# SDR FDEA200812135138

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 13, 2008
- Submitted: December 16, 2008
- Operation: Air carrier
- Aircraft: [N668FE](https://openairdocs.org/aircraft/N668FE), registered now
- Make and model: Airbus A300 F4-605R
- Registry model: [Airbus A300 F4-605R](https://openairdocs.org/model/airbus-industrie-a300-f4-605r) (OpenAirDocs)
- Aircraft serial: 772
- Aircraft time: 19,049 hours, 10,220 cycles
- System (JASC): [2897 · Fuel System Wiring](https://openairdocs.org/jasc/2897)
- Part: Wire
- Condition: Damaged
- Location: Fuel System
- Stage of operation: CL
- How discovered: O
- Nature of condition: O
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA200812135138

## Discrepancy

DURING CLIMB THRU 18K, LOW FUEL QTY DECREASING AT APPX 500-1000 LBS/MIN, THIS WAS ON THE ECAM & OVHD PANEL.  REF QRH, "POSSIBLE FUEL LEAK" PULLED FQI CHAN SUPPLY 1 2 C/B'S.  WHEN FQI RETURNED LOW RESUMED IT'S STEADY DECREASE.  AFTER LANDING, ALL FUEL IND'S RETURNED TO NORMAL.  ACFT RELEASED FOR SERVICE PER MEL/CDL: 28-42-01-01 RELEASED FOR SERVICE.  BITE TEST OF CGCC & FUEL QTY COMPUTER NORMAL.  DEPINNED SHIELDED WIRE PIN -W FOR INSPECTION & TWO SHIELD WIRES THAT WERE PIGGY-BACKED TO IT PULLED OUT OF THE SOLDER. RETERMINATED SOCKET FOR CENTER CONDUCTOR AND REASSEMBLED SOLDER SLEEVE FOR SHIELD & TWO PIGGY-BACKED WIRES.

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