 30 22 Apr 2019 2 31 22 Apr 2019 2 32 22 Apr 2019 2 33 22 Apr 2019 2 34 22 Apr 2019 2 35 22 Apr 2019 2 36 22 Apr 2019 2 37 22 Apr 2019 2 38 22 Apr 2019 2 39 22 Apr 2019 2 40 22 Apr 2019 2 41 22 Apr 2019 2 42 22 Apr 2019 2 43 22 Apr 2019 2 44 22 Apr 2019 Section 3 SYSTEM PRE CONFIGURATIO...

Страница 17: ...2019 F 4 43 4 44 22 Apr 2019 4 45 22 Apr 2019 4 46 22 Apr 2019 Section 5 SOFTWARE CONFIGURATION 5 1 22 Apr 2019 5 2 22 Apr 2019 5 3 22 Apr 2019 5 4 22 Apr 2019 5 5 22 Apr 2019 5 6 22 Apr 2019 5 7 22 Apr 2019 5 8 22 Apr 2019 5 9 22 Apr 2019 5 10 22 Apr 2019 5 11 22 Apr 2019 5 12 22 Apr 2019 5 13 22 Apr 2019 5 14 22 Apr 2019 5 15 22 Apr 2019 5 16 22 Apr 2019 5 17 22 Apr 2019 5 18 22 Apr 2019 5 19 22...

Страница 18: ...AINTENANCE PRACTICES 6 1 22 Apr 2019 6 2 22 Apr 2019 6 3 22 Apr 2019 6 4 22 Apr 2019 6 5 22 Apr 2019 6 6 22 Apr 2019 6 7 22 Apr 2019 6 8 22 Apr 2019 6 9 22 Apr 2019 6 10 22 Apr 2019 6 11 22 Apr 2019 6 12 22 Apr 2019 6 13 22 Apr 2019 6 14 22 Apr 2019 6 15 22 Apr 2019 6 16 22 Apr 2019 6 17 22 Apr 2019 6 18 22 Apr 2019 6 19 22 Apr 2019 6 20 22 Apr 2019 6 21 22 Apr 2019 6 22 22 Apr 2019 6 23 22 Apr 20...

Страница 19: ... 22 Apr 2019 A 3 22 Apr 2019 A 4 22 Apr 2019 A 5 22 Apr 2019 A 6 22 Apr 2019 A 7 22 Apr 2019 A 8 22 Apr 2019 A 9 22 Apr 2019 A 10 22 Apr 2019 A 11 22 Apr 2019 A 12 22 Apr 2019 LIST OF EFFECTIVE PAGES Cont Subheading and Page Date Subheading and Page Date EFFECTIVITY Honeywell International Inc Do not copy without express permission of Honeywell Page LEP 5 22 Apr 2019 Indicates a changed or added p...

Страница 20: ...l International Inc Do not copy without express permission of Honeywell Page LEP 6 22 Apr 2019 23 15 49 Blank Page SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 21: ...SK 23 15 49 1 1 A General 1 1 B Hardware Part Numbers 1 1 2 HPA Description TASK 23 15 49 1 3 A About High Power Amplifier HPA 1 3 3 SDU System TASK 23 15 49 1 6 A Satellite Data Unit 1 6 B SDU Functions and Services 1 6 C Application Mode Single Channel Aspire 400 ACD AIS Configuration 1 6 D Application Mode Dual Channel Aspire 400 ACD AIS PIES Configuration 1 8 E SDU System Characteristics 1 10 ...

Страница 22: ... Attenuator 2 11 C Tx Gain Monitoring 2 11 D Input Power Detector Function 2 12 8 Controller Functions 2 13 A Single Event Upset 2 13 B Self Test 2 14 9 ARINC 429 Messaging 2 16 A Message Set Integrity 2 16 B HPA Status Word ARINC 429 Label 143 2 17 10 SDU Modes of Operations 2 17 A Power On Mode 2 17 B External System Interfaces 2 18 C Application Modes 2 18 11 Cockpit Control and Display MCDU TA...

Страница 23: ...perations 2 40 A SDU Configuration Test Mode 2 40 B SATCOM System Configuration Test Mode 2 40 16 Safety Data Services TASK 23 15 49 2 40 A Overview 2 40 B AAP Protocol and Supported Services 2 40 17 Aircraft Information TASK 23 15 49 2 41 A Time and Date 2 41 B Operational Air Ground Status 2 42 C Temperature Profile 2 43 D AES ID 2 43 SECTION 3 SYSTEM PRE CONFIGURATION 3 1 1 Aircraft Information...

Страница 24: ... Input 4 26 E DC Momentary Power Interruptions 4 26 F Ground Reference Fluctuation 4 26 6 Electrical Drawings 4 26 A Electrical Drawings 4 26 7 Power Conditioning Characteristics 4 45 A Secondary Power Monitoring and Control 4 45 B Hold Up Capacity Power Interruption 4 46 SECTION 5 SOFTWARE CONFIGURATION 5 1 1 Overview TASK 23 15 49 5 1 A Software Part Numbers 5 1 B Software 5 1 C Aspire 400 Licen...

Страница 25: ...20 J PIES AT Header Compression 5 25 K NTP 5 25 L FOIP 5 25 M Cabin Voice Communications 5 25 N Cabin VOIP 5 26 O Receive RF Signal Selection 5 26 8 Satellite Selection and Handover 5 26 A Overview 5 26 B Satellite Selection 5 27 C Satellite Handover 5 28 9 Safety Data Session 5 29 A Safety Data VPN Establishment 5 29 B IPsec Tunnel creation 5 30 C AAP Safety Data Gateway Log On 5 30 10 Aircraft F...

Страница 26: ...cal Logs and Records 6 1 B Historical Usage Log and Records 6 1 C Historical Security Log and Records 6 1 D BITE Flight Leg 6 3 E Historical ORT Records 6 3 2 Web Interface 6 3 A WEB GUI 6 3 B Display Format 6 4 C Maintenance Access Levels 6 6 D User Level 6 7 E Maint Level 6 8 F Advanced Maint Level 6 9 G System Integration Test Level 6 9 H Factory Level 6 10 I Eng Level 6 10 J Maintenance Functi...

Страница 27: ...D 7 1 A ACD Startup Functions 7 1 B ACD Boot 7 1 C Satellite Connectivity State Logon Condition 7 4 2 Loss of PS CS Attachment 7 6 A ACD Loss of PS CS Attachment 7 6 B PIESD Loss of PS CS Attachment 7 8 C Short Service Interruption Handling 7 9 D Doppler Compensation 7 9 E Miscellaneous Inmarsat Functions 7 9 F AAP Safety Data Gateway Log Off 7 10 G Datalink Service Status Reporting to the CMU 7 1...

Страница 28: ...ASK 23 15 49 A 8 A Thermal Appraisal A 8 B Audio Frequency Conducted Emissions Tests A 8 7 Industry Standards A 8 A ARINC Inc A 8 B Institute for Interconnecting and Packaging Electronic Circuits A 8 C Telecommunications Industry Association A 9 D RTCA Inc A 9 E Inmarsat A 9 F International Electrotechnical Commission IEC A 9 G Society of Automotive Engineers SAE A 9 H Other A 9 8 Certification Ba...

Страница 29: ...am of an AES6 and its Major Components 1 18 1 9 Block Diagram of an AES7 and its Major System Components 1 20 2 1 Modes of Operation 2 2 2 2 Dual SATCOM Standalone Configuration 2 21 2 3 Dual SATCOM Dual Configuration 2 24 2 4 Incoming PS Call Decision Logic 2 32 4 1 HPA Outline and Installation 4 3 4 4 4 2 SCM Outline and Installation 4 9 4 10 4 3 SDU Outline and Installation 4 11 4 12 4 4 ARINC ...

Страница 30: ...Status 2 42 4 1 SDU Standalone Identification System SIS Interface Characteristics 4 23 5 1 Software Part Numbers 5 1 5 2 TCCA CAN TSOs for the Aspire 400 5 2 5 3 CAN TSO submittals 5 3 5 4 ARINC Swift MIB Branches 5 15 5 5 Data from Primary IRS GNSS 5 42 5 6 Data from Secondary IRS GNSS 5 43 5 7 Data from GNSS to SDU 5 44 5 8 AES ID Input 5 44 5 9 Label 050 Coded Discrete Command Word 5 45 5 10 L...

Страница 31: ...NTENANCE MANUAL ASPIRE 400 TABLE OF CONTENTS Continued LIST OF TABLES Table Description Page 7 1 Priority SATCOM System State Description 7 4 7 2 Priority Non Safety Logon State Description 7 5 A 1 Environmental Conditions and Test Procedures A 4 A 2 TCCA CAN TSOs for the Aspire 400 A 9 A 3 Planned CAN TSO submittals A 10 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 32: ... International Inc Do not copy without express permission of Honeywell Page TOC 12 22 Apr 2019 23 15 49 Blank Page SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 33: ...ce procedure which if not obeyed can cause damage to the equipment c A NOTE gives data not commands The NOTE helps personnel when they do the related instruction 5 Warnings and cautions go before the applicable paragraph or step Notes follow the applicable paragraph or step B Observance of Manual Instructions 1 All personnel must carefully obey all safety quality operation and shop procedures for ...

Страница 34: ...nicians about the wiring installation and setup of every component of the Aspire 400 The installer is responsible for the approval and certification of system components on the aircraft and for the installation of wiring in the aircraft This manual includes information for end users about how to operate the Aspire 400 The Aspire 400 connects to the Inmarsat satellite network and provides data and ...

Страница 35: ...Honeywell Online Technical Publications Website at http www myaerospace com To download or see publications online To order a publication To tell Honeywell of a possible data error in a publication B Honeywell Aerospace Contact Team 1 If you do not have access to the Honeywell Technical Publications Website or if you need to speak to personnel about non Technical Publication matters the Honeywell ...

Страница 36: ...tps cage dla mil IEEE 315 ANSI Y32 2 Graphic Symbols for Electrical and Electronics Diagrams available from the American National Standards InstituteInstitute at http www ansi org 3 Acronyms and Abbreviations TASK 23 15 49 A General 1 The abbreviations are used in agreement with ASME Y14 38 2 Acronyms and non standard abbreviations used in this publication are as follows Table INTRO 2 List of Acro...

Страница 37: ...ated ASME American Society of Mechanical Engineers ASPIRE Aero Standard Peer Inspection Review Environment ATA Air Transport Association ATC Air Traffic Control ATE automated test equipment ATLAS abbreviated test language for all systems ATN Aeronautical Telecommunications Network ATS Air Traffic Services AWG American Wire Gage BGAN Broadband Global Area Network BITE Built In Test Equipment C Cels...

Страница 38: ...cuit Switched CSD cargo smoke detector DABC Dual BGAN Card DAC Digital to Analog Converter DAH Design Approval Holder DAL Design Assurance Level DHCP Dynamic Host Control Protocol DLNA Diplexer Low Noise Amplifier DSP Digital Signal Processor DPL detailed parts list EASA European Aviation Safety Agency ECO Engineering Change Order ECU electronic control unit EDI equipment designator index EEPROM E...

Страница 39: ...e HAS Hardware Accomplishment Summary HF High Frequency HGA High Gain Antenna HLD HPA LNA Diplexer HPA High Power Amplifier HW Hardware HAQM Honeywell Aerospace Quality Manual IDT Integrated Design Technology IP Internet Protocol IPDS Integrated Product Development Support ISDN Integrated Service Digital Network ISEDC Innovation Science and Economic Development Canada ISO International Standards O...

Страница 40: ...um Performance Standards NA Not Applicable NGSS Next Generation Satellite Services NXP NXP Semiconductors NHA next higher assembly NI numerical index No number OHM overhaul manual OMM overhaul maintenance manual OPR operation OPS operational program software OEM Original Equipment Manufacturer ORT Owner Requirements Table PN part number Pub publication PAH Production Approval Holder PDP Packet Dat...

Страница 41: ...Frequency RTCA Radio Technical Commission for Aeronautics SAE Society of Automotive Engineers SAS Software Accomplishment Summary SATCOM Satellite Communications SATDATA Satellite Data SATVOICE Satellite Voice SB service bulletin SBB Swift Broad Band SBD Short Burst Data SCI Software Configuration Index SCM SDU Configuration Module SCMP Software Configuration Management Plan SDIM System Descriptio...

Страница 42: ...d practices manual SRU shop replaceable unit TCCA Transport Canada Civil Aviation TPOS test programs and operational software TR temporary revision TSDP technical support and data package TPA Transmit Pre Amplifier U S A United States of America USMS United States Measurement System UUT unit under test UMTS Universal Mobile Telecommunications Service USIM UMTS Subscriber Identity Module VoIP Voice...

Страница 43: ...Flight Bag services A second channel for cabin voice and data services 3 The Aspire 400 contains three main components the HPA the SDU and the SCM 4 The Aspire 400 system consists of three main components the High Power Amplifier HPA the Satellite Data Unit SDU and the SDU Configuration Module SCM B Hardware Part Numbers 1 At the time of writing of this document the SATCOM Products were identified...

Страница 44: ...nal Inc Do not copy without express permission of Honeywell Page 1 2 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 1 1 Aspire 400 System Diagram D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 45: ...75 01 mm MAX Width 2 41 inches 61 2 mm MAX Height 7 88 Inches 200 2 mm MAX Mounting Information 2MCU Tray per ARINC 600 Weight 9 00 Lbs 4 08 Kg MAX Power Dissipation 240 W MAX Power Consumption 280 W MAX Operating Voltage 115 VAC Cooling UNIT IS DESIGNED TO OPERATE IN FORWARD O H CROWN DRAW THROUGH MEASURED AT THE BASE AIR FLOW OF 35 2 KG HR 77 60 LB HR AMBIENT PRESSURE OF 101 3 KPA 14 696 PSIA AI...

Страница 46: ...D5 interface 4 The L band Tx Power Amplification provides the primary function RF signal amplification Control for gain settings and activation is defined by ARINC 429 ID6 messaging from the SDU The RF performance functional health and operational status is continuously monitored and reported via ARINC 429 ID6 messaging back to the SDU In addition to enabling the ARINC 429 ID6 control and response...

Страница 47: ... Do not copy without express permission of Honeywell Page 1 5 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 1 2 High Power Amplifier HPA Block diagram D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 48: ...art of this process as well as interface routing The Dual Aeronautical BGAN Card provides two segregated channels B SDU Functions and Services 1 The Aspire 400 SDU provides SATVOICE and DATA using the Inmarsat extended L Band Swift Broadband service in support of the following categories of communications a Air Traffic Service ATS b Aircraft Operational Control AOC c Aeronautical Administrative Co...

Страница 49: ...nal Inc Do not copy without express permission of Honeywell Page 1 7 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 1 3 Aspire 400 Single Channel D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 50: ...DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 NOTE The above diagram is a logical representation of the SDU functions and interconnections and does not imply a direct mapping to the physical implementation D Application Mode Dual Channel Aspire 400 ACD AIS PIES Configuration D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 51: ...onal Inc Do not copy without express permission of Honeywell Page 1 9 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 1 4 Dual Channel Aspire 400 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 52: ...INC 600 Weight 8 00 Lbs 3 63 Kg MAX Power Dissipation 70 W MAX Power Consumption 60 W MAX Operating Voltage 115 VAC Cooling UNIT IS DESIGNED TO OPERATE IN FORWARD EBAY CABIN AND NON PRESSURIZED COMPARTMENT UNIT REQUIRES FORCE AIR COOLING AS FOLLOWS AIR FLOW OF 15 4 KG HR 34 0 LB HR AMBIENT PRESSURE OF 101 3 KPA 14 696 PSI AIR TEMPERATURE OF 40 C 104 F INTERNAL FAN USED DURING LOSS OF COOLING CONDI...

Страница 53: ...SDU and SCM Table 1 4 SCM Component Specifications Component Characteristic Specification SCM Part Number 90402652 000 Length 4 75 Inches 120 7 mm MAX Width 1 00 Inches 25 4 mm MAX Height 4 00 Inches 101 6 mm MAX Weight 0 50 Lbs 0 23 Kg MAX Power Dissipation 10 7 W MAX Power Consumption 16 W MAX Operating Voltage 18 VDC MAX Cooling PASSIVELY COOLED AND DOES NOT REQUIRE FORCED AIR THERE ARE NO INTE...

Страница 54: ...sing an Intermediate Gain Antenna IGA transceiver SDU SCM and HPA function and Diplexer Low Noise Amplifier DLNA Sub class 7F A 7F transceiver is defined as a transceiver unit capable of operating within an AES7 system which uses a DF diplexer and IGA It includes the SDU HPA and the SCM as shown in Figure 1 2 Block Diagram of an AES7 and its Major System Components B Honeywell SwiftBroadband Syste...

Страница 55: ...Inc Do not copy without express permission of Honeywell Page 1 13 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 1 5 Inmarsat Communications Overview D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 56: ...s SDU2 will operate on the Inmarsat network 4 Determination of the active and standby system is determined either by the crew or by an Aircraft algorithm outside the SATCOM The remainder of this document focuses on the Inmarsat portion of the SATCOM avionics suite The Inmarsat avionics equipment consists of an Aspire 400 Satellite Data Unit SDU the Aspire 400 SDU Configuration Module SCM and Aspir...

Страница 57: ...copy without express permission of Honeywell Page 1 15 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 1 6 AES Class 6 System Configuration Showing 6F Sub Class D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 58: ...copy without express permission of Honeywell Page 1 16 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 1 7 AES Class 7 System Configuration Showing 7F Sub Class D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 59: ... a Air Traffic Service ATS b Aircraft Operational Control AOC c Aeronautical Administrative Communication AAC and d Aeronautical Passenger Communications APC 2 The Aspire 400 Class 6F 7F Transceiver provides up to two Swift Broadband channels a A Swift Broadband safety channel for the following services b ACARS data Aircraft Communications Addressing and Reporting System c Voice two channels one C...

Страница 60: ...t copy without express permission of Honeywell Page 1 18 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 1 8 Block Diagram of an AES6 and its Major Components D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 61: ...2 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 E AES sub class 7F 1 Due to this application being a sub class 7F no DLNA or HGA data will be provided NOTE The modem in Figure 1 9 includes the function of the SDU and the SCM D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 62: ...opy without express permission of Honeywell Page 1 20 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 1 9 Block Diagram of an AES7 and its Major System Components D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 63: ...o support both classes of operation The class of operation is determined by SDU configuration settings contained in a Secure Owner Requirement Table ORT File 2 ORT files are used to identify aircraft specific configurations and have a unique part number associated with each file created These files are created and their associated part numbers are created by the air framer or end user using the OR...

Страница 64: ...l International Inc Do not copy without express permission of Honeywell Page 1 22 22 Apr 2019 23 15 49 Blank Page SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 65: ...ere the SDU then boots up and begins validation a If the validation fails then the system begins a safe power shut down 1 Data load command signal will begin a load progress reset 2 SDU configuration or ORToperation software must be fixed 3 The SDU will then have the option for several tests and checks a Maintenance Test Command which places the system in Aircraft Test Mode once finished the syste...

Страница 66: ...tional Inc Do not copy without express permission of Honeywell Page 2 2 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 2 1 Modes of Operation D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 67: ... a license b SDU configuration incomplete c SDU configuration discrepancy or corruption d SATCOM LRU configuration discrepancy antenna or PA type mismatch 3 Upon entry into RF Safe Mode the SDU keeps the RF carrier off 4 When in Safe Mode the SDU indicates its inability to provide data and voice services on the following interfaces which are able to be activated a Pilot control and display b CMU 5...

Страница 68: ...e accounts for Inmarsat System per carrier gain adjustment 10 dB Antenna reporting gain range 8 dB AES system gain adjustments to overcome gain tolerance 2 dB Tx RF Input Damage Level The HPA meets the transmit performance requirements after exposure to a total average input power of 20 dBm Tx RF Load VSWR Capability The HPA does not sustain permanent damage if operated continuously at full output...

Страница 69: ...lowing definition of Tx carriers apply a Reference signal generator will be set for the following setup conditions b Data Source PN c Repeat Continuous d Phase Polarity Normal e Differential Data Encoding Off 2 The modulation characteristics for the applicable bearer type are shown in Table 2 2 where Channel Bandwidth is the Necessary Bandwidth Table 2 2 Modulation Characteristics Multiplier Modul...

Страница 70: ...is held in the disabled state the HPA net Tx gain capability Tx input port to Tx output port is 20 dB under conditions of 0 dB input attenuator back off C Tx Frequency Response 1 The Tx band gain tolerance as assessed from the transmit port input to the transmit port output is less than 1 dB peak to peak under conditions of a PA function is enabled b Any output level as achieved from a correspondi...

Страница 71: ... dB d A carrier signal s of carrier rated power and a system applicable modulation e Limit assessment at frequency offset greater than 70 dBc intercept relaxed to 70 dBc f dBe limits expressed in relative power with respect to the carrier power measured in the same bandwidth NOTE Allocation Case I is 2 5 dB more stringent than Inmarsat system specification G Intermodulation Products in the Tx band...

Страница 72: ...ne performance for both in band narrow spurious and broadband spurious If narrow band spurious are present they should not form part of the Broadband noise compliance 2 Tx in band spurious 1626 5 MHz to 1660 5 MHz defined elsewhere C Spurious Outside of Tx band When No Carrier Present 1 Under conditions of no carriers present at the input and with the PA function enabled the out of Tx band spuriou...

Страница 73: ... 1000 Modulated ETSI Above Tx band to 1762 5 7 1728 5 to 1762 5 81 1000 Modulated ETSI Above Tx band to 3400 9 1762 5 to 3400 81 1000 Modulated ETSI Above Tx band 3400 9 3400 to 18000 80 CW DO 210 NOTES 1 Modulated carriers must have unique test sequences from each other 2 On aircraft equipped with Glonass 5th order IM control algorithm limiting carriers no more than 30 MHz of carrier separation m...

Страница 74: ... hold the PA function as disabled a Power interruption exceeds the transparency time b Upon power up and until the first ARINC 429 Label 143 HPA Command Word received with the state of indication of PA Control identified as Carrier ON c Over temperature exceeding critical level d Fault conditions of the HPA preclude operation e The HPA is executing a Self Test f The detection of a single event ups...

Страница 75: ...that is readable by software Persistent means by hardware or manufacturer reserved memory that cannot be overwritten by application reload The software reported PA Backoff Range is Input Attenuator Maximum Attenuation Capability 16 computed in dBs and expressed in 4 bits The reportable attenuator maximum attenuation capability is therefore limited to a range of 16 0000 to 31 1111 3 The state of in...

Страница 76: ...function 2 Within the measurement reporting tolerance the sample of input power is not affected by the enable disable state of the PA function 3 The sample of input power is implemented with a directivity 20 dB 4 The input power detector function that assesses the sample of input power is able to measure signals in a logarithmic response over the input dynamic range with an accuracy of less than 0...

Страница 77: ...input sample be 30 dBm in the reporting interval then the Actual Power Out Status status is reported as Actual Power in ARINC 429 label 143 HPA Status word 8 Controller Functions A Single Event Upset 1 The HPA is ruggedized against Single Multiple Event Upset 2 Implementation may employ redundant memory error correcting hardware memory software correction encoding or other suitable techniques in a...

Страница 78: ...l RAM is detected and confirmed as compromised then the following occurs for as long as the RAM is compromised a The state of indication of Internal RAM Integrity in ARINC 429 label 350 HPA Maintenance word is declared as RAM Fault b Failure Warning is identified as a ARINC 429 word SSM reportable condition of the HPA c While Failure Warning persists as the ARINC 429 word reportable condition for ...

Страница 79: ...n GREEN e As a minimum Off line Self Test should perform the following tests 1 CRC verification of integrity of application RAM and supporting software modules in RAM 2 CRC verification of integrity of application in ROM 3 The integrity of the power supply function 4 Fault evaluation of Temperature sensors 5 ARINC 429 receive communication integrity 6 Invasive ARINC 429 loopback verification 7 The...

Страница 80: ...1 The HPA does not react to ARINC 429 label 143 HPA Command word if a The computed parity of the Word is not Odd b The Source Destination ID SDI is other than All Call or HPA 2 The HPA does not apply parameter information of the ARINC 429 label 143 HPA Command word if a The SSM identifies Failure Warning FW of the LRU of the sourced information b The SSM identifies No Computed Data NCD of the sour...

Страница 81: ...g No Computed Data Detector as a ARINC 429 word SSM reportable condition of the HPA to be applied to ARINC 429 label 357 Aero Power word until identified otherwise b Recording the occurrence of deassertion to the Event log B HPA Status Word ARINC 429 Label 143 1 The HPA assigns the state of indication of the various Indicators that define the ARINC 429 label 143 HPA Status word format in accordanc...

Страница 82: ...ncurrent displays connected via the MCDU interfaces activated by ORT 2 The Cockpit Control and Display provides synchronized display fields across all displays when the same menu page is selected except for the scratchpad B Wire Voice Control and Display Functions 1 This section describes the essential 4 wire voice control and display elements 2 The 4 Wire Voice Control and Display a Allows each d...

Страница 83: ...Display NOTE SATCOM Select Modes are SDU1 SDU2 or Auto b The SDU displays if it is currently the Active or Standby SATCOM via the Cockpit Control and Display c The SDU allows user to set SATCOM Select Mode via the Cockpit Control and Display E MCDU Type Cockpit Display Functions 1 The MCDU type cockpit display pages are rendered by the SDU 2 The MCDU type 4 Wire Voice Control and Display permits a...

Страница 84: ... only one SDU b Dual Safety SATCOM 2 SDUs interconnected but only one can be active and logged onto safety services at any one time 2 If the SDU Dual System Disable DSD discrete is asserted the SDU a Silently Logs off if already logged on b Disables its RF transmission c De asserts its Dual System Select DSS NOTE This applies for all configurations B Standalone Configuration 1 In Standalone Config...

Страница 85: ...c Do not copy without express permission of Honeywell Page 2 21 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 2 2 Dual SATCOM Standalone Configuration D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 86: ...onsiders itself as SDU in coverage when a SDU can see a satellite that has elevation angle 4 degrees 5 When ORTconfigured for Dual Safety SATCOM on entering the Active state the SDU a Asserts its DSS discrete before enabling RF transmission this will assert the companion SDU DSD discrete b Enables its RF transmission c Sets Bit 18 of Label 270 SDU ACARS MU CMU Status Word to 0 d Continues to asser...

Страница 87: ... copy without express permission of Honeywell Page 2 23 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 c Labels 272 and 274 on the Data from MDCU 1 2 or 3 interfaces D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 88: ... Inc Do not copy without express permission of Honeywell Page 2 24 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 2 3 Dual SATCOM Dual Configuration D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 89: ...alid from MCDU 1 then MCDU 3 when Label 272 is missing invalid from both MCDU 1 2 g The ACD keeps the ACDir Select Mode unaltered when all the following are true 1 SSM of Label 272 is set to FT 2 Bits 12 11 Operational Mode Command is 01b SDU1 Active SDU2 Standby or 10b SDU2 Active SDU1 Standby in Label 272 Operational Mode Command Word that is being used NOTE The priority is to use Label 272 from...

Страница 90: ...either of the following occur 1 The SDU is logged onto an Inmarsat satellite 2 The SDU has transitioned to the Standby mode p The SDU sets bit 13 of Label 274 SATCOM OCA Interface Status to 0 when 1 ORTconfigured for Aircraft Directed Dual Safety SATCOM 2 The SDU has logged off due to a manual command from the pilot 3 The SDU sets bit 13 of Label 274 SATCOM OCA Interface Status to 1 E Electronic U...

Страница 91: ...ent c SDU vendor information d SDU function e SDU short name f The TAC code portion of the IMEI g The SVN portion of the IMEI h The Serial Number portion of the IMEI 7 On startup of the SB safety Voice Service the ACD retrieves the Channel Card Side A USIM IMSI and the IMEI from the Safety Channel card 8 On startup of the SB safety Voice Service and if Side B is ORTenabled the ACD retrieves the Ch...

Страница 92: ...e ORT to be present b Distinguishing between the absence of configuration data due to non support of configuration reporting of the remote LRU and expected but missing data 1 Dashes have previously been used for expected but unavailable information 2 It may not always be known by ORT if an LRU supports configuration reporting however it can be inferred if other receive BITE information present but...

Страница 93: ...e to logon to each satellite 2 Each row of the table contains data for one satellite and includes a Satellite id b Satellite name c Satellite region d Satellite position e SBB PSAB Frequencies 3 When there is no valid non volatile stored ACD copy of the Satellite Table the ACD synchronizes the ACD stored copy to the values from the ORT Satellite Table on the SCM 4 The ACD updates its non volatile ...

Страница 94: ...ted channel call light discrete set to LOW d The ACD 1 Asserts the associated SATCOM Voice Call bits based on 4 wire interface and priority of the call in SDU to CMU Label 270 Channel 1 2 Alert bits are 24 25 respectively for P4 calls Channel 1 2 Call bits are 22 23 respectively for P1 2 3 calls 2 Asserts SELCAL bit 14 in SDU to CMU Label 270 B Air to Ground Call Direction 1 Whenever a 4 wire call...

Страница 95: ...he SDU accepts control inputs from a Cockpit Voice Mic On Discrete b Call Place End discrete c Call display and control protocol e g via MCDU 2 The SDU supports two modes of call control a Latched Bidirectional audio path is present while the call is connected b Push to talk call Air to Ground audio only present when call is connected and the Mic is activated E Ground to Air Call Decision NOTE Thi...

Страница 96: ... not copy without express permission of Honeywell Page 2 32 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 2 4 Sheet 1 of 2 Incoming PS Call Decision Logic D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 97: ... not copy without express permission of Honeywell Page 2 33 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 2 4 Sheet 2 of 2 Incoming PS Call Decision Logic D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 98: ... a ground to air annunciated call enter CONNECTED state on any of the following conditions a ANSWER CALL command received on the call display and control protocol b The first transition of the associated Cockpit Voice Mic On Discrete 4 In PTT mode when a call is CONNECTED the ACD a Activates cockpit microphone when the associated Cockpit Voice Mic On discrete is on and b Mutes the cockpit micropho...

Страница 99: ...ir to Ground calls to unused connections in the following order a The AMBE 2 CS connection b VoIP over PS connection 2 Based on ORTconfiguration PS or CS Ground to Air call requests of public priority is a Rejected b Routed to the 4 wire interfaces NOTE The ORTconfiguration settings are mutually exclusive 3 The ACD PBX routes Ground to Air calls to 4 wire interfaces as follows a To ORT defined 4 w...

Страница 100: ...k or Safety Logon attempt have failed then reject the call 5 If informed by the Channel Card that any of the following activations triggered by the Safety voice CS initiation has failed a The eMLPP registration b Call waiting activation the ACD continues to service voice calls NOTES 1 Absence of eMLPP will prevent sending the priority field 2 Absence of call waiting will prevent the new call from ...

Страница 101: ...text 3 With the specified TFTand if successful a Activate by sending a SIP INVITE to the SIP server with b MSISDN as the calling party 4 If unsuccessful terminate the call by a Indicating call failure to user b Commanding the Channel Card to terminate the Secondary context NOTE No Session Description Protocol SDP offer is required in the SIP INVITE message for A2G initiated calls b The ACD PBX pop...

Страница 102: ... Inertial Data and are given priority accordingly b Navigation information is shown in Table 2 6 Table 2 6 Navigation Data Description Priority Labels Aircraft Position 1 254 Latitude Hybrid 255 Longitude Hybrid 2 110 Latitude GNSS 111 Longitude GNSS 3 310 Present Position Latitude INS 311 Present Position Longitude INS Ground Speed 1 175 Ground Speed Hybrid 2 112 Ground Speed GNSS 3 312 Ground Sp...

Страница 103: ...or co packaged HPA b Standalone or co packaged DLNA c Gain of antenna d Type of antenna e Number of Antenna f Control Interfaces 2 The RF configuration items are generally ORTspecified but in some cases such as type of antenna they may also be communicated by the Antenna 3 The ACD manages the EIRP of each RF carrier to the level associated with the ORT identified terminal class 4 Based on ORTsetti...

Страница 104: ... entered when ACD Application code begins executing No User services are available as Application Mode has not yet been selected The SDU Configuration and Test Mode includes a ORTand license validation b Configuring the SDU based upon strapping ORTsettings and licenses c Executing SDU startup and invasive tests d Transitioning to data load mode if a data load is in progress B SATCOM System Configu...

Страница 105: ...A Time and Date 1 The SDU uses Time and Date for a Timestamping messages to the CFDS b Timestamping log entries c Assessing validity of PIMBIT test frequencies 2 On start up the internal clock is set to a default time and date Thus prior to synchronizing to an external source it only represents a time relative to start up 3 The SDU also stores snapshots of the Network Date for a Assessing validity...

Страница 106: ...set 4 Satellite handover 5 Manual logoff B Operational Air Ground Status 1 Operational Air Ground Status is used to prohibit or abort ground maintenance operations when the aircraft is in the air Examples of applicable ground maintenance operations are a Execution of full versus rapid POST b Data Loading c Commanded Self Test d Execution of PIMBIT 2 Operational Air Ground Status is also sent to th...

Страница 107: ...ternary Valid Ground Speed 40 KTS On Ground Ground Speed Ground Speed 40 KTS In Air Invalid or Unavailable On Ground NOTE In the future the default when the Ground Speed is invalid or unavailable i e when all fails could be defined as an ORT parameter containing the default state C Temperature Profile 1 In application mode the SDU maintains a temperature profile histogram in non volatile memory wh...

Страница 108: ...st two valid and matching ICAO address labels received after power up on the ground is stored in non volatile memory and used until the next on ground power up NOTE If present the stored ICAO is used after in air power ups 4 The SDU considers any of the following ICAO addresses invalid a All zeros 0b b All ones 1b c ARINC 429 ICAO words with parity errors NOTE The SSM field has intentionally not b...

Страница 109: ...d copy of User ORT data only and not to the SCM USER ORTcopy C License Keys 1 License keys are installed in the SCM and activate optional SDU features License keys can be viewed and updated via the appropriate Maintenance Access Levels 2 The ACD stores licenses on the SCM 3 Each licensed feature that has specific CAN TSO functionality is associated with a secure ORT item and has no expiry date D L...

Страница 110: ... feature set ARINC 781 ORT items not covered include a Items for which only one value is applicable so option selection is not required b Items that do not apply e g items relating to Classic or Swift 64 operation 3 The Aspire 400 ORTs also include additional parameters for the Aspire 400 feature set that are described ARINC 781 4 The ARINC 781 ORT items that are not applicable are explicitly list...

Страница 111: ... ORT 8 The PIESD ensures that all PIESD ORT parameters are assigned to the Secure ORT F Satellite Table 1 The ACD ensures the ORTcontains the following information for up to 16 satellites a Satellite identity b Name c Position d Priority e SBB global beam frequencies G SBB Safety Data 1 The ACD ensures the ORTcontains the following parameters for SBB Safety Data configuration a AAP Position Report...

Страница 112: ...D 1 Enable 2 Disable c 4 wire 1 Connectivity 2 Preferred routing for Ground to Air Calls d Cockpit headset parameters 1 Audio level 2 Mic level 3 Side tone level e Hook switch operation 1 Latched 2 PTT f Call Pre Select g Call Discretes 1 Alternate behavior 2 Standard behavior 2 There is no requirement to support the following as an ORTconfigurable item a Phone number preset A781 Ref D8 MAKE CALL ...

Страница 113: ...ss permission of Honeywell Page 3 5 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 b SDU codec 1 dedication A781 Ref D1 always services cockpit voice c Dual SATCOM Voice Channel Mapping D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 114: ...ll International Inc Do not copy without express permission of Honeywell Page 3 6 22 Apr 2019 23 15 49 Blank Page SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 115: ... of SATCOM communication is less than 9 376E 5 per FH c There is no scheduled maintenance with the exception of INMARSAT required scheduled activities such as PIMBIT d There is a failure rate of less than 2 5E 6 per FH on all input power bus components that are not protected though short circuit topology e There is a failure rate of less than 2 5E 8 per FH on each ARINC 429 receive interface resul...

Страница 116: ... caution symbol with bold upper case letters to identify that they contain high voltage components NOTE An acceptable phrasing is WARNING 250 V d The SDU has a triangular Field Loadable Software warning label with bold upper case letters NOTES 1 An acceptable phrasing is CAUTION THIS EQUIPMENT REQUIRES FIELD LOADABLE SOFTWARE ENSURE CORRECT SOFTWARE IS LOADED REFER TO AMM 2 The label should be vis...

Страница 117: ...not copy without express permission of Honeywell Pages 4 3 4 4 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 4 1 Sheet 1 of 3 HPA Outline and Installation D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 118: ...D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 119: ...not copy without express permission of Honeywell Pages 4 5 4 6 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 4 1 Sheet 2 of 3 HPA Outline and Installation D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 120: ...D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 121: ...not copy without express permission of Honeywell Pages 4 7 4 8 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 4 1 Sheet 3 of 3 HPA Outline and Installation D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 122: ...D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 123: ...nc Do not copy without express permission of Honeywell Pages 4 9 4 10 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 4 2 SCM Outline and Installation D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 124: ...D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 125: ...ot copy without express permission of Honeywell Pages 4 11 4 12 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 4 3 Sheet 1 of 2 SDU Outline and Installation D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 126: ...D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 127: ...ot copy without express permission of Honeywell Pages 4 13 4 14 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 4 3 Sheet 2 of 2 SDU Outline and Installation D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 128: ...D R A F T 3rd rvw Draft as of 29 January 2020 ...

Страница 129: ... Size 1 Coax c J1 C 4X 20 Contacts 3X 16 Contacts 4X 12 Contacts 2X 5 Contact C SCM Installation 1 Power Requirements a The SCM system runs on 18 VDC with a maximum power consumption of 16 W and has a maximum power dissipation of 10 7 W 2 Interfaces a 15 Position D SUB Plug MALE TE 5745908 2 D SDU Installation 1 Power Requirements a The SDU system runs on 115 VAC with a maximum power consumption o...

Страница 130: ...o not copy without express permission of Honeywell Page 4 16 22 Apr 2019 23 15 49 SYSTEM DESCRIPTION INSTALLATION AND MAINTENANCE MANUAL ASPIRE 400 Figure 4 4 ARINC 600 Receptacle with Index Pin Coding D R A F T 3rd rvw Draft as of 29 January 2020 ...

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