This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Nozzles and Ports – Gravity Fueling Interface Standards for Civil Aircraft
- Aerospace Standard
Published January 03, 2012 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This SAE Aerospace Standard (AS) defines the maximum allowable free opening dimensions for airframe fueling ports on civil aircraft that require the exclusive use of gasoline as an engine fuel, and the minimum free opening dimensions for airframe fueling ports on civil aircraft that operate with turbine fuels as the primary fuel type and with gasoline as the emergency fuel type. This SAE Aerospace Standard (AS) also defines the features and dimensions for airframe refueling ports on civil aircraft that require the exclusive use of turbine fuel as an engine fuel.
In addition, this document defines the minimum fuel nozzle spout dimensions for turbine fuel ground service equipment, and the maximum fuel nozzle spout diameter for gasoline ground service equipment.
This document has been determined to contain basic and stable technology which is not dynamic in nature.
|Aerospace Standard||Standard Test Procedure and Limit Value for Shutoff Surge Pressure of Pressure Fuel Dispensing Systems|
|Aerospace Standard||Turbine Flowmeter Fuel Flow Calculations|
|Technical Paper||Aircraft Super Integrated Power Unit|
Data Sets - Support Documents
|TABLE 1||Airframe Fueling Ports|
|TABLE 2||Ground Fueling Nozzle Spouts|
* 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.