This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Aircraft Lightning Test Methods
- Aerospace Standard
Published March 17, 2005 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This document is one of a set covering the whole spectrum of aircraft interaction with lightning. This document is intended to describe how to conduct lightning direct effects tests and indirect system upset effects tests. Indirect effects upset and damage tolerance tests for individual equipment items are addressed in DO-160/ED-14. Documents relating to other aspects of the certification process, including definition of the lightning environment, zoning, and indirect effects certification are listed in Section 2.
This document presents test techniques for simulated lightning testing of aircraft and the associated systems. This document does not include design criteria nor does it specify which items should or should not be tested. Acceptable levels of damage and/or pass/fail criteria for the qualification tests must be approved by the cognizant certification authority for each particular case. When lightning tests are a part of a certification plan, the test methods described herein are an acceptable means, but not the only means, of meeting the test requirements of the certification plan.
Each test method is set out in a uniform format, describing the test purpose, test object, test setup, test waveforms (voltage and/or current), measurements and data recording, test procedure and data interpretation. Guidance is provided on how to select the appropriate test or series of tests, and how the test results can be assessed.
Natural lightning is a complex and variable phenomenon and its interaction with different types of vehicles may be manifested in many different ways. It is not intended that every test described herein be applied to every system requiring lightning verification tests. The document is written so that specific aspects of the environment can be called out for each specific program as dictated by the vehicle design, performance and mission constraints.
|Aerospace Standard||General Requirements for WDM Backbone Networks|
|Aerospace Standard||Aircraft Lightning Test Methods|
|Aerospace Standard||Electronic Engine Control Design Guide for Electromagnetic Environmental Effects|
Data Sets - Support Documents
|[Unnamed Dataset 1]|
|[Unnamed Dataset 2]|
|[Unnamed Dataset 3]|
|TABLE 1||Typical Test Current Attachment Configurations|
|TABLE 2||Examples of Applications of Fuel System Tests|
|TABLE 3||Equivalent Flight Altitude versus Air Pressure|
SAE AE-2 LIGHTNING COMMITTEE It is the duty of the AE-2 committee to produce advisory materials for the aerospace community in the following areas:The natural lightning environment and related environment standards Protection of aerospace vehicles from the effects of lightning and other atmospheric electrical environments. Means of verifying the adequacy of protection measures. Standardized and other atmospheric electrical environments for lightning simulation and test methods.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.