# SDR QMLA2017100717102

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 7, 2017
- Submitted: October 10, 2017
- Operation: Air carrier
- Aircraft: [N135CJ](https://openairdocs.org/aircraft/N135CJ), registered now
- Make and model: Urocop EC135T2
- Registry model: [Urocop EC135T2](https://openairdocs.org/model/eurocopter-deutschland-ec135t2) (OpenAirDocs)
- Aircraft serial: 0495
- Aircraft time: 3,342 hours, 12,832 cycles
- System (JASC): [2700 · Flight Control System](https://openairdocs.org/jasc/2700)
- Part: Warning Light
- Condition: Illuminated
- Location: Nr 2 Inverter
- Stage of operation: AA
- How discovered: O
- Nature of condition: J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/QMLA2017100717102

## Discrepancy

DURING FLIGHT,  THE DG,  NR 2 INVERTER, AND PR SAS ILLUMINATED ON THE CAD AND THE NR 2 GENERATOR AMPS WERE RUNNING ABOUT 20 AMPS HIGHER THAN THE NR 1 GENERATOR.  THE AIRCRAFT BECAME UNSTABLE LIKE IT LOST ALL OF STABILITY. GOT EVERYTHING TO CLEAR ON THE CAD. DURING THE TURN, RECEIVED THE DG, NR 2 INVERTER AND PR SAS ON THE CAD.  AT THIS POINT,  WAS 5 MILES FROM BASE SO ELECTED TO RETURN AND HAVE ANOTHER AIRCRAFT FINISH THE TRANSPORT.   LANDED WITHOUT ANY ISSUES. THE PR SAS AND NR 2 INVERTER WOULD NOT CLEAR. THE MECHANIC INSPECTED THE SYSTEM. THE AIRCRAFT WAS SUBSEQUENTLY RETURNED TO SERVICE WITH THE NR 2 INVERTER SYSTEM DEFERRED. OPEN

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