# SDR 07FDEA05051

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 13, 2007
- Submitted: December 17, 2007
- Operation: Air carrier
- Aircraft: [N650FE](https://openairdocs.org/aircraft/N650FE), 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: 726
- Aircraft time: 20,840 hours, 10,777 cycles
- System (JASC): [3413 · Rate of Climb Indicator](https://openairdocs.org/jasc/3413)
- Part: Pin
- Part number: C6646120
- Condition: Sheared
- Stage of operation: CR
- How discovered: O
- Nature of condition: J, G, S
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/07FDEA05051

## Discrepancy

F/O TAT FAILED, CAUSING SECONDARY LOSS OF NR 2 PITCH TRIM, NR 2 CABIN PRESS REGULATOR 34-62 0508.  NR 2 INTERMITTENT FOUND PROX  SYS FAULTING SENSOR.  REF:MDIS  32 10 0511, BOLT/PIN BROKEN ON RT MLG AT DRAG LINK ATTACHMENT FOR GEAR SENSORS.  REMOVED AND REPLACED 62GB SENSOR PER AMM 32-61-00. CLEARED   FAULT CODES AND BITE TEST ON PROX BOX SHOWS NO FAULTS.GROUND SCAN AUTOPILOT SYSTEM PASSED WITH NO FAULTS.

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