# SDR CA110611004

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 7, 2011
- Submitted: September 9, 2011
- Operation: Air carrier
- Make and model: Bell 212
- Registry model: [Bell 212](https://openairdocs.org/model/bell-212) (OpenAirDocs)
- Aircraft time: 13,606 hours
- Engine: Pwa PT6T3B
- System (JASC): [7310 · Engine Fuel Distribution](https://openairdocs.org/jasc/7310)
- Part: Lock Plate
- Part number: 3011158
- Condition: Bent
- Location: Transfer Tube
- Stage of operation: HO
- How discovered: O
- Nature of condition: R, J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA110611004

## Discrepancy

FUEL TRANSFER TUBE DISENGAGED FROM FUEL NOZZLE ALLOWING UN-RESTRICTED HIGH PRESSURE FUEL LEAKAGE.  THE FUEL TRANSFER TUBE LOCK PLATE AT THE NR 6 FUEL NOZZLE LOCATION ON THE NR 1 ENGINE HAD NOT BEEN CORRECTLY INSTALLED 353.2 HOURS PREVIOUS DURING A SCHEDULED NOZZLE CHANGE.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.