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Standard

MULTI-TRANSMITTER DATA BUS PART 2 APPLICATIONS GUIDE

1999-02-26
CURRENT
ARINC629P2-2
Defines the aviation industry standards for transfer of digital data between avionics system elements using multiple access, bi-directional protocol. Developed to provide an efficient data distribution system resulting in a reduction in the amount of airplane wiring and equipment interfaces.
Standard

GUIDE FOR USING THE ADA PROGRAMMING LANGUAGE IN AVIONIC SYSTEMS

1998-01-04
CURRENT
ARINC613
In 1986 the airlines selected Ada as the high-order development language for avionics. ARINC 613 describes the Ada domain most suited for avionics software development. The standard provides valuable guidance to Ada compiler developers and Ada programmers.
Standard

DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS

1987-01-05
CURRENT
ARINC609
This standard describes electrical power system design and performance standards brought about by extensive use of digital avionics. This Report provides guidelines for designers of aircraft power system components and of power utilization components, both avionics and power converters such as motors and heaters.
Standard

CONTROL/DISPLAY INTERFACES

1981-02-10
CURRENT
ARINC601
This Specification provides standards for the effective control of the environment for avionic equipment, including basic design standards for avionics equipment and its installation to assure suitable thermal interfaces, design criteria, and cooling appraisal.
Standard

ARINC REPORT 634 HF DATA LINK SYSTEM DESIGN GUIDANCE MATERIAL

1996-08-30
CURRENT
ARINC634
This Report provides the reader with material to enhance the understanding of high frequency data link. This standard provides a snapshot of guidance material used in the development of ARINC 753, HF Data Link System, and ARINC 635, HF Data Link Protocols.
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