ARINC 743 : 1990
Current
The latest, up-to-date edition.
AIRBORNE GLOBAL POSITIONING SYSTEM RECEIVER
Hardcopy , PDF
English
01-03-1990
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1.0 INTRODUCTION
1.1 Purpose of this Document
1.2 Summary of GPS System Operational Characteristics
1.3 Brief Description of the System
1.4 Interchangeability
1.5 Regulatory Approval
1.6 Reliability
1.7 Testability and Maintainability
2.0 INTERCHANGEABILITY STANDARDS
2.1 Introduction
2.3 Standardized Signaling
2.4 Standard Interwiring
2.5 Power Circuitry
2.6 Environmental Conditions
3.0 GPS SENSOR SYSTEM DESIGN
3.1 General
3.2 System Application
3.3 General System Capabilities
3.4 Specific System Capabilities
4.0 GPS SENSOR DESIGN
4.1 Integrity
4.2 Modes
4.3 System Interfaces
4.4 Sensor Performance (2 MCU Configuration)
5.0 INTEGRATED ANTENNA/PREAMPLIFIER/FILTER DESIGN
5.1 Antenna Requirements
5.2 Preamplifier Assembly Performance
5.3 Antenna/Preamplifier/Filter Requirements
5.4 Physical Characteristics
Describes the characteristics of the Global Positioning System (GPS) sensor portion of a GPS system intended for installation in commercial transport aircraft.
| DocumentType |
Standard
|
| Pages |
42
|
| PublisherName |
Aeronautical Radio Inc.
|
| Status |
Current
|
| FAA AC 20-165 : 2015 | AIRWORTHINESS APPROVAL OF AUTOMATIC DEPENDENT SURVEILLANCE - BROADCAST OUT SYSTEMS |
| FAA AC 20-172 : 2015 | AIRWORTHINESS APPROVAL FOR ADS-B IN SYSTEMS AND APPLICATIONS |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.