Summary
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.
Technical characteristics
| Publisher | SAE International |
| Publication Date | 12/18/2020 |
| Page Count | 5 |
| Themes | Aerospace |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
Replaces
05/02/2013
Superseded
, Reaffirmed
Historical