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37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
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| Attributes | |
| ACN | 863383 |
| Time | |
| Date | 200912 |
| Local Time Of Day | 1801-2400 |
| Place | |
| Locale Reference | ZZZ.Airport |
| State Reference | US |
| Environment | |
| Flight Conditions | VMC |
| Light | Night |
| Aircraft 1 | |
| Make Model Name | SF 340B |
| Operating Under FAR Part | Part 121 |
| Flight Phase | Descent |
| Flight Plan | IFR |
| Component | |
| Aircraft Component | Turbine Engine |
| Person 1 | |
| Function | Pilot Flying First Officer |
| Qualification | Flight Crew Commercial |
| Experience | Flight Crew Last 90 Days 33 Flight Crew Total 3300 Flight Crew Type 1200 |
| Person 2 | |
| Function | Pilot Not Flying Captain |
| Qualification | Flight Crew Air Transport Pilot (ATP) |
| Experience | Flight Crew Last 90 Days 33 Flight Crew Total 3700 Flight Crew Type 1500 |
| Events | |
| Anomaly | Aircraft Equipment Problem Critical |
Narrative:
Shortly after leaving cruise altitude of 21;000 the left engine experienced a compressor stall. After initiating the descent I (flying pilot) reduced the power levers to approximately 50-60 % torque which is when the compressor stall occurred. We both noticed that the ignition light has come on and there were audible pops. As we were initiating the emergency non-normal card; I reduced the power further after noting a high itt; and the itt over temp light was on for approx 5 seconds. After reducing the power to approximately 30-40% the stall stopped and we finished the emergency non-normal card and checklist. After finishing the emergency non-normal checklists we continued the descent; notified the flight attendant and passengers and conduced a normal visual landing with no further abnormalities.
Original NASA ASRS Text
Title: An SF-340 Flight Crew experienced a compressor stall on descent. They ran the procedure and landed without incident.
Narrative: Shortly after leaving cruise altitude of 21;000 the left engine experienced a compressor stall. After initiating the descent I (flying pilot) reduced the power levers to approximately 50-60 % torque which is when the compressor stall occurred. We both noticed that the ignition light has come on and there were audible pops. As we were initiating the emergency non-normal card; I reduced the power further after noting a high ITT; and the ITT over temp light was on for approx 5 seconds. After reducing the power to approximately 30-40% the stall stopped and we finished the emergency non-normal card and checklist. After finishing the emergency non-normal checklists we continued the descent; notified the flight attendant and passengers and conduced a normal visual landing with no further abnormalities.
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.