# SDR FDEA201009303801

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 30, 2010
- Submitted: September 30, 2010
- Operation: Air carrier
- Aircraft: N411FE
- Make and model: Airbus A310-203
- Registry model: [Airbus A310-203](https://openairdocs.org/model/airbus-industrie-a310-203) (OpenAirDocs)
- Aircraft serial: 359
- Aircraft time: 36,500 hours, 21,133 cycles
- Engine: Ge CF680A3
- System (JASC): [5340 · Fuselage Main, Attach Fittings](https://openairdocs.org/jasc/5340)
- Part: Fitting
- Part number: A53778669206
- Condition: Corroded
- Location: Zone 100
- Part time: 36,500 hours, 21,133 cycles
- 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/FDEA201009303801

## Discrepancy

134AR ACCESS DOOR SURROUNDING INTEGRAL FITTING FOUND CORROSION (FR23-  24, STGR49R-STGR54L)   REMOVE CORROSION IAW SRM 51-74-10.  MEASURE THE REMAINING THICKNESS IAW NTM51-10-04 AND NTM51-10-08 CHECK FOR CRACK.  MAKE THE REPAIR PARTS IAW SRM53-13-12-201 REPAIR NR 4.   HEAT TREAT THE REPAIR PARTS FROM 2024-0 TO 2024-T42 CONDITION IAW SRM51-25-00.   DRILL FASTENER HOLES AND DEBURR IAW SRM 51-40-40.   APPLY ALODINE TO THE REPAIR PARTS AND REPAIR AREA IAW SRM51-21-10 AND SRM51-23-00 APPLY PAINT.   INSTALL THE REPAIR PARTS IAW SRM 51-40-21.   APPLY SEALANT TO THE REPAIR AREA IAW SRM 51-76-10 AND APPLY PAINT IAW SRM51-23-00.  THIS REPAIR MUST BE INSPECTED IAW SRI 53-13-12-2-001-00 AND SRI 53-13-12-2-002-00.

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