# SDR FDEA201005031429

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 3, 2010
- Submitted: May 3, 2010
- Operation: Air carrier
- Aircraft: [N658FE](https://openairdocs.org/aircraft/N658FE), 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: 752
- Aircraft time: 22,440 hours, 11,916 cycles
- Engine: Ge CF680C2A5F
- System (JASC): [5420 · Nacelle/Pylon Miscellaneous Structure](https://openairdocs.org/jasc/5420)
- Part: Web
- Part number: A5461106820000
- Condition: Cracked
- Location: Zone 400
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA201005031429

## Discrepancy

NR 2 ENG /PYLON---PYLON WEB STRUCTURE IS CRACKED IN 2 PLACES AS SEEN THROUGH NACELLE ACCESS PANEL 421 CL.  STOP DRILLED CRACKS IAW SRM 54-52-11.  INSTALLED REPAIR IAW SRM 54-21-11, FIG 201, PGS 205 / 206, CONFIG 2 AND SRM 51-40-30.  DISPLACED AND REINSTALLED WIRE BUNDLE IAW SRM 51-40-21, PARA 5.  DISCONNECTED AND REINSTALLED GROUND WIRES ON UPPER PYLON AFT WALL IAW ESPM 20-23-11-0.  OPS CHECK GOOD ON ENGINE BLEED AIR SYS IAW AMM 36-11-00-5.  PERFORMED NR 2 ENGINE IDLE CHECK IAW AMM 71-00-00, CHECKS GOOD..

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