ARINC 824 : 2009
Current
The latest, up-to-date edition.
ONBOARD MOBILE TELEPHONY SYSTEM (OMTS)
Hardcopy , PDF
English
29-05-2009
1.0. INTRODUCTION
1.1. Purpose and Scope
1.2. Relationship to other Documents
1.3. Interoperability
1.4. Regulatory Approval
1.5. Reliability
1.6. Testability and Maintainability
1.7. Certification and Software Security and Partitioning
Considerations
2.0. SYSTEM OVERVIEW
2.1. General Description of OMTS-Related Functions
3.0. SYSTEM UNITS AND INTERFACES
3.1. General Description of the System Units
3.2. General Description of the OMTS Associated Units
4.0. CONFIGURATION
4.1. Interchangeability Objectives
4.2. Configuration Options
4.3. Link Budget Considerations
4.4. Power
4.5. Environmental Conditions
4.6. Grounding and Bonding
ATTACHMENTS
ATTACHMENT 1 - SYSTEM INTERFACES
ATTACHMENT 2 - REMOTE-MOUNTED EQUIPMENT DEFINITION
ATTACHMENT 3 - RACK-MOUNTED EQUIPMENT DEFINITION
APPENDICES
APPENDIX A - ACRONYMS AND ABBREVIATIONS
Provides standards necessary to achieve interchangeability between equipment providers.
| DocumentType |
Standard
|
| Pages |
50
|
| PublisherName |
Aeronautical Radio Inc.
|
| Status |
Current
|
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| ARINC 628P9-5:2017 | CABIN EQUIPMENT INTERFACES - PART 9: CABIN INTERFACE NETWORK (CIN) |
| ARINC 763A : 2008 | MARK 2 NETWORK SERVER SYSTEM (NSS) - FORM AND FIT DEFINITION |
| ARINC 628-0 : 2015 | CABIN EQUIPMENT INTERFACES - PART 0: CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM - OVERVIEW |
| ARINC 413A : 1976 | GUIDANCE FOR AIRCRAFT ELECTRICAL POWER UTILIZATION AND TRANSIENT PROTECTION |
| ARINC 833 : 2011 | CABIN UNIVERSAL WIRELESS DISTRIBUTION SYSTEM (UWDS) |
| ARINC 781 : 2005 SUPP 7 | MARK 3 AVIATION SATELLITE COMMUNICATIONS SYSTEMS |
| CEA CEB18 : 2007(R2017) | RECOMMENDED PRACTICE FOR TRANSMITTER CONTROL AND STATUS INDICATION IN TRANSMITTING PORTABLE ELECTRONIC DEVICES (T-PEDS) |
| ARINC 834 : 2008 SUPP 7 | AIRCRAFT DATA INTERFACE FUNCTION (ADIF) |
| ARINC 664-3 : 2002 SUPP 2 | AIRCRAFT DATA NETWORK - PART 3: INTERNET-BASED PROTOCOLS AND SERVICES |
| ARINC 609 : 1987 | DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS |
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