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Aircraft Fuel System Pressure Definitions
- Aerospace Standard
Published December 18, 2020 by SAE International in United States
Downloadable datasets availableAnnotation ability available
The information in this document is limited to aircraft engine fuel feed, refueling, and transfer components (see 2.1). It is assumed that isothermal, liquid fluid conditions exist, herein referred to as fuel. Where applicable and allowable, it is understood that a referee fluid may be substituted for fuel.
The word “pressure” can be combined with a dozen of different words to define a wide range of technical definitions; this AIR is intended to present a list of such definitions in order to assist the industry's work.
The SAE Five-Year Review process identified that the reference section needed updating and some pressure definitions could be improved. The revision also has been considered beneficial because the document was in the old format (typewriter created).
Sections 4 and 5 have been added to the document as the committee has considered important and were absent in the original document
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
|AIR1408||AEROSPACE FUEL SYSTEM SPECIFICATIONS AND STANDARDS|
|ARP1665||DEFINITION OF PRESSURE SURGE TEST AND MEASUREMENT METHODS FOR RECEIVER AIRCRAFT|
|ARP243||NOMENCLATURE, AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS|
|MIL-F-17874||This document is not part of the subscrption.|
|MIL-F-38363||This document is not part of the subscrption.|
|MIL-F-87154||This document is not part of the subscrption.|
|MIL-P-25030||This document is not part of the subscrption.|
|MIL-P-5238||This document is not part of the subscrption.|
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