This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Aerospace - Lightning Effects on Hydraulic Transport Elements on Aircraft
- Aerospace Standard
Published August 28, 2015 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This SAE Aerospace Information Report (AIR) describes hydraulic system design and installation to minimize the effects of lightning, especially when the aircraft structure is composite. Techniques for effective electrical bonding, hydraulic system lightning protection, and lightning protection verification techniques are discussed.
There is a need to address the effects of lightning on hydraulic systems in aircraft, especially where there is a significant use of composite materials in the aircraft structure. This is due to the potential structural damage and component failures that could occur. This document addresses this need.
|Journal Article||Lightning Effects on Hydraulic Transport Elements in Composite Aircraft|
|Aerospace Standard||Aerospace - Commercial Aircraft Hydraulic Systems|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
A-6A1 Commercial Aircraft Committee
The Commercial Aircraft Panel is responsible for the development of standards and recommended practices related to the integration of fluid power and actuation technologies into commercial air vehicles. The Panel provides a forum for aircraft manufacturers, suppliers, airworthiness regulatory engineers and operators to exchange technical information and discuss regulatory updates, recent technology developments, lessons learned, and issues related to system development and in service operation.
|ARP5412||Aircraft Lightning Environment and Related Test Waveforms|
|ARP5414||Aircraft Lightning Zoning|
|ARP5415||User’s Manual for Certification of Aircraft Electrical/Electronic Systems for the Indirect Effects of Lightning|
|ARP5416||Aircraft Lightning Test Methods|
|ARP5577||Aircraft Lightning Direct Effects Certification|
|FAA AC 20-136B||This document is not part of the subscrption.|
|FAA AC 20-53B||This document is not part of the subscrption.|
|NASA 1008||This document is not part of the subscrption.|
|NASA-STD-P023||This document is not part of the subscrption.|
|NASA/TM-1999-209734||This document is not part of the subscrption.|
* 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.