37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
|
Attributes | |
ACN | 1539651 |
Time | |
Date | 201805 |
Local Time Of Day | 0001-0600 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | IMC |
Light | Night |
Aircraft 1 | |
Make Model Name | DC-10 Undifferentiated or Other Model |
Operating Under FAR Part | Part 121 |
Flight Phase | Cruise |
Flight Plan | IFR |
Component | |
Aircraft Component | RPM/N1/N2/Etc Indication |
Person 1 | |
Function | Captain Pilot Flying |
Qualification | Flight Crew Air Transport Pilot (ATP) |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe |
Narrative:
At 10;000 ft and 280 kts with autopilot and autothrottles engaged we saw engines 1&2 N1's cycle to idle as engine 3 N1 exceeded its limit; we saw as much as 124%. Upon seeing this I disconnected the auto throttles and moved throttle lever #3 to idle. The first officer reviewed the QRH for the indicated engine 3 exceedance. Not sure if this was real or just an indication issue we left throttle #3 at idle and operated the rest of the flight with throttles 1&2 only. Throughout the rest of the flight with the #3 throttle at idle we noticed the N1 indication for that engine continued to fluctuate even as high as 70%. We [advised] ATC and were given vectors to the ILS. We executed an autoland.
Original NASA ASRS Text
Title: MD-10 Captain reported that one of the engines had an erratic N1 indication.
Narrative: At 10;000 ft and 280 kts with autopilot and autothrottles engaged we saw engines 1&2 N1's cycle to idle as engine 3 N1 exceeded its limit; we saw as much as 124%. Upon seeing this I disconnected the auto throttles and moved throttle lever #3 to idle. The FO reviewed the QRH for the indicated ENG 3 EXCEEDANCE. Not sure if this was real or just an indication issue we left throttle #3 at idle and operated the rest of the flight with throttles 1&2 only. Throughout the rest of the flight with the #3 throttle at idle we noticed the N1 indication for that engine continued to fluctuate even as high as 70%. We [advised] ATC and were given vectors to the ILS. We executed an autoland.
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.