# SDR U0GA125467

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 25, 2009
- Submitted: August 21, 2009
- Operation: Air carrier
- Aircraft: N358EH
- Make and model: Bell 212
- Registry model: [Bell 212](https://openairdocs.org/model/bell-212) (OpenAirDocs)
- Aircraft serial: 31211
- Engine: Pwa PT6T3
- System (JASC): [7200 · Engine (Turbine/Turboprop)](https://openairdocs.org/jasc/7200)
- Part: Engine
- Condition: Stopped
- Location: Nr 1
- Stage of operation: CL
- How discovered: O
- Nature of condition: Y, J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/U0GA125467

## Discrepancy

DURING A NEW HIRE INITIAL TRAINING FLIGHT, NR 1 ENGINE QUIT.  DEPARTED A CONFINED AREA WITH A SIMULATED ENGINE FAILURE OF THE NR 2 ENGINE.  THE SIMULATED NR 2 ENGINE FAILURE WAS INDUCED BY THE INSTRUCTOR WITH PLENTY OF OBSTACLE CLEARANCE PAS VTOCS, ACCELERATING TO VY.  ALSO THE NR 2 THROTTLE WAS ROLLED BACK ONLY PARTIALLY AS A SAFETY PRECAUTION.  OUR FIRST INDICATION WAS A "BANG" WITH A SPOOL DOWN OF N1 AND A NR 1 ENG OUT LIGHT.  WHILE PILOT FLYING (PF) CONTINUED TO CLIMB AT VY, THE PILOT MONITORING (PM) CALLED OUT SINGLE ENGINE FAILURE, CHECKED NR, WHILE SIMULTANEOUSLY ROLLED THE PARTIALLY RETARDED.

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