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Attributes | |
ACN | 1572630 |
Time | |
Date | 201808 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Light | Daylight |
Aircraft 1 | |
Make Model Name | B737-800 |
Operating Under FAR Part | Part 121 |
Flight Phase | Taxi |
Flight Plan | IFR |
Component | |
Aircraft Component | Engine Starting System |
Person 1 | |
Function | Captain Pilot Flying |
Qualification | Flight Crew Instrument Flight Crew Multiengine Flight Crew Air Transport Pilot (ATP) |
Experience | Flight Crew Last 90 Days 354 |
Person 2 | |
Function | Pilot Not Flying First Officer |
Qualification | Flight Crew Multiengine Flight Crew Air Transport Pilot (ATP) Flight Crew Instrument |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe Deviation - Procedural Published Material / Policy |
Narrative:
We were pushing back from the gate in a maximum 8 and were starting the number 2 engine. The first officer (first officer) configured the air conditioning panel before the tick on the egt was gone; causing the eec (electronic engine controller) to abort the engine start. Once we saw the white box flashing; we aborted the engine start; reviewed the qrc; and followed the QRH guidance. After confirming with maintenance (and a review of the [operation manual]) a second successful start was made.we conducted a briefing about the maximum engine start and the items that we were going to see; and time limits associated during our normal preflight briefings. I was very surprised when the aborted start happened due to the fact that we had reviewed the start process. I will continue to brief the engine start procedures with a bigger emphasis on the egt roll back.
Original NASA ASRS Text
Title: B737 MAX-8 crew reported failing to follow the engine start procedure resulting in an aborted engine start.
Narrative: We were pushing back from the gate in a MAX 8 and were starting the number 2 engine. The FO (First Officer) configured the air conditioning panel before the tick on the EGT was gone; causing the EEC (Electronic Engine Controller) to abort the engine start. Once we saw the white box flashing; we aborted the engine start; reviewed the QRC; and followed the QRH guidance. After confirming with Maintenance (and a review of the [operation manual]) a second successful start was made.We conducted a briefing about the MAX engine start and the items that we were going to see; and time limits associated during our normal preflight briefings. I was very surprised when the aborted start happened due to the fact that we had reviewed the start process. I will continue to brief the engine start procedures with a bigger emphasis on the EGT roll back.
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.