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|
Attributes | |
ACN | 961835 |
Time | |
Date | 201107 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Aircraft 1 | |
Make Model Name | EMB ERJ 145 ER&LR |
Operating Under FAR Part | Part 121 |
Flight Phase | Takeoff |
Component | |
Aircraft Component | Fuel Booster Pump |
Person 1 | |
Function | First Officer |
Qualification | Flight Crew Commercial |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Published Material / Policy |
Narrative:
All checklists were read and had been complied with; to my knowledge; per emb aom volume 1. At approximately 75 KTS during takeoff roll; the captain stated abort; abort; abort; and a low speed abort procedure was executed. An EICAS message said #1 engine fuel low press; which is what prompted the captain to issue the abort. However; there was never an oral caution; or master caution warning associated with the message; the captain just so happened to see the message during the takeoff roll. After exiting the runway; we assessed that the #1 engine electric fuel pump was off; which explained the associated message. We turned the fuel pump on and taxied back to the end of the runway and prepared for takeoff. We did have to wait approximately ten minutes for the brakes to return into the green range for takeoff. The rest of the flight was non eventful.fuel pumps are an item on the engine start checklist. I read the checklist; and the captain responded as normal. It is now evident that the #1 engine fuel pump was not turned on during this checklist; even though the captain responded that both were on. As a crewmember; I failed to double check that the captain's responses matched the actual switch configuration for the #1 fuel pump.
Original NASA ASRS Text
Title: Takeoff was rejected when an EICAS message for #1 ENG FUEL LOW PRESS displayed. The electric fuel pump switch was found in the incorrect off position.
Narrative: All checklists were read and had been complied with; to my knowledge; per EMB AOM volume 1. At approximately 75 KTS during takeoff roll; the Captain stated ABORT; ABORT; ABORT; and a low speed abort procedure was executed. An EICAS message said #1 ENG FUEL LOW PRESS; which is what prompted the Captain to issue the abort. However; there was never an oral caution; or master caution warning associated with the message; the Captain just so happened to see the message during the takeoff roll. After exiting the runway; we assessed that the #1 engine electric fuel pump was off; which explained the associated message. We turned the fuel pump on and taxied back to the end of the runway and prepared for takeoff. We did have to wait approximately ten minutes for the brakes to return into the green range for takeoff. The rest of the flight was non eventful.Fuel pumps are an item on the Engine Start Checklist. I read the checklist; and the Captain responded as normal. It is now evident that the #1 engine fuel pump was not turned on during this checklist; even though the Captain responded that both were on. As a crewmember; I failed to double check that the Captain's responses matched the actual switch configuration for the #1 fuel pump.
Data retrieved from NASA's ASRS site as of April 2012 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.