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ARINC 730 : 79 SUPP 3

Withdrawn
Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

AIRBORNE SEPARATION ASSURANCE SYSTEM
Withdrawn date

07-23-2013

Published date

01-12-2013

1.0 INTRODUCTION AND DESCRIPTION
   1.1 Purpose of this Document
   1.2 System Descriptions
   1.3 ASAS Equipment Functions
   1.4 Unit Descriptions
   1.5 Altitude Reporting Data
   1.6 DABS Data Link Data
   1.7 Interchangeability
   1.8 Regulatory Approval
2.0 INTERCHANGEABILITY STANDARDS
   2.1 Introduction
   2.2 Form Factor, Connectors and Index Pin Coding
   2.3 Interwiring
   2.4 Power Circuitry
   2.5 Environmental Conditions
   2.6 Cooling
   2.7 Grounding and Bonding
3.0 ATCRBS/DABS SYSTEM CHARACTERISTICS
   3.1 Purpose of this Chapter
   3.2 ATCRBS/DABS Compatibility
   3.3 Interrogation Signal Characteristics
   3.4 Reply Transmission Characteristics
                 (Signals-In-Space)
   3.5 System Utilization of Modes
   3.6 Sources of Reply Code Data
4.0 ACTIVE BCAS SYSTEM CHARACTERISTICS
5.0 TRANSPONDER FUNCTIONAL DESCRIPTION
   5.1 Functional Capability
   5.2 Transponder Receiver Characteristics
   5.3 Transponder Transmitter Characteristics
   5.4 Transponder Functional Test and Monitoring
   5.5 Antenna Diversity Operation
   5.6 Standard Message (SM) Data Transfer
   5.7 Extended Length Message (ELM) Transfer
6.0 ACTIVE BCAS FUNCTIONAL DESCRIPTION
7.0 PROVISIONS FOR AUTOMATIC TEST EQUIPMENT
   7.1 General
   7.2 Unit Identification
8.0 CONTROL PANEL DESIGN
   8.1 Form Factor and Connector
   8.2 Control Information Transfer
   8.3 Control Functions
   8.4 VFR/IFR Annunciation
   8.5 X-Pulse Selection
   8.6 IRS/FMC Data Input Source Select
   8.7 Control Panel Power and Initialization
   8.8 Dual ASAS Control Panel Considerations
9.0 ANTENNA
   9.1 Impedance and VSWR
   9.2 Gain and Polarization
   9.3 Power Rating
   9.4 Radiation Pattern
   9.5 Connector
   9.6 L-Band Systems Physical Isolation
   9.7 Antenna Installation
   9.8 Angle of Arrival-Sensitive Antennas
ATTACHMENTS
   1A ASAS Computer Unit Connector Positioning
   1B Control Unit Connector Positioning
   2A Standard Interwiring
   2B Notes Applicable To The Standard Interwiring
   2C ASAS Unit/Control Panel Wiring
   2D DABS Data Link I/O Interface Alternatives
   3A ATCRBS Reply Code And Pulse Characteristics
   3B Mode A Reply Code Combinations
   4 DITS Control Word for ASAS
   4A DITS Data Output Word for ASAS
   5 DABS Message and Data Block Formats
   6 Independent Standard Message (SM) Protocols
   7 Suppression Pulse System Characteristics
   8 Typical Blade Antenna
   9 Diversity Antenna Selection
   10 Environmental Test Categories
   11 AEEC Letters 78-166/XPDR-21 and 78-175/XPDR-22
APPENDICES
   1 SM Data Transfer Using the Standard Message
                 Interface
   2 SM Data Transfer Using ARINC 429 "Mark 33
                 Digital Information System (DITS)" Standards
   3 Draft US National Aviation Standard For Active
                 Beacon-Based Collision Avoidance System

Describes and Airborne Separation Assurance System specifically designed for installation in commercial type aircraft.

DevelopmentNote
OBSOLETE meaning the standard is no longer recommended for use or maintained current for new equipment designs.
DocumentType
Standard
PublisherName
Aeronautical Radio Inc.
Status
Withdrawn

STANAG 4193(PT3) : 2016 TECHNICAL CHARACTERISTICS OF THE IFF MK XIIA SYSTEM - PART 3: INSTALLED SYSTEM CHARACTERISTICS
STANAG 4193 (PT4) : 0 TECHNICAL CHARACTERISTICS OF IFF MK XA AND MK XII INTERROGATORS AND TRANSPONDERS - PART IV: TECHNICAL CHARACTERISTICS OF MODE S IN MILITARY INTERROGATORS AND TRANSPONDERS

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