# SDR UIEA200600184

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 22, 2006
- Submitted: August 2, 2006
- Operation: Air carrier
- Aircraft: [N492MC](https://openairdocs.org/aircraft/N492MC), registered now
- Make and model: Boeing 747-47UF
- Registry model: [Boeing 747-47UF](https://openairdocs.org/model/boeing-747-47uf) (OpenAirDocs)
- Aircraft serial: 29253
- Aircraft time: 33,147 hours, 6,643 cycles
- Engine: Ge CF680C2*
- Engine time: 31,121 hours, 6,182 cycles
- System (JASC): [7530 · Compressor Bleed Control](https://openairdocs.org/jasc/7530)
- Part: Actuator
- Part number: 1211342005
- Part serial: APMRV214
- Condition: Malfunctioned
- Location: Nr 2 Engine
- Stage of operation: TO
- How discovered: O
- Nature of condition: J
- Precautionary procedure: C
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/UIEA200600184

## Discrepancy

NR 2 ENGINE FUEL CONTROL STATUS MSG, AFTER LOW SPEED ABORT.  ENGINE NR 2 N1 78.5 MAX AT T/O ROLL OTHER ENGINES NORMAL.  REMOVED AND REPLACED RT VSV ACTUATOR IAW AMM 75-31-02, DUE ON VISUAL INSP FOUND CLEVIS END DETACHED FROM ACTUATOR ASSY.  ENGINE TEST 12 COMPLIED PASS, REF 71-00-00-705-246-J00.  ENGINE RUN, LEAK CHECK C/W SATIS IAW AMM 71-00-00, ADJ/TEST.

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