Nozzles and Ports - Gravity Fueling Interface Standard for Civil Aircraft

Standard:
Revised:
  • 2006-03-24
 
  • HISTORICAL Access the latest revision: AS1852D
Publisher:
  • SAE International
Pages:
5
Scope:

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.

Rationale:

New Diesel engines and turbine airplanes that require use of turbine fuel only, require the addition of a new airplane refueling port to the standard.

History:
Standard Published Revision Status
AS1852D 2012-01-03 Latest Stabilized
2006-03-24 Historical Revised
1997-08-01 Historical Revised
1988-02-01 Historical Revised
1984-12-01 Historical Issued
AKA:
  • SAE AS 1852
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