13,241
edits
(→C: + CTOT, Calculated take-off time) |
(→E: + ECEF – Earth-Centred, Earth-Fixed coordinate system) |
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| EAT || <u>E</u>stimated <u>A</u>rrival <u>T</u>ime | | EAT || <u>E</u>stimated <u>A</u>rrival <u>T</u>ime | ||
|- | |||
| ECEF || <u>E</u>arth-<u>C</u>entred, <u>E</u>arth-<u>F</u>ixed coordinate system || Cartesian 3D coordinate system with origo at the Earth's center of mass and x axis intersecting 0°E, 0°N | |||
|- | |- | ||
| EDT || <u>E</u>stimated <u>D</u>eparture <u>T</u>ime | | EDT || <u>E</u>stimated <u>D</u>eparture <u>T</u>ime | ||
|- | |- | ||
| EFATO || <u>E</u>ngine <u>f</u>ailure <u>a</u>fter <u>t</u>ake <u>o</u>ff || | | EFATO || <u>E</u>ngine <u>f</u>ailure <u>a</u>fter <u>t</u>ake <u>o</u>ff || Usually resulting in a force-landing. | ||
|- | |- | ||
| EFIS || <u>E</u>lectronic <u>F</u>light <u>I</u>nstrument <u>S</u>ystem || | | EFIS || <u>E</u>lectronic <u>F</u>light <u>I</u>nstrument <u>S</u>ystem || Combination of displays (PFD and MFD) with autopilot | ||
|- | |- | ||
| EICAS || [http://en.wikipedia.org/wiki/Eicas <u>E</u>ngine <u>I</u>ndication and <u>C</u>rew <u>A</u>lerting <u>S</u>ystem] | | EICAS || [http://en.wikipedia.org/wiki/Eicas <u>E</u>ngine <u>I</u>ndication and <u>C</u>rew <u>A</u>lerting <u>S</u>ystem] |