# SDR C2X2008F00013

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 18, 2008
- Submitted: August 6, 2008
- Operation: Air carrier
- Aircraft: N17560
- Make and model: Emb EMB-145LR
- Registry model: [EMB EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (OpenAirDocs)
- Aircraft serial: 145605
- Engine: Rroyce AE3007A1
- Engine time: 13,739 hours
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Corroded
- Location: Fuselage
- Stage of operation: IN
- How discovered: D
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/C2X2008F00013

## Discrepancy

ACFT 560 WAS IN FOR A 3C INSPECTION AND CORROSION WAS FOUND ON THE FRONT FRAME FORWARD FLANGE THAT HAD HOLES 9,24,24 AND 40 THAT WERE GREATER THAN THE R/R MANUAL LIMITS.  EC 7220-01056 AND TVF5284 WAS ISSUED APPROVING THE REPAIR OF THE DAMAGE AND CONTINUED OPERATION OF THE ENG.  MX REMOVED THE CORROSION TO A MINIMUM.  CREATED A SMOOTH TRANSITION RADIUS FROM THE AFFECTED AREAS.  INSPECT THE AREA WITH SPORT FLUORESCENT PENETRANT INSPECTION METHOD C SENSITIVITY LEVEL 3 IAW ROLLS ROYCE MANUAL.  ALL WORK WAS ACCOMPLISHED IAW WITH EC7220-01057 AND TVF 5284 AND WILL BE RELEASED AT THE END OF THE C-CHECK.  (S)

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