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Attributes | |
ACN | 913205 |
Time | |
Date | 201010 |
Local Time Of Day | 0601-1200 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Light | Dawn |
Aircraft 1 | |
Make Model Name | B737-800 |
Operating Under FAR Part | Part 121 |
Flight Phase | Takeoff |
Component | |
Aircraft Component | Engine Control |
Person 1 | |
Function | Pilot Not Flying First Officer |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe Deviation - Procedural Published Material / Policy |
Narrative:
We had return to the gate for a mechanical problem which maintenance fixed. We ran the checklist again; started and taxied normally. During the takeoff roll we got a master caution light which I inadvertently and instinctively punched off. The speed was 90 KTS. There were no high speed abort item indications. In flight; we discovered that we left the probe heat switches off; which we then turned on. Also; both engine eec's [engine electronic control] were in alternate mode. We ran the QRH procedure and selected alternate on the eec's switches. We suspected that the probe heat switches off triggered the eec's to automatically switch to alternate. No engine parameters were exceeded and the eec's reset normally at our destination.checklist discipline; review abort parameters and procedures.
Original NASA ASRS Text
Title: B737-800 First Officer reports forgetting to turn on the probe heat switches prior to takeoff after returning to the gate for maintenance. Lack of probe heat apparently caused the EEC's to revert to alternate mode triggered a master caution during takeoff which was investigated airborne.
Narrative: We had return to the gate for a mechanical problem which maintenance fixed. We ran the checklist again; started and taxied normally. During the takeoff roll we got a master caution light which I inadvertently and instinctively punched off. The speed was 90 KTS. There were no high speed abort item indications. In flight; we discovered that we left the probe heat switches off; which we then turned on. Also; both engine EEC's [Engine Electronic Control] were in alternate mode. We ran the QRH procedure and selected alternate on the EEC's switches. We suspected that the probe heat switches off triggered the EEC's to automatically switch to alternate. No engine parameters were exceeded and the EEC's reset normally at our destination.Checklist discipline; review abort parameters and procedures.
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.