Page 1 U.S. government or as otherwise authorized by U.S. law and regulations. ECCN: 7E994. 23-15-49 Page T-1 Publication Number D201902000020, Revision 0 Initial 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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Page 3 U.S. Government. You may not design or manufacture a Honeywell part or detail of a Honeywell part, to create a repair for a Honeywell part, design or manufacture any part that is similar or...
Page 4 LIFE OF THE COMPONENTS. INCORRECTLY FABRICATED SPECIAL TOOLING OR TEST EQUIPMENT CAN RESULT IN DAMAGE TO THE PRODUCT COMPONENTS OR GIVE UNSATISFACTORY RESULTS. 23-15-49 Page T-4 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 5 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. 23-15-49 Page T-5 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Blank Page 23-15-49 Page T-6 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 7 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 TRANSMITTAL INFORMATION TO 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...
Page 8 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Blank Page EFFECTIVITY 23-15-49 Page TI-2 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 9 Refer to the Revision History in the TRANSMITTAL INFORMATION section for revision data. Revision Revision Date Put in Revision Revision Date Put in Number Date Manual Number Date Manual EFFECTIVITY 23-15-49 Page RR-1 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 10 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Blank Page EFFECTIVITY 23-15-49 Page RR-2 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 11 TR has been deleted. Date Date Temporary Removed Revision Page Issue From Number Status Number Date Manual Manual EFFECTIVITY 23-15-49 Page RTR-1 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 12 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Blank Page EFFECTIVITY 23-15-49 Page RTR-2 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 13 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 SERVICE BULLETIN LIST Service Bulletin / Date Put In Revision Number Title Modification Manual EFFECTIVITY 23-15-49 Page SBL-1 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 14 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Blank Page EFFECTIVITY 23-15-49 Page SBL-2 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 15 22 Apr 2019 TOC-3 1-10 22 Apr 2019 TOC-4 22 Apr 2019 Indicates a changed or added page. Indicates a foldout page. EFFECTIVITY 23-15-49 Page LEP-1 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 16 22 Apr 2019 22 Apr 2019 2-17 22 Apr 2019 22 Apr 2019 Indicates a changed or added page. Indicates a foldout page. EFFECTIVITY 23-15-49 Page LEP-2 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 17 22 Apr 2019 4-35/4-36 22 Apr 2019 5-23 22 Apr 2019 Indicates a changed or added page. Indicates a foldout page. EFFECTIVITY 23-15-49 Page LEP-3 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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Page 19 22 Apr 2019 22 Apr 2019 22 Apr 2019 A-10 22 Apr 2019 Indicates a changed or added page. Indicates a foldout page. EFFECTIVITY 23-15-49 Page LEP-5 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 20 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Blank Page EFFECTIVITY 23-15-49 Page LEP-6 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 21: Table Of Contents
2 Modes of Operations ........................2-1 Modes of Operation Transition Path ..................2-1 RF Safe Mode .........................2-3 3 HPA Modes of Operations .........................2-3 General ...........................2-3 EFFECTIVITY 23-15-49 Page TOC-1 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 22 G SBB Bulletin Board and Satellite Table ..................2-29 13 Standard Call Discretes (TASK 23-15-49) ..................2-30 Ground to Air - Call Direction ....................2-30 EFFECTIVITY 23-15-49 Page TOC-2 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 23 HPA/SDU Installation .......................4-1 SCM Installation ........................4-1 Design and Construction ......................4-1 Miscellaneous .........................4-1 Engineering Drawings ......................4-2 2 Electrical Installation (TASK 23-15-49) ....................4-15 General ..........................4-15 EFFECTIVITY 23-15-49 Page TOC-3 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 24 Security Gateway Functions (SecGW) ..................5-8 PKI Certificate Check .......................5-8 PKI Certificate Request ......................5-9 Safety Voice Services ......................5-9 5 AISD / PIESD Processor (APP) .......................5-10 EFFECTIVITY 23-15-49 Page TOC-4 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 25 Type 1 Configuration Report Format ..................5-39 G Receiving Command Label .....................5-41 CFDS Commanded Self-Test ....................5-41 Shop Fault Reporting ......................5-41 13 Navigation System Interfaces ......................5-41 EFFECTIVITY 23-15-49 Page TOC-5 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 26 RF Carrier Test ........................6-16 G Historical Log Retrieval ......................6-17 Faults and Events ........................6-17 Fault and Event Annunciation ....................6-18 POST Fault and Event Monitoring ...................6-18 EFFECTIVITY 23-15-49 Page TOC-6 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 27 Applicable Documents ......................A-3 2 Standards and Specifications ......................A-3 Military Standards and Specifications ..................A-3 Federal Aviation Administration ....................A-3 EFFECTIVITY 23-15-49 Page TOC-7 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 28 9 Certification Requirements (TASK 23-15-49) ..................A-12 Design Assurance Levels ...................... A-12 10 Other Considerations ........................A-12 TCCA Advisory Circulars ....................... A-12 Radio Transmission Licensing ....................A-12 EFFECTIVITY 23-15-49 Page TOC-8 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 29 AISD ARINC Swift MIB Entry Point..................5-14 Call Annunciation State Machine..................5-34 Configuration Report Format ....................5-40 Web GUI Login Page ......................6-5 ACD Boot Stages.......................7-2 EFFECTIVITY 23-15-49 Page TOC-9 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 30 ACP Transmit/Recieve Codes ..................5-55 Service Descriptions of Syslog Messages Formatted by ACD ..........6-2 Group Descriptions and Associated PRI Sections of Message Groups........6-3 EFFECTIVITY 23-15-49 Page TOC-10 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 31 Priority "Non-Safety Logon State" Description ..............7-5 Environmental Conditions and Test Procedures ..............A-4 TCCA CAN-TSOs for the Aspire 400 .................. A-9 Planned CAN-TSO submittals..................A-10 EFFECTIVITY 23-15-49 Page TOC-11 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 32 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Blank Page EFFECTIVITY 23-15-49 Page TOC-12 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 33: Introduction
The signal names followed by an "*" show an active low signal. The symbols in Figure 1-1 show non-ionizing radiation hazard, ESDS, and moisture sensitive devices. EFFECTIVITY 23-15-49 Page INTRO-1 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 34: Units Of Measure
Scope This manual provides detailed information for avionics technicians 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.
Page 35: Organization
– To tell Honeywell of a possible data error in a publication Honeywell Aerospace Contact Team 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 Aerospace Contact Team gives 24/7 customer service to Air Transport &...
Page 36: General
Airborne Electronic HW Aeronautical Earth Station Aerospace Guidance Aircraft Information System AISD Aircraft Information Systems Domain AMBE Advanced Multiband Excitation Advanced Micro Devices EFFECTIVITY 23-15-49 Page INTRO-4 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 37 Conference of European Postal and Telecommunication-European 1 (2048 bps, 30- channel PCM) CFDS Central Fault and Display System Code of Federal Regulation EFFECTIVITY 23-15-49 Page INTRO-5 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 38 Electrically Erasable Programmable Read-Only Memory Electro-Magnetic Interference EMS Technologies electrostatic discharge sensitive ESDS Fahrenheit FANS Future Air Navigation System Federal Communications Commission Functional Hazard Assessment EFFECTIVITY 23-15-49 Page INTRO-6 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 39 Institute of Electrical and Electronics Engineers illustrated parts catalog illustrated parts list kilopascal line replaceable unit LODA Letter of Deviation Authority manufacturer EFFECTIVITY 23-15-49 Page INTRO-7 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 40 Plan for Hardware Aspects of Certification PIES Passenger Inflight Entertainment Service PIESD Passenger Inflight Entertainment Domain PPPoE Point-to-Point Protocol over Ethernet Packet Switched EFFECTIVITY 23-15-49 Page INTRO-8 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 41 Single Event Upset Serial Interface Protocol SITA Société Internationale de Télécommunications Aéronautiques Stage of Involvement System Safety Assessment Supplemental Type Certificate Software EFFECTIVITY 23-15-49 Page INTRO-9 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 42 UMTS Universal Mobile Telecommunications Service USIM UMTS Subscriber Identity Module VoIP Voice over IP WACO Wichita Aircraft Certification Office eXtended L-Band EFFECTIVITY 23-15-49 Page INTRO-10 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 43: System Description
Reporting System), Cockpit voice, Position Reporting and AIS Electronic Flight Bag services. A second channel for cabin voice and data services. The Aspire-400 contains three main components, the HPA, the SDU, and the SCM. 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).
Page 44 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 1-1. Aspire 400 System Diagram EFFECTIVITY 23-15-49 Page 1-2 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 45: Hpa Description (Task 23-15-49)
J1-B (70X #22 Contacts, 1X Size 1 Coax) J1-C (4X #20 Contacts, 3X #16 Contacts, 4X #12 Contacts, 2X #5 Contacts) System Requirements RTCA/DO-160G EFFECTIVITY 23-15-49 Page 1-3 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 46 Power Amplification through activation/deactivation current profile sequencing and continuous gain optimization. A high level block diagram is shown in Figure 1-2. EFFECTIVITY 23-15-49 Page 1-4 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 47 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 1-2. High Power Amplifier (HPA) Block diagram EFFECTIVITY 23-15-49 Page 1-5 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 48: Sdu System (Task 23-15-49)
Application Mode: Single Channel Aspire 400 ACD/AIS Configuration The following figures are provided to show the interconnection between the Aspire 400 and other aircraft systems and services. EFFECTIVITY 23-15-49 Page 1-6 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 49 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 1-3. Aspire 400 Single Channel EFFECTIVITY 23-15-49 Page 1-7 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 50: Application Mode: Dual Channel Aspire 400 Acd/Ais/Pies Configuration
The above diagram is a logical representation of the SDU functions and interconnections and does not imply a direct mapping to the physical implementation. Application Mode: Dual Channel Aspire 400 ACD/AIS/PIES Configuration EFFECTIVITY 23-15-49 Page 1-8 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 51 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 1-4. Dual Channel Aspire 400 EFFECTIVITY 23-15-49 Page 1-9 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 52: Sdu System Characteristics
The SCM provides memory for storage of ORT files and licenses, USIMs needed for SBB network access and a Security Smart card that is needed for Safety service EFFECTIVITY 23-15-49 Page 1-10 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 53: Scm System Characteristics
This plan includes schedule information for each of the applications. These classes are detailed in the Table 1-5 Equipment Class and Subclass Identification: EFFECTIVITY 23-15-49 Page 1-11 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 54: Honeywell Swiftbroadband System Overview
GDGW (Ground Datalink Gateway) Safety Voice. The Basic configuration of the Network in relation to aircraft user terminal functionality is depicted in Figure 1-5: EFFECTIVITY 23-15-49 Page 1-12 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 55 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 1-5. Inmarsat Communications Overview EFFECTIVITY 23-15-49 Page 1-13 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 56 Module (SCM), and Aspire 400 High Power Amplifier (HPA) installed in the crown area, together forming the 6F transceiver. A Type F DLNA and HGA complete the AES. EFFECTIVITY 23-15-49 Page 1-14 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 57 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 1-6. AES Class 6 System Configuration Showing 6F Sub-Class EFFECTIVITY 23-15-49 Page 1-15 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 58 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 1-7. AES Class 7 System Configuration Showing 7F Sub-Class EFFECTIVITY 23-15-49 Page 1-16 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 59: Aes Class 6/7 Functions And Services
Due to this application being a sub-class 6F, no DLNA or HGA data will be provided. NOTE: The modem in Figure 1-8 includes the function of the SDU and the SCM. EFFECTIVITY 23-15-49 Page 1-17 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 60 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 1-8. Block Diagram of an AES6 and its Major Components EFFECTIVITY 23-15-49 Page 1-18 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 61: Aes Sub-Class 7F
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. EFFECTIVITY 23-15-49 Page 1-19 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 62 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 1-9. Block Diagram of an AES7 and its Major System Components EFFECTIVITY 23-15-49 Page 1-20 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 63: Commonality Across Classes
These files are created and their associated part numbers are created by the air framer or end user using the ORT creation tool. EFFECTIVITY 23-15-49 Page 1-21 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 64 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Blank Page EFFECTIVITY 23-15-49 Page 1-22 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 65: System Operation
Figure 2-1 provides an understanding of the modes of operation and the possible transitions between the different modes. EFFECTIVITY 23-15-49 Page 2-1 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 66 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 2-1. Modes of Operation EFFECTIVITY 23-15-49 Page 2-2 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 67: Rf Safe Mode
The HPA operates as a means of transmitting RF signal between the SDU and antenna. The HPA supports the following modes: L-band Tx RF Power Amplification Processor RF Power Management and Diagnostics. EFFECTIVITY 23-15-49 Page 2-3 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 68: Tx Rf Modes Of Operation
2:1 VSWR circle is: EFFECTIVITY 23-15-49 Page 2-4 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 69: Tx In-Band (L-Band) Performance
100 kHz 16-QAM 84 ksym/s 16-QAM 0.25 151.2 ksym/s 189 kHz 200 kHz 16-QAM 0.13 168 ksym/s 189.8 kHz 200 kHz EFFECTIVITY 23-15-49 Page 2-5 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 70: Tx Gain
Burst period of 20 ms. Rated output power carrier level Carrier is modulated by 64-QAM with the permitted characteristics Constant temperature EFFECTIVITY 23-15-49 Page 2-6 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 71: E Tx Evm
A carrier signal of 5 dB less than maximum carrier-rated power and a system applicable modulation 17 dBi antenna gain EFFECTIVITY 23-15-49 Page 2-7 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 72: Tx Noise Figure
Port of a Type F diplexer connected in-line with the Tx output port incurring a net loss of 2.5 dB at midband is no greater than the performance limits as expressed in Table 2-3: EFFECTIVITY 23-15-49 Page 2-8 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 73: Harmonics Above The Tx-Band (>1670 Mhz)
Tx output port referenced harmonics is less than the following limits over the respective frequency range when used with Type F Diplexer and 1.4 dB of coax interconnecting cable shown in Table 2-4: EFFECTIVITY 23-15-49 Page 2-9 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 74: Rf Monitoring And Control
Receipt of ARINC-429 Label 143 HPA Command Word "PA control" set to "Carrier Off" Presence of any inhibitions complying the PA function to be disabled. EFFECTIVITY 23-15-49 Page 2-10 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 75: Input Attenuator
"Output Level" reported in ARINC-429 label 357 Aero Power word "Relative Power" reported in ARINC-429 label 143 HPA Status word EFFECTIVITY 23-15-49 Page 2-11 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 76: Input Power Detector Function
For purposes of conveyance in ARINC-429 label 357 Aero Power word, the computed average input level in dBm over the interval is expressed as a binary number in accordance with the following formulation: EFFECTIVITY 23-15-49 Page 2-12 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 77: Controller Functions
Declares the detection as an inhibition cause to the PA function. Immediately latches the Reset Reason register corresponding to "Single Event Upset". EFFECTIVITY 23-15-49 Page 2-13 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 78: Self Test
PA function being enabled will not be possible. Awareness and interaction to other AES system components is maintained. EFFECTIVITY 23-15-49 Page 2-14 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 79 At the completion of functional test the following actions occur: "Functional Test" is no longer identified as a ARINC-429 word SSM reportable condition of the HPA EFFECTIVITY 23-15-49 Page 2-15 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 80: Arinc 429 Messaging
No longer identifying "No Computed Data" (Command) as a ARINC-429 word SSM reportable condition of the HPA to be applied to ARINC-429 label 143 HPA Status word until identified otherwise EFFECTIVITY 23-15-49 Page 2-16 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 81: Hpa Status Word - Arinc 429 Label 143
SDU Modes of Operations Power-On Mode Power-On Mode is entered when power is applied to the SDU and is responsible for: EFFECTIVITY 23-15-49 Page 2-17 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 82: External System Interfaces
Allows the user to modify a pre-set or default priority state and to cycle through the following when placing an air-to-ground call using any ORT enabled display: From Emergency High High EFFECTIVITY 23-15-49 Page 2-18 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 83: Satellite Logon Control And Display Functions
Incorrect entries may be fixed by loading a correct one over top of an existing one. Dual SATCOM Configuration Master Control EFFECTIVITY 23-15-49 Page 2-19 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 84: Standalone Configuration
This applies for all configurations. Standalone Configuration In Standalone Configuration, the SDU is always the active SDU, no other SDU is considered. EFFECTIVITY 23-15-49 Page 2-20 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 85 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 2-2. Dual SATCOM Standalone Configuration EFFECTIVITY 23-15-49 Page 2-21 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 86: Dual Safety Satcom (Warm Standby)
Communication and control of the SDU in an Aircraft Directed Dual Safety SATCOM Configuration are via: Dual System Disable (DSD) Dual System Select (DSS) EFFECTIVITY 23-15-49 Page 2-22 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 87 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Labels 272 and 274 on the "Data from MDCU 1, 2 or 3" interfaces. EFFECTIVITY 23-15-49 Page 2-23 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 88 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 2-3. Dual SATCOM Dual Configuration EFFECTIVITY 23-15-49 Page 2-24 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 89 That SDU transitions to Standby state when the ORT configured for Aircraft Directed Dual Safety SATCOM. On entering Active mode, the ACD: EFFECTIVITY 23-15-49 Page 2-25 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 90: Electronic Unit Identification And Satcom Configuration Reports
Pilot Displays (MCDU/TCP). The SDU maintains the following SDU configuration information with the characters limited to the maximum indicated: SDU Name 11 characters EFFECTIVITY 23-15-49 Page 2-26 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 91 The SDU retrieves and maintains the following SCM information: LRU Name 11 characters Hardware Part Number 15 characters max Serial Number 15 characters max. EFFECTIVITY 23-15-49 Page 2-27 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 92: Inmarsat Operational
ACARS and/or ATN ARINC 429 CMU (via Williamsburg V3) 2 safety voice channels 4-wire1, 4-wire2 Aircraft Position reporting ARINC 429 navigation input data. EFFECTIVITY 23-15-49 Page 2-28 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 93: G Sbb Bulletin Board And Satellite Table
If a new satellite is added to the non-volatile stored copy of the Satellite Table based on the System Information Broadcast, the ACD assigns it: The lowest priority (9) EFFECTIVITY 23-15-49 Page 2-29 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 94: Standard Call Discretes (Task 23-15-49)
And the ORT indicates standard call discretes, the ACD de-asserts the associated channel call light discrete. Whenever a 4-wire call is in the following states: CONNECTED EFFECTIVITY 23-15-49 Page 2-30 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 95: 4-Wire Call Control
CC if present else, set the call priority as Public. The following figure describes the incoming call decision logic for the PS channel: EFFECTIVITY 23-15-49 Page 2-31 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 96 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 2-4. (Sheet 1 of 2) Incoming PS Call Decision Logic EFFECTIVITY 23-15-49 Page 2-32 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 97 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 2-4. (Sheet 2 of 2) Incoming PS Call Decision Logic EFFECTIVITY 23-15-49 Page 2-33 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 98: Push-To-Talk (Ptt) Cockpit Call Control Mode
The Call Place/End discrete is not used for placing calls. In Latched mode, the ACD accepts an annunciated Ground-to-Air call (enter CONNECTED state) on any of the following: EFFECTIVITY 23-15-49 Page 2-34 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 99: Satellite Facing Voice Handling
4-wire1, The SDU does not support automatic redial on Air-to-Ground call fail. 4-wire2, The SDU does not support automatic redial on Air-to-Ground call fail. Safety Circuit Switched (CS) Voice Service EFFECTIVITY 23-15-49 Page 2-35 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 100: Ps (Sip) Voice Service
The ACD PBX responds to SIP OPTIONS polling from the network. NOTES: Absence of eMLPP will prevent sending the priority field EFFECTIVITY 23-15-49 Page 2-36 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 101: Air To Ground Call Set-Up
Commands the safety Channel Card to terminate the Secondary context. If a VoIP call is terminated by ground side SIP:BYE, the ACD: EFFECTIVITY 23-15-49 Page 2-37 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 102: Aircraft Information
370 GNSS Height (HAE) 261 Hybrid Altitude MSL 076 GNSS Altitude 361 Inertial Altitude True Heading 132 True Heading Hybrid 314 True Heading (INS) EFFECTIVITY 23-15-49 Page 2-38 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 103: Rf Power Control
The ACD calculates the back-off to send to the HPA considering the following: EIRP level for the ORT selected class of operation Installed static losses Gain performance of the installed antenna HPA gain. EFFECTIVITY 23-15-49 Page 2-39 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 104: Scm Modes Of Operations
Safety Data services include Air Traffic Services (ATS) and Airline Operational Control (AOC) datalink messages. ACARS data services are supported for SBB safety. AAP Protocol and Supported Services EFFECTIVITY 23-15-49 Page 2-40 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 105: Time And Date
The ACD distributes its internal time and date to the AP Processor at minimum at startup or when a resynchronization occurs. EFFECTIVITY 23-15-49 Page 2-41 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 106: Operational Air/Ground Status
WOW doesn’t equates to aircraft on ground, per ORT In-Air setting Weight-On- Use Secondary Source Wheels configured (WOW) per ORT setting, or invalid EFFECTIVITY 23-15-49 Page 2-42 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 107: Temperature Profile
The SDU configures the Safety Voice and ACARS Data services using the received 24- bit AES ID (ICAO address), obtained from the ORT identified source. EFFECTIVITY 23-15-49 Page 2-43 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 108 The SSM field has intentionally not been included in the validity criteria. Thus, ICAO information can be processed from ARINC 429 labels with SSM other than Normal Operation. EFFECTIVITY 23-15-49 Page 2-44 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 109: System Pre-Configuration
For each of the above, the license is permanent even if constructed with an expiry date. The Aspire 400 SDU supports permanent and expiring licensing of the following ACD controlled features: EFFECTIVITY 23-15-49 Page 3-1 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 110: Ort Parameters
Circuit mode data for ground-to-air calls (A781 Ref E2): Not applicable to SBB Ground-to-Air calls. Global beam high rate (A781 Ref E3): Not applicable to SBB return channel. EFFECTIVITY 23-15-49 Page 3-2 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 111: Satellite Table
SBB Type Approval Code Aircraft Type. Location ID SATCOM 1 Not Applicable Applicable. Location ID Description. SATCOM 2. Not Applicable Applicable. EFFECTIVITY 23-15-49 Page 3-3 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 112: Safety Voice
Cockpit Air-Ground Call Camp On Timer (A781 Ref D5) has the capability of pre- empting on-going call attendant call at any time, it is not based on a timer. EFFECTIVITY 23-15-49 Page 3-4 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 113 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 SDU codec #1 dedication (A781 Ref D1) always services cockpit voice. Dual SATCOM Voice Channel Mapping. EFFECTIVITY 23-15-49 Page 3-5 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 114 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Blank Page EFFECTIVITY 23-15-49 Page 3-6 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 115: Installation
The components have a label with a triangular Electrostatic Sensitive Devices caution symbol with bold upper case letters. NOTE: An acceptable phrasing is found in ATA 300, Chapter 6: EFFECTIVITY 23-15-49 Page 4-1 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 116: Engineering Drawings
For HPA Outline and Installation, refer to Figure 4-1. For SCM Outline and Installation, refer to Figure 4-2. For SDU Outline and Installation, refer to Figure 4-3. EFFECTIVITY 23-15-49 Page 4-2 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 117 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 4-1. (Sheet 1 of 3) HPA Outline and Installation EFFECTIVITY 23-15-49 Pages 4-3/4-4 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 118 3rd rvw Draft as of: 29 January, 2020...
Page 119 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 4-1. (Sheet 2 of 3) HPA Outline and Installation EFFECTIVITY 23-15-49 Pages 4-5/4-6 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 120 3rd rvw Draft as of: 29 January, 2020...
Page 121 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 4-1. (Sheet 3 of 3) HPA Outline and Installation EFFECTIVITY 23-15-49 Pages 4-7/4-8 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 122 3rd rvw Draft as of: 29 January, 2020...
Page 123 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 4-2. SCM Outline and Installation EFFECTIVITY 23-15-49 Pages 4-9/4-10 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 124 3rd rvw Draft as of: 29 January, 2020...
Page 125 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 4-3. (Sheet 1 of 2) SDU Outline and Installation EFFECTIVITY 23-15-49 Pages 4-11/4-12 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 126 3rd rvw Draft as of: 29 January, 2020...
Page 127 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 4-3. (Sheet 2 of 2) SDU Outline and Installation EFFECTIVITY 23-15-49 Pages 4-13/4-14 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 128 3rd rvw Draft as of: 29 January, 2020...
Page 129: General
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Electrical Installation (TASK 23-15-49) General The Electrical System for the Aspire-400 consists of three main components, the HPA, SCM and SDU, with the SDU acting as a central hub for the other two. HPA Installation Power Requirements The HPA system runs on 115 VAC with a maximum power consumption of 280 W and has a maximum power dissipation of 240 W.
Page 130 3rd rvw Draft as of: 29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Figure 4-4. ARINC 600 Receptacle with Index Pin Coding EFFECTIVITY 23-15-49 Page 4-16 22 Apr 2019 © Honeywell International Inc. Do not copy without express permission of Honeywell.

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Honeywell ASPIRE-400 System Description, Installation And Maintenance Manual

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