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Electronic Propulsion Control System/Aircraft Interface Control Documents
- Aerospace Standard
- AIR6181
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Aerospace Information Report (AIR) provides guidelines to document the functional and physical interface requirements for the electrical systems (including an EPCS and its components) between a given propulsion system and the aircraft on which the system is installed and the functionality pertinent to each interface.
The scope includes civilian aircraft powered by turbofan, turboprop, and turboshaft engines equipped with electronic engine controls.
Rationale
In response to a committee initiative, the revision of this document is intended to elaborate on the structure and content of an Interface Control Document for the Electronic Propulsion Control System, to be used by the airframe/engine manufacturers. This document is based on the previously released ARP4874. It has been revised to reflect input collected as part of the ‘5-Year Review’ process.
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Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
TABLE A1 | PARAMETERS USED IN DEFINITION OF DIGITAL DATA |
Issuing Committee
E-36 Electronic Engine Controls Committee
Areas of interest will include, but not be limited to, the design, installation, operation and maintenance of engine control system components including metering components and actuators and the interface and communication methods for (A) Cockpit Displays, (B) Flight Control, ¿ Diagnostic and Health Monitoring Systems. Coordination with other SAE committees will occur to minimize redundant activities within the organization and maximize the benefit of additional recommendations and standards.
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Number | Title |
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EASAAMC20-1 | This document is not part of the subscrption. |
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