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Electronic Engine Control Design Guide for Electromagnetic Environmental Effects
- Aerospace Standard
- AIR5060A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
The purpose of this document is to provide reference material for establishing compatibility of electronic gas turbine engine control systems and associated components with the electromagnetic environment and achieving compliance with associated airworthiness requirements.
Rationale
This document is being updated to incorporate policy and guidance changes made in the last 5 years in the area of Electromagnetic and Lightning environments.
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| Technical Paper | Model-Based Energy Management Functions for Aircraft Electrical Systems |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Unnamed Dataset 4 | ||
| TABLE 1 | HIRF ENVIRONMENTS AS DEFINED IN FAA AC-20-158 | |
| Unnamed Dataset 6 | ||
| TABLE 2 | EMP CHARACTERISTICS |
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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