37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
|
Attributes | |
ACN | 1194248 |
Time | |
Date | 201408 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZZ.Airport |
State Reference | FO |
Environment | |
Flight Conditions | IMC |
Aircraft 1 | |
Make Model Name | B767-300 and 300 ER |
Operating Under FAR Part | Part 121 |
Flight Phase | Takeoff |
Component | |
Aircraft Component | Turbine Engine |
Person 1 | |
Function | First Officer Pilot Flying |
Qualification | Flight Crew Air Transport Pilot (ATP) |
Experience | Flight Crew Total 14500 |
Person 2 | |
Function | Captain Pilot Not Flying |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Altitude Overshoot Deviation - Speed All Types |
Narrative:
I was the pilot flying on this flight we took-off and were flying the departure. We started to clean-up at 3;000 ft AGL and commenced an approximate 60 degree right hand turn for the SID. We were cleared to 6;000 ft as per the SID. I was hand-flying the aircraft during the departure and throttles were being commanded with auto-throttle. About this same time; the plane entered IMC with choppy ride conditions. During the last part of the turn; as we were rolling out; flaps were retracted to zero. It was at this point; as we were climbing to 6;000; in choppy ride conditions; that we encountered a stick shaker warning. I immediately lowered the nose; power was advanced; and the warning ceased. As power was advanced; it was then that we discovered the right engine RPM had rolled back in an apparent compressor stall. As per the checklist; the right thrust lever was immediately retarded to idle as the left thrust lever was advanced to save airspeed. We tried advancing the right thrust lever after a short wait but encountered a secondary compressor stall after moving the thrust lever only a small amount. Once again; the right thrust lever was retarded back to idle. During the troubleshooting process for the compressor stall and then trying to fly a very heavy; performance limited aircraft on a single engine; our altitude varied slightly between 4;800 ft and 5;300 ft on the SID. We subsequently declared an emergency with departure control and elected to remain at 5;000 ft for our return for an overweight landing. Approach control vectored us around for our arrival and ILS approach. We completed our emergency checklists; dumped a slight amount of fuel (with approval from approach control) and conducted an ILS approach. During the vectoring for our arrival; we tried advancing the right thrust lever one more time; and this time; power came back normally. We subsequently landed with both engines working normally. Landing and taxi-in were normal and uneventful. Continue to emphasize engine failures/compressor stalls not only immediately after take-off but also in a turn and in the weather during training. This type of failure is very insidious and potentially dangerous.
Original NASA ASRS Text
Title: B767 flight crew experiences an engine rollback climbing out of 5;000 FT that result in a large yaw angle and a momentary stick shaker. The thrust lever for the affected engine is brought to idle and attempts to increase thrust are not successful. An emergency is declared; some fuel is dumped and the flight returns to the departure airport. While being vectored for approach the thrust lever is advanced again and the engine responds normally.
Narrative: I was the pilot flying on this Flight We took-off and were flying the departure. We started to clean-up at 3;000 FT AGL and commenced an approximate 60 degree right hand turn for the SID. We were cleared to 6;000 FT as per the SID. I was hand-flying the aircraft during the departure and throttles were being commanded with auto-throttle. About this same time; the plane entered IMC with choppy ride conditions. During the last part of the turn; as we were rolling out; flaps were retracted to zero. It was at this point; as we were climbing to 6;000; in choppy ride conditions; that we encountered a stick shaker warning. I immediately lowered the nose; power was advanced; and the warning ceased. As power was advanced; it was then that we discovered the right engine RPM had rolled back in an apparent compressor stall. As per the checklist; the right thrust lever was immediately retarded to idle as the left thrust lever was advanced to save airspeed. We tried advancing the right thrust lever after a short wait but encountered a secondary compressor stall after moving the thrust lever only a small amount. Once again; the right thrust lever was retarded back to idle. During the troubleshooting process for the compressor stall and then trying to fly a very heavy; performance limited aircraft on a single engine; our altitude varied slightly between 4;800 FT and 5;300 FT on the SID. We subsequently declared an emergency with Departure Control and elected to remain at 5;000 FT for our return for an overweight landing. Approach Control vectored us around for our arrival and ILS approach. We completed our emergency checklists; dumped a slight amount of fuel (with approval from Approach Control) and conducted an ILS approach. During the vectoring for our arrival; we tried advancing the right thrust lever one more time; and this time; power came back normally. We subsequently landed with both engines working normally. Landing and taxi-in were normal and uneventful. Continue to emphasize engine failures/compressor stalls not only immediately after take-off but also in a turn and in the weather during training. This type of failure is very insidious and potentially dangerous.
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.