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|
Attributes | |
ACN | 1715418 |
Time | |
Date | 202001 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZ.TRACON |
State Reference | US |
Environment | |
Flight Conditions | IMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | EMB ERJ 170/175 ER/LR |
Operating Under FAR Part | Part 121 |
Flight Phase | Takeoff |
Flight Plan | IFR |
Component | |
Aircraft Component | Engine Vibration Indication |
Person 1 | |
Function | First Officer Pilot Flying |
Qualification | Flight Crew Air Transport Pilot (ATP) Flight Crew Multiengine Flight Crew Instrument |
Person 2 | |
Function | Pilot Not Flying Captain |
Qualification | Flight Crew Air Transport Pilot (ATP) Flight Crew Instrument Flight Crew Multiengine |
Events | |
Anomaly | Aircraft Equipment Problem Critical |
Narrative:
Flight XXXX from ZZZ to ZZZ1; returned to field right after departing ZZZ. Shortly after takeoff; the captain and I noticed high vibration on engine #2 lp as we climbed through 5;000 - 6;000 feet. Initially; the vibration fluctuated between normal range (green) to amber (caution) range. However; after several seconds; it remained in the caution range. We contacted ATC to level out at 6;000 ft and delay vectors while we ran the QRH checklist. Upon completion of the QRH procedure we kept engine #2 vibration in normal range. The captain and I both came upon the decision to return to ZZZ. There were two previous occurrences of engine vibration on engine # 2 in the aml within the last week. We felt it was prudent to return to ZZZ because we did not want to make any more high power demands; i.e. Climb; with the issue at hand. We requested delay vectors to burn off the fuel in order get below max landing weight limitations. ATC vectored us around; and we successfully landed at ZZZ. No emergency was declared. We returned to the field as it [was the] safest decision to do. With two previous documented occurrences of high engine vibration on #2; we did not want to risk another occurrence. By continuing our climb from 6;000 ft to cruising altitude; it puts the engine in a higher power demand with a high probability of another occurrence.
Original NASA ASRS Text
Title: EMB-175 flight crew experienced a high engine vibration during climbout. A precautionary air return was made to the departure airport.
Narrative: Flight XXXX from ZZZ to ZZZ1; returned to field right after departing ZZZ. Shortly after takeoff; the Captain and I noticed high vibration on Engine #2 LP as we climbed through 5;000 - 6;000 feet. Initially; the vibration fluctuated between normal range (green) to amber (caution) range. However; after several seconds; it remained in the caution range. We contacted ATC to level out at 6;000 ft and delay vectors while we ran the QRH checklist. Upon completion of the QRH procedure we kept Engine #2 vibration in normal range. The Captain and I both came upon the decision to return to ZZZ. There were two previous occurrences of engine vibration on Engine # 2 in the AML within the last week. We felt it was prudent to return to ZZZ because we did not want to make any more high power demands; i.e. climb; with the issue at hand. We requested delay vectors to burn off the fuel in order get below max landing weight limitations. ATC vectored us around; and we successfully landed at ZZZ. No emergency was declared. We returned to the field as it [was the] safest decision to do. With two previous documented occurrences of high engine vibration on #2; we did not want to risk another occurrence. By continuing our climb from 6;000 ft to cruising altitude; it puts the engine in a higher power demand with a high probability of another occurrence.
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.