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B-757 captain reported a rejected takeoff due to an engine bleed fault message.
| Attributes | |
| ACN | 1616654 |
| Time | |
| Date | 201902 |
| Local Time Of Day | 1801-2400 |
| Environment | |
| Flight Conditions | Marginal |
| Aircraft 1 | |
| Make Model Name | B757-200 |
| Operating Under FAR Part | Part 121 |
| Flight Phase | Takeoff |
| Flight Plan | IFR |
| Component | |
| Aircraft Component | Pneumatic Valve/Bleed Valve |
| Person 1 | |
| Function | Captain Pilot Flying |
| Qualification | Flight Crew Air Transport Pilot (ATP) Flight Crew Instrument Flight Crew Multiengine |
| Events | |
| Anomaly | Aircraft Equipment Problem Less Severe |
Narrative:
On takeoff roll (max power due to environmental conditions); and at approximately 80 knots; PF (pilot flying) noticed amber EICAS message right engine hi stage alert. Pm (pilot monitoring) was making the '80 knots call' and noticed immediately the alert also. PF announced and performed rejected takeoff procedure.minimum brake was used due to very strong headwind component and lighter than usual aircraft; and the distance to the runway exiting taxiway. Aircraft was slowly taxied to the next available exiting taxiway.PF taxied aircraft to parking. During taxi; pm reviewed the engine hi stage QRH checklist. However; with synergetic input from the PF; it was decided to wait until parking at the gate to see if maintenance personnel would like to troubleshoot the issue with the engine configuration at time of the failure.all other operational procedures were performed and the aircraft was secured at the ramp.
Original NASA ASRS Text
Title: B-757 Captain reported a rejected takeoff due to an engine bleed fault message.
Narrative: On takeoff roll (Max Power due to environmental conditions); and at approximately 80 knots; PF (Pilot Flying) noticed Amber EICAS Message R ENG HI STAGE alert. PM (Pilot Monitoring) was making the '80 knots call' and noticed immediately the alert also. PF announced and performed rejected takeoff procedure.Minimum brake was used due to very strong headwind component and lighter than usual aircraft; and the distance to the runway exiting taxiway. Aircraft was slowly taxied to the next available exiting taxiway.PF taxied aircraft to parking. During taxi; PM reviewed the ENG HI STAGE QRH checklist. However; with synergetic input from the PF; it was decided to wait until parking at the gate to see if Maintenance personnel would like to troubleshoot the issue with the engine configuration at time of the failure.All other operational procedures were performed and the aircraft was secured at the ramp.
Data retrieved from NASA's ASRS site 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.