AS1852A Nozzles and Ports - Gravity Fueling Interface Standard for Civil Aircraft

Revised

02/01/1988

Features
Issuing Committee
Scope
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS1852A
Pages
1
Citation
SAE International Technical Standard, Nozzles and Ports - Gravity Fueling Interface Standard for Civil Aircraft, SAE Standard AS1852A, Revised February 1988, Issued December 1984, https://doi.org/10.4271/AS1852A.
Additional Details
Publisher
Published
Feb 1, 1988
Product Code
AS1852A
Content Type
Technical Standard
Status
Revised
Language
English

Revisions