ARINC 609 : 1987
Current
The latest, up-to-date edition.
Hardcopy , PDF
English
01-05-1987
1.0 INTRODUCTION AND DESCRIPTION
1.1 Purpose of this Document
1.2 Background
1.3 Relationship to Other Specifications and
Standards
1.4 Use of ARINC Report 609
1.5 Definition of Terms
2.0 SYSTEM DESIGN CONSIDERATIONS FOR AIRCRAFT
ELECTRICAL POWER
2.1 General
2.2 Regulatory and Other Concerns
2.3 Power Sources
2.4 Power Distribution
2.5 Built-In Test Equipment (BITE)
3.0 AIRCRAFT ELECTRICAL POWER COMPONENT DESIGN
3.1 General
3.2 AC Systems
3.3 DC Systems
4.0 AIRCRAFT ELECTRICAL POWER DISTRIBUTION,
PROTECTION AND CONTROL CHARACTERISTICS
4.1 General
4.2 Special Requirements
4.3 Distribution Considerations
4.4 Distribution Protection Philosophy
4.5 Control Philosophy
4.6 Summary of Different System Considerations -
Specific Limits
4.7 Requirements
5.0 AIRCRAFT ELECTRICAL POWER UTILIZING EQUIPMENT
DESIGN
5.1 General
5.2 Avionics
5.3 Electric Motors and Electromechanical
Actuators
5.4 Heaters
5.5 Lighting
6.0 CONSIDERATIONS FOR THE ALL-ELECTRIC AIRPLANE
6.1 Background
ATTACHMENTS
1 115 and 230 Volt/400 Hz Limits
2 28 VDC Transient Limits
3 Envelope of Voltage Spikes
4 270 VDC Limits
5 Abnormal Transient Voltage 115 Volt/400 Hz
System
6 Abnormal Transient Voltage 230 Volt/400 Hz
System
7 Proposed Voltage Transient Limits for
C.V.V.F. AC Generators
8 Abnormal Transient Voltage 115 Volt/Variable
Voltage System
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