Honeywell International Inc. 400 Maple Grove Road Ottawa, Ontario, K2V 1B8 Canada CAGE: 38473 Telephone: 800-601-3099 (Toll Free U.S.A./Canada) Telephone: 602-365-3099 (International Direct) Website: www.myaerospace.com ASPIRE-200 System Description, Installation, and Maintenance Manual This guide provides procedures for installation, configuration, and operation of the equipment listed below.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Model Part Number AMT-1800 Intermediate Gain Antenna with CNX-900 1541-K-1007-52 AMT-700 High Gain Antenna with CNX-200 1541-K-1006-11 AMT-700 High Gain Antenna with CNX-250 1541-K-1006-31 AMT-700 High Gain Antenna with CNX-900 1541-K-1006-51 AMT-3800 High Gain Antenna with CNX-200 1541-K-1006-12 AMT-3800 High Gain Antenna with CNX-250 1541-K-1006-32 AMT-3800 High Gain Antenna with CNX-900 1541-K-1006-52 23-15-45 © Honeywel
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Proprietary Information Honeywell – Confidential COPYRIGHT BY HONEYWELL INTERNATIONAL INC. (“HONEYWELL”). ALL RIGHTS RESERVED. THIS DOCUMENT AND ALL INFORMATION CONTAINED HEREIN ARE THE CONFIDENTIAL AND PROPRIETARY INFORMATION OF HONEYWELL AND CONTAIN HONEYWELL TRADE SECRETS.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 and may not decompile or disassemble software provided under this License Agreement, except and only to the extent that such activity is expressly permitted by applicable law notwithstanding this limitation. You may not create derivative works or modify the Materials in any way. You agree that Materials shall only be used for the purpose of the rights granted herein. The Material furnished hereunder may be subject to U.S.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 10. Remedies - Honeywell reserves the right to pursue all available remedies and damages resulting from a breach of this License Agreement. 11. Limitation of Liability - Honeywell makes no representations or warranties regarding the use or sufficiency of the Materials.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 WARNING: INCORRECTLY REPAIRED COMPONENTS CAN AFFECT AIRWORTHINESS OR DECREASE THE LIFE OF THE COMPONENTS. INCORRECTLY FABRICATED SPECIAL TOOLING OR TEST EQUIPMENT CAN RESULT IN DAMAGE TO THE PRODUCT COMPONENTS OR GIVE UNSATISFACTORY RESULTS. 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Copyright - Notice Copyright 2011, 2018 Honeywell International Inc. All rights reserved. Honeywell is a registered trademark of Honeywell International Inc. All other marks are owned by their respective companies. Aspire-200, System Description, Installation, and Maintenance Manual Document Number: MN-0000042, Revision F 28 Feb 2018 Revision Table Revision ECR Description A N/A First release.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 RECORD OF REVISIONS When revisions are received, insert revised pages, record the date, and initial. Revision Number Issue Date Date Inserted Inserted by (initial) Revision Number Issue Date Date Inserted 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 SERVICE BULLETIN LIST Service Bulletin Number Subject Mod Dot 6 Implementation Manual Rev. Manual Rev.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 LIST OF EFFECTIVE PAGES * An asterisk indicates pages changed, added, or deleted by the current revision. F indicates a right foldout page with a blank back. Section All Page All Date 28 Feb 2018 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 TABLE OF CONTENTS ABOUT THIS MANUAL 1. Scope...................................................................................................................... 1-1 2. Part Numbers ........................................................................................................ 1-1 3. Organization.......................................................................................................... 1-2 4. Precautions .........
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 6. AMT-1800 IGA ...................................................................................................... 3-11 7. AMT-3500 IGA ...................................................................................................... 3-13 8. AMT-3800 HGA ................................................................................................... 3-15 9. AMT-700 HGA ...........................................................
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 (1) Selecting a Location for the Blade Antenna ................................................................4-7 (2) Installing the Blade Antenna ........................................................................................4-8 I. AMT-1800 IGA ...................................................................................................................4-8 (1) Antenna to Aircraft Fuselage ....................................
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 A. Configuring a SwiftBroadband Dialer (Windows XP) .......................................................5-9 B. Configuring a SwiftBroadband Dialer (Windows 7) ........................................................5-15 TROUBLESHOOTING 1. Basic Equipment Checks .................................................................................... 6-1 A. Checking the FWD ID ..................................................................
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 LIST OF TABLES Table 2-1 HDU-200, IPLD, and SCM Specifications .................................................................. 2-2 Table 2-2 Specification Overview of ASPIRE-200 Components ................................................ 2-3 Table 2-3 ARINC 429 IRS Navigational Requirements............................................................ 2-10 Table 2-4 GNSS Navigational Data...................................................
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 LIST OF FIGURES Figure 2-1 Aspire-200 Variants .................................................................................................. 2-1 Figure 2-2 Cabin Network .......................................................................................................... 2-6 Figure 3-1 HDU Outline Drawing ................................................................................................
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 ABOUT THIS MANUAL This manual provides information about the installation, operation, and maintenance of the eNfusion® Aspire-200. 1. Scope This manual provides detailed information for avionics technicians about the wiring, installation, and setup of every component of the Aspire-200. The installer is responsible for the approval and certification of system components on the aircraft, and for the installation of wiring in the aircraft.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 • 1541-A-3000-01—HDU-200 • 1541-A-2000—IPLD • 1252-A-4120-01—SCM • 1541-A-9011—LGA • 1242-K-7001—AMT-1800 IGA • 1242-A-2210-01—eNfusion® AMT-3500 IGA AC • 1242-A-0010-02—eNfusion® AMT-3800 HGA DC • 1428-A-0010-02—eNfusion® AMT-700 HGA DC • 1233-A-0200—eNfusion® CCU-200 • 1110-A-0501-20—eNfusion® CNX-200 Series 2 Network Accelerator • CNX-900 router SCD-90406174 (CNX-900 router comes with Personality Module SCD-90406256)
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 pinout tables for all the connectors • Installation—information and procedures for the installation of the Aspire-200 • System Setup—information and procedures for setting up the system after installation • Troubleshooting—troubleshooting information and where to find it • Specifications—environmental specifications for every piece of equipment available with the Aspire-200 • Glossary. 4.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 INTRODUCTION 1. About the Aspire System The Aspire-200 connects to the Inmarsat satellite network and provides data and voice services to the aircraft cabin. You can install the Aspire-200 with various antennas, and each variation of the system provides a different level of service. With higher gain antennas, higher rates of transfer are possible, and you can access information faster and use applications that require higher bandwidth.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 The eNfusion® Communication Convergence Unit (CCU) extends the capabilities of the Aspire system with additional user connections and features for the aircraft cabin. For more information about the CCU, see “Introduction to the Cabin Network” on page 2-6, “eNfusion® CCU Interfaces” on page 2-7, and the CCU Network Administrator’s Guide, MN-1233-10054.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Table 2-1 HDU-200, IPLD, and SCM Specifications Component HDU-200 Characteristic Specification Dimensions 14.88 by 2.43 by 7.81 in. (378 by 62 by 198 mm) Mounting Information 2-MCU Tray Weight 8.8 pounds (4.0 kg) maximum Frequency Band Tx: 1626.5 to 1660.5 MHz Rx: 1525.0 to 1559.0 MHz Power Dissipation 40 W maximum (Typical 30 W) Operating Voltage 20.5 VDC to 32.2 VDC Cooling 15.5 lb/hr air @ 0.44 +/- 0.025 in.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Table 2-2 Specification Overview of ASPIRE-200 Components Component LGA AMT-1800 Characteristic Specification Dimensions 11 by 4.25 by 4.6 in. (279 by 108 by 117 mm) Weight 1.35 pouns (0.61 kg) Dimensions 18.3 by 7.6 by 1.98 in. (465 by 193 by 50 mm) Weight Flat variant - 5.5 lbs (2.5 kg) maximum Curved variant - 6.0 lbs (2.7 kg) maximum Power +28 VDC @ 0.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Table 2-2 Specification Overview of ASPIRE-200 Components Component CCU-200 Characteristic Specification Dimensions 8.65 by 7.7 by 2.3 in. (220 by 196 by 58 mm) Weight 4.0 lb (1.81 kg) maximum Clearance 2.0 in.(5.08 cm) on all sides Voltage 28 VDC Nominal Power Dissipation 6 W Nominal Power Consumption 28 VDC / 0.5 A Interfaces Ethernet: 8 x LAN 1-/100 Ethernet: 1 WAN USB: 2 x USB 1.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Table 2-2 Specification Overview of ASPIRE-200 Components Component CNX-900 Characteristic Specification Power 43.4 W maximum Mounting Mounts using ¼ in (10-24 mm) fasteners Software DO-178B Level E Clearances 2 in. (51 mm) clearance recommended Dimensions 2MCU ARINC 600 Form Factor Weight 6.4 pounds (2.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 You can create a sophisticated airborne network that includes WiFi access and an airborne LAN with the CCU. The CCU is a multi-function networking device that provides wireless LAN, Ethernet LAN, 2 and 4-wire voice, and ISDN services. The CCU can also create a telephone system for the airborne office, including extensions for each phone on the aircraft and an automated attendant.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 F. • Two USB 1.1 interfaces • One RS-232 interface for access to maintenance functions • One RS-232 full modem interface • One 802.11 b/g WAP (Wireless Access Point) • Two 4-Wire interfaces (for the cockpit) • Two FXS interfaces for POTS • Two FXO interfaces for POTS • Four ISDN interfaces.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 • 802.11 ac Wi-Fi, three Wi-Fi antennas • 3G/4G/LTE cellular for future connectivity to the public Internet while on the ground • Two ISDN BRI Interfaces for future telephony trunking support • I. 80Gb solid state media storage. Aspire-200 Connections to Aircraft The Aspire-200 communicates with various systems in your aircraft to control the antenna and distribute resources to its subsystems.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Table 2-3 ARINC 429 IRS Navigational Requirements Label (Octal) Name Minimum Interval Rate (ms) Maximum Interval Rate (ms) 310 Latitude 100 200 311 Longitude 100 200 312 Ground Speed 25 50 313 True Track 25 50 314 True Heading 25 50 324 Pitch Angle 10 20 325 Roll Angle 10 20 361 Altitude 20 40 Table 2-4 GNSS Navigational Data Label (Octal) Name Minimum Interval Rate (ms) Maximum Interval Rate (ms) 37
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Table 2-5 Hybrid Inertial/GNSS Navigational Data Label (Octal) Name Minimum Interval Rate (ms) Maximum Interval Rate (ms) 132 or 314 True Heading, Hybrid, 25 or Intertial 50 324 Pitch Angle 10 20 325 Roll Angle 10 20 261 or 076 Hybrid Altitude MLS or 20 GNSS Altitude 40 Table 2-6 FMS Navigational Data Label (Octal) Name Minimum Interval Rate (ms) Maximum Interval (ms) 203 Pressure Altitude 31.3 62.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 The Aspire-200 can access services from two of Inmarsat’s satellite networks. The I-3 satellite network provides Swift 64 services, and the I-4 satellite network provides SwiftBroadband (SBB) services. Throughout 2018, Inmarsat will transition Swift64 services to the I-4 network and then decommission the I-3 network. 3.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 • • Class 7 systems can access circuit-switched services (AMBEvoice) in the full coverage area of the I-4 satellite network. • An Aspire-200 equipped with an IGA can access only Class 7 services. • Class 7 ISDN circuit-switched services such as 56k RDI, 64k UDI, and 3.1KHz (fax) are only available when the look angle to the satellite is greater than 45 degrees.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 6. Subscribe to a service plan from a SwiftBroadband or Swift 64 Service Provider. 7. If an HDR upgrade has been installed on the Aspire-200 System, ensure the applicable keys have been provisioned to use the HDR system with the Inmarsat network. 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 EQUIPMENT DRAWINGS This section includes outline drawings of every component in the Aspire-200. 1. HDU-200 Figure 3-1 HDU Outline Drawing 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 2. HDU Rear Connector Figure 3-2 HDU Rear Connector 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 3. IPLD Figure 3-3 IPLD Outline Drawing 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 4. SCM Figure 3-4 SCM Outline Drawing 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 5. Omni Blade Antenna Figure 3-5 Omni Blade Antenna Outline Drawing 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 6. AMT-1800 IGA 5 (X) 5.50 IN. 7.525 (2 PLACES) ±0.02 IN. B B 7.64 IN. (MAX) (OUTSIDE OF LIGHTNING DIVERTERS) TRIMETRIC VIEW: TOP (NTS) 10.00 IN. (2 PLACES) 18.30 IN. (MAX) 0.02 IN. MOUNTING BOSS PROJECTED FROM A DIA 0.69 IN. 1.98 IN. (MAX) (4 PLACES) UP 0.62 IN. "D" (SEE TABLE 1) B-B (NTS) (FOUR MOUNTING HOLES) 0.15 IN. MEASURED AT CENTERLINE ALL VARIANTS (2 PLACES) 16 15 (2 PLACES) 2.750 IN. 8 TAMPERPROOF/QA LABEL 0.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 7. AMT-3500 IGA Figure 3-7 AMT-3500 IGA Outline Drawing 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 8. AMT-3800 HGA Figure 3-8 AMT-3800 HGA Outline and Installation Drawing 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 9. AMT-700 HGA Figure 3-9 AMT-700 HGA Outline Drawing 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 10. CCU-200 Figure 3-10 CCU-200 Outline and Installation Drawing 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 11. CNX-200 Figure 3-11 CNX-200 Outline and Installation Drawing 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 ID-658118 E90403134-1-A 12. CNX-250 Figure 3-12 CNX-250 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 13. CNX-900 Figure 3-13 CNX-900 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 14. CNX-900 Personality Module Figure 3-14 CNX-900 Personality Module 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 INSTALLATION 1. Installation Overview The Aspire system includes five LRUs: • HDU • IPLD • SCM • Antenna—LGA, IGA, or HGA • Optional router. The first four LRUs of the core Aspire system provide all the functions and services described in “Aspire-200 Features” on page 2-7 and “Aspire-200 User Interfaces” on page 2-7. The router provides additional features that can create a network or office for users in the aircraft cabin.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 3. Mechanical Installation This section includes information about installing the equipment in the core Aspire-200. Contact Honeywell about installation kits that include mating connectors and cables. A. HDU Install the HDU in a standard 2-MCU rack. The Aspire-200 ships only the equipment in the core system. The customer is responsible for the mounting tray, mating ARINC 600 connector and cables.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 The IPLD does not require forced cooling. However, to ensure that the IPLD can dissipate heat, install the IPLD in a location that meets as many of the following conditions as possible: • temperature controlled • air can circulate around the IPLD • the IPLD can dissipate heat to that aircraft structure.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 D. CCU-200 You can install the CCU in a pressurized or non-pressurized environment. Figure 3-9 on page 3-17 illustrates the physical and mechanical specifications of the CCU-200. (1) Physical Placement Bolt the CCU to a flat surface within the aircraft cabin in any orientation. Install the mounting flange of the CNX CCU using four 10-32 bolts. The CCU must have two inches of clearance on all sides.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 WARNING: TO PREVENT DAMAGE TO THE UNIT, DO NOT INSERT THE SCREWS MORE THAN 0.26 INCHES INSIDE THE CHASSIS OF THE UNIT. (4) Installation Notes 29B 1. All wire in accordance with MIL-W-22759/34, or equivalent, unless otherwise specified. 2. All cable in accordance with MIL-C-27500 unless otherwise specified. 3. All coaxial cable in accordance with MIL-C-17 unless otherwise specified.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 F. CNX-250 The CNX-250 must be installed in a pressurized cabin. Refer to CNX-250 Cabin Gateway Installation Manual, ATA No. 23-15-18. (1) Cooling Requirements CNX Cabin Gateway products do not require external, forced-air cooling as long as clearance requirements are maintained and ventilation is provided as required to ensure that the maximum operating temperature does not exceed 131°F (55°C).
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 (3) Clearance and Accessibility Requirements If mounting on a shelf with other avionic equipment the recommended minimum thermal clearances are: • At least 1 inch (25.4 mm) to the left from the adjacent LRU • At least 2.25 inches (57.2 mm) to the right (CNX-900 Heat Sink side).
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 • Separation resulting in greater than 40dB of isolation should be provided between the Blade Antenna and the GPS Antenna at 1572.0 to 1616.0 MHz (GPS band) and 1626.5 to 1660.5 MHz (SATCOM band). The Blade Antenna provides 50dB of filtering. If another antenna is installed, check the documentation for GPS isolation. (2) Installing the Blade Antenna To install the antenna assembly: 1.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Center the O-ring seals on the J1 and J2 connector holes (approximately). Ensure that there is no overlap between the O-rings and the fuselage penetration holes. NOTE: Do not re-use gasket or O-rings. Additionally, the perimeter of the AMT-1800 IGA should be sealed to the mounting surface (aircraft fuselage or Antenna Interface Mount, if applicable) to avoid water entrapment and corrosion.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 offset to correct beam steering. During the initial installation, set the pitch, roll, and rotation offset angles to within ± 0.25° in the AMT-1800 IGA EEPROM— MN-1242-70010 provides information about setting up the AMT-1800 IGA. Refer to the AMT-1800 IGA SDIM for more information on setting these values through the Antenna interface.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 this orientation, the principal axes of the AMT-3500 IGA should be aligned with those of the aircraft to within ± 0.25°. This is the default position for the AMT-3500 IGA. You can install the AMT-3500 IGA in a position that is slightly offset from the default position.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 7. Seal the interfaces. NOTE: The aft cover interfaces do not require sealing. 8. Test the satellite communication equipment as specified by the manufacturer. Honeywell recommends towing the aircraft in a figure eight pattern or 360 degrees while monitoring the signal strength. K.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 (3) Aligning the AMT-3800 HGA Orientation of the AMT-3800 HGA is defined with respect to the principal axes on the antenna. The principal axes are illustrated in Figure 3-7 on page 3-13. The connector access cover on the radome is towards the aft of the aircraft. In this orientation, the principal axes of the AMT-3800 HGA should be aligned with those of the aircraft to within ± 0.25°. This is the default position for the AMT-3800 HGA.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 7. Seal the interfaces. NOTE: The aft cover interfaces do not require sealing. 8. Test the satellite communication equipment as specified by the manufacturer. Honeywell recommends towing the aircraft in a figure eight pattern while monitoring the signal strength. L.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 3. Measure the +28 VDC input voltage to the HGA at A1-P1 V and Y to A1-P1 P and S. 4. Measure the +28 VDC input voltage to the DLNA at A2-P4 G to A2-P4 K. 5. Switch OFF the breaker to the antenna subsystem components. 6. Connect the +28 VDC supply cable to A1-J1 and A2-J4. Perform manufacturer-specific satellite communication avionics tests.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Figure 4-2 Remote Lamp Panel Circuit Remote lamps are available on connector pins: • MP-10A—Power • MP-10B—Channel available. 5. Cabling Requirements In single point cabling, the cable shield is terminated at one end only via a connector or suitable crimp terminal.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Table 4-3 Cable Shielding and Termination Specifications Cable Conductor Type RF TX and RX Coaxial Single Point Multiple Point Yes Minimum Conductor Coverage by Shield 95% When installing the Aspire-200, follow the cabling requirements listed below: • The maximum recommended length for USB data connections is 16 feet. • The maximum recommended length for USB power connections is 30 feet.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Figure 4-3 ASPIRE-200 Interconnect Drawing, 1541-B-1000 Rev D00 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Figure 4-4 ASPIRE-200 Interconnect Drawing, 1541-B-1000 Rev D00 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Figure 4-5 ASPIRE-200 Interconnect Drawing, 1541-B-1000 Rev D00 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Figure 4-6 ASPIRE-200 Interconnect Drawing, 1541-B-1000 Rev D00 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 SYSTEM SETUP 1. Setting up Operational Parameters After the Aspire-200 is installed in the aircraft, you must configure fundamental parameters in order to operate the system: • Cable losses • LES IDs • The APN • Navigational input to the system. A. Connecting to the Aspire-200 Maintenance Port You can connect to the Aspire-200 through the maintenance port. To connect to the maintenance port: 1.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 To configure cable loss parameters: 1. Connect to the HDU maintenance port—see “Connecting to the Aspire-200 Maintenance Port” on page 1. 2. In the maintenance menus, press CTRL + N to navigate to menu 3. 3. In menu 3, to access miscellaneous EEPROM parameters, press m. The list of miscellaneous EEPROM parameters appears.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 3. In menu 3, to access Ocean Region Parameters, press p. The Ocean Region Parameter prompt appears. REGION REGION REGION REGION REGION REGION REGION REGION 0 1 2 3 4 5 6 7 AORW AORE POR IOR MTSAT APAC EMEA AMERICAS SAT LONG 54.0W 15.5W 178.0E 64.0E 142.5E 143.5E 25.0E 97.5W LES ID 0 0 0 0 TNID 0 0 0 0 SERVICES SW64/AERO SW64/AERO SW64/AERO SW64/AERO AERO AERO/SBB AERO/SBB AERO/SBB WHICH OCEAN REGION (0-7) ? 0 4.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 SATELLITE SERVICES (A=AERO S=SWIFT64 B=SBB) (ie, AB) ? 9. To accept the existing value, press ENTER. 10. Restart the HDU. You can restart the HDU using menu 2, option Z. To configure an LES ID for all Ocean Regions: 1. Connect to the HDU maintenance port—see “Connecting to the Aspire-200 Maintenance Port” on page 1. 2. In the maintenance menus, press CTRL + N to navigate to menu 3. 3. In menu 3, to access Ocean Region Parameters, press i.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 4. To navigate the list of parameters, press CTRL + N. 5. To configure the APN, press the number next to the Data I/O APN parameter, and then press ENTER. The Data I/O APN prompt appears. DATA I/O APN ?[ ] = ? 6. Type the new APN, and then press ENTER. 7. Restart the HDU. You can restart the HDU using menu 2, option Z. E. Configuring NAV The Aspire-200 uses information from the aircraft’s navigation system to steer the antenna.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 6. Type the number next to the available NAV type. 7. To configure the NAV2 type, press the number next to the NAV2 Type parameter, and then press ENTER. The NAV2 Type prompt appears. NAV2 TYPE NOT INSTALLED 0="NOT INSTALLED" 1=INERTIAL 4=HYBRID 7=AHRS 8=FMS = ? 3=GNSS 8. Type the number next to the available NAV2 type. 9. To configure the NAV3 type, press the number next to the NAV3 Type parameter, and then press ENTER.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 F. Entering the Antenna Alignment Parameters: ROLL, PITCH, ROTATION 1. Ensure the terminal emulation program is connected to the Aspire-200 maintenance console (see section A). 2. Navigate to menu 3 select option m. At this point the MISCELLANEOUS PARAMETERS submenu will be displayed. 3. Enter N to navigate to the next page.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 5. To enter the ROLL parameter Navigate to menu 3 select option m then select option 94. Enter the ROLL parameter value noting the correct sign, either + or -. The following text will be displayed after selecting option 94. It will display the current ROLL parameter value and provide the option to enter a new ROLL parameter value. Values displayed below are examples only.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 8. To confirm the parameter values entered navigate to any of the menu selections in steps 5, 6, or 7. Select the menu option to display the current parameter value then hit to terminate the menu option if you don’t want to enter a new parameter value. If the displayed parameter’s value is incorrect a new parameter value may be entered. 2. Configuring Dialers Dialers enable your computer to connect to the Internet or other networks.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 3. Click Create a new connection. The New Connection Wizard appears. 4. Click Next. The Network Connection Type page appears. 5. Click Connect to the Internet, and then click Next. The Getting Ready page appears. 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 6. Click Set up my connection manually, and then click Next. The Internet Connection page appears. 7. Click Connect using a broadband connection that requires a user name and password, and then click Next. The Connection Name page appears. 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 8. In the ISP Name field, type SBB, and then click Next. The name you enter is the name that appears in the list of connections available on your computer. The Connection Availability page appears. 9. Click Anyone's use or My use only, and then click Next. The Internet Account Information page appears. 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 10. If required by your service provider, type a User name and Password in the appropriate fields. 11. In the Confirm password text box, retype the password. 12. Click Next. The Completing the New Connection Wizard page appears. 13. To complete the connection setup, click Finish. The Connect dialog box appears. 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 14. Click Properties. The Properties dialog box appears. 15. In the Service Name text box, type the service name BGAN:BACKGROUND@USER=username@PASS=password@APN=my.a pn.com. Replace the text “username”, “password”, and “my.apn.com” with your own username, password, and APN IP address. NOTE: Each parameter of the service name is independent and if you do not type it in the service name, the system uses the value from it’s configuration.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 B. Configuring a SwiftBroadband Dialer (Windows 7) To configure a dialer to access SBB services on an Ethernet connection: 1. Click the Start button, click Control Panel, click Network and Internet, and then click Network and Sharing Center. The Network Connections window appears. 2. Click Set up a new connection or network. The Set up a Connection or Network window appears. 3. Click Connect to the Internet, and then click Next.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 4. Click No, create a new connection, and then click Next. A list of connection types appears. 5. Click Broadband (PPPOE). A list of connection parameters appears. 6. In the User name and Password fields, type the username and password assigned by your service provider. 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 7. In the Connection name field, type a descriptive name for this connection. The name you enter is the name that appears in the list of connections available on your computer. 8. Click Connect. The Connection to the Internet page appears. The connection is ready for use. 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 TROUBLESHOOTING This chapter provides information and procedures to help users diagnose and repair common problems. NOTE: If you have a computer connected to the internet, Honeywell product support engineers can help troubleshoot your terminal using a remote desktop application. 1.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 FIRMWARE VERSIONS: KERNEL: APPLICATION: CHANNEL CARD: DATA IO CARD: 09:38:54 V2.2 -- Tue Dec 07 17:56:11 2010 V28.1 -- Fri Oct 03 13:41:54 2014 6.8.7.0 -- 1.4.0.0 -- -- 4.2.3.0 Version 1.84.0.0 built on Apr 27 2011 CHANNEL CARD STATISTICS CARD #1 BGAN 15X (SERIAL 58080): 1742.5 hrs powered 1138.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 INMARSAT TYPE APPROVAL: -----CHAN #1: ABCDEF (AERO WITH MPDS) B. Checking the APN The Aspire-200 MPU can display EEPROM parameters, including the APN. To view the strapped APN: 1. Connect to the HDU maintenance port—see “Connecting to the Aspire-200 Maintenance Port” on page 1.. 2. In the maintenance menus, press CTRL + N to navigate to menu 3. 3. To view Miscellaneous EEPROM parameters, press m. The list of parameters appears.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 3. To navigate through the list of reports, press CTRL + N. 4. To access a report, type the number next to the report name, and then press ENTER. B. System Status Reports The vt100 scenario report provides information about various aspects of the channel card operation. To view the report, in the list of available reports, press the number next to vt100 scenario report. Figure 6-1 provides an example of the output of the report. 45D25'12.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Table 6-1 VT100 Scenario Report Content (Continued) Output Example Description LOOK ANGLE=33.1 Antenna elevation angle to the satellite, with respect to the horizontal axis of the aircraft CHAN The channel card number C/N0 RF input Carrier-to-Noise (C/No) level; typically 50.0 to 55.0 for Swift 64, 55.0 to 60.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Figure 6-2 System Config Strapping Report D. Antenna Reports Three reports provide information about the status and operation of the Aspire-200 antenna. • port antenna arinc input • port antenna maintenance word • port antenna status word To view the report, in the list of available reports, press the number next to the report name. Figure 6-3 provides an example of the port antenna ARINC input report.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 port status $708039 OMNIDIRECTIONAL MODE port status $708039 OMNIDIRECTIONAL MODE port status $708039 OMNIDIRECTIONAL MODE port status $708039 OMNIDIRECTIONAL MODE SDI: PRT/TOP SSM: NORMAL gain=14.0 open loop tracking port/top active SDI: PRT/TOP SSM: NORMAL gain=14.0 open loop tracking port/top active SDI: PRT/TOP SSM: NORMAL gain=14.0 open loop tracking port/top active SDI: PRT/TOP SSM: NORMAL gain=14.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 hit '0' for complete log '1' for 'special' events '-' for specific entry HDU EMS SERIAL NUMBER S/N ??? EVENT LOG: 1027 entries -- powerup #44 (15 hours) most recent entry at address 337a10 HIT 'S' FOR MORE -- '.' LISTS ALL REMAINING ENTRIES DIAGNOSTIC (ENTRIES #1026 - #1027): address 337a10: 160 seconds after powerup powerup #44 15 hours operation Nov 29 18:02:47 2014 CHAN 1 REQUESTED 0.0 dBW -- 654.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 4. To view all log entries, press 0. 4. Instructions for Continued Airworthiness This section presents the instructions for continued airworthiness, as per FAR 25.1529, of the equipment in the Aspire-200 system.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 APPENDIX A: SPECIFICATIONS 1. HDU Inmarsat Terminal Section Condition DO-160E Category 4.0 Temperature and Altitude 4.5.1 Ground Survival Low Temperature Test and Short-Time Low Operating Temperature Test A4/C4 4.5.2 Operating Low Temperature A4/C4 4.5.3 Ground Survival High Temperature and Short-Time High Operating Temperature A4/C4 4.5.4 Operating High Temperature A4/C4 4.6.1 Altitude A4/C4 4.6.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 2. Integrated Power and Low-noise Amplifier and Diplexer (IPLD) Section Condition DO-160E Category 4 Temperature and Altitude—70 000ft E1 4 Overpressure—200kPa E1—Extended 4 Decompression—8000ft E1—Extended 5.0 Temperature Variation—10°C/minute A 6.0 Humidity B 7.0 Operational Shocks and Crash Safety E 8.0 Vibration S (curves L, M, Y, C, E), R (curves C1 and E1), and U (curve G) 9.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 3. External Satcom Configuration Module Section Condition DO-160 Category 4.0 Temperature and Altitude F2 5.0 Temperature Variation B 6.0 Humidity A 7.0 Operational Shocks and Crash Safety B 8.0 Vibration S—curves B, L, M, Y; R— curves B, B1 9.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 4. Blade Antenna Section Condition DO-160 Category 4.0 Temperature and Altitude E1 5.0 Temperature Variation A2 6.0 Humidity A 7.0 Operational Shocks and Crash Safety C, B 8.0 Vibration S, U 9.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 5. AMT-3500 Intermediate Gain Antenna Section Condition DO-160E Category 4.0 Temperature and Altitude A2, E1 5.0 Temperature Variation A 6.0 Humidity B 7.0 Operational Shocks and Crash Safety E 8.0 Vibration S, R, U 9.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 6. AMT-1800 High Gain Antenna Section Condition DO-160E Category 4.0 Temperature and Altitude E1 4.5.1 Ground Survival Low and Short Time Operating Low E1 modified 4.5.2 Operating Low Temperature E1 modified 4.5.3 Ground Survival High Temperature E1 4.5.3 Short Term Operation High Temperature E1 modified 4.5.4 Operating High E1 4.5.5 In Flight Loss of Cooling X 4.6.1 Altitude Test E1 4.6.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Section Condition DO-160E Category 22 Lightning Induced Transient Susceptibility A3J33 23 Lightning Direct Effects 2A 24 Icing A 25 Electrostatic Discharge A 26 Fire, Flammability X—not required 23-15-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 7. AMT-3800 High Gain Antenna Section Condition DO-160E Category 4.0 Temperature and Altitude E1 5.0 Temperature Variation A 6.0 Humidity B 7.0 Operational Shocks and Crash Safety B/E 8.0 Vibration S, R 9.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 8. AMT-700 High Gain Antenna Section Condition DO-160E Category 4.0 Temperature and Altitude E1 5.0 Temperature Variation A 6.0 Humidity B 7.0 Operational Shocks and Crash Safety B/E 8.0 Vibration S, R 9.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 9. CNX-200Series 2 Network Accelerator 23BX DO-160E Section Environmental Condition Description of Test 4.0 Temperature and Altitude A4 5.0 Temperature Variation B 6.0 Humidity A 7.0 Operational Shocks and Crash Safety B 8.0 Vibration S 9.0 Explosion Proofness E 10.0 Waterproofness X—not required 11.0 Fluid Susceptibility X—not required 12.0 Sand and Dust X—not required 13.0 Fungus Resistance F 14.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 10.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 11. CNX-250 Section DO-160G Category Environmental Condition 4 Temperature and Altitude Cat A1 (max.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 Section DO-160G Category Environmental Condition 18 Audio Frequency Conducted Susceptibility–Power Input Cat Z for DC powered equipment 19 Induced Signal Susceptibility Cat AC (DC powered equipment) 20 Radio Frequency Susceptibility (Radiated and Conducted) RR - conducted and radiated (bench testing is allowed to meet the HRF associated with the normal environment) 21 Emission of RF Energy Cat M 22 Lightning Induced Transie
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 12. CNX-900 The Avionics LRU and PM of the CNX-900 Communication Family are environmentally qualified to RTCA DO-160G. Qualification rest report TN2000-TR-0001 is available to support aircraft certification activities.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 APPENDIX B: GLOSSARY 1.
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