# SDR FDEA202011142842

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 14, 2020
- Submitted: November 17, 2020
- Operation: Air carrier
- Aircraft: [N726FD](https://openairdocs.org/aircraft/N726FD), registered now
- Make and model: Airbus A300 B4-622R
- Registry model: [Airbus A300 B4-622R](https://openairdocs.org/model/airbus-a300-b4-622r) (OpenAirDocs)
- Aircraft serial: 575
- Aircraft time: 55,348 hours, 28,971 cycles
- System (JASC): [2613 · Overheat Detection](https://openairdocs.org/jasc/2613)
- Part: Sensing Element
- Part number: 3551848400
- Condition: Failed
- Location: Overheat
- Stage of operation: CL
- How discovered: O
- Nature of condition: N
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA202011142842

## Discrepancy

DURNING CLIMBOUT ENGINE NO 1 BLEED LEAK, DIVERTED INTO TPA BECAUSE WE LOST PRESSURIZATION DUE TO DEFERRED NO 2 PACK, DECLARED EMERGENCY.  FACT 15NOV20 16:06 TPA.  R & R MANIFOLD OVERHEAT SENSING ELEMENT ON LT WING PYLON I/R/T MM 36-22-12-04, REMOVAL P/N 35518-48-400 FENWALL, NSN, INSTALLED S/N IS BMM8825, P/N 35518-48-400 FENWALL.  RAN ENGINE I/R/T JRH CHAP 5, NO DISCREPANCY'S NOTED, NO FAULTS.  PREFORMED OPERATIONAL TEST I/R/T MM 39-22-00, ALL TEST GOOD.

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