# SDR CGO2003F00007

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 7, 2003
- Submitted: May 6, 2003
- Operation: Air carrier
- Aircraft: N8283S
- Make and model: Beech 2000
- Registry model: [Beech 2000](https://openairdocs.org/model/beech-2000) (OpenAirDocs)
- Aircraft serial: NC41
- Engine: Pwa PT6*
- System (JASC): [5414 · Nacelle/Pylon, Plate/Skin](https://openairdocs.org/jasc/5414)
- Part: Panel
- Part number: 1229100713
- Condition: Cracked
- Location: Lt Nacelle
- Part time: 2,470 hours
- Stage of operation: NR
- How discovered: 9
- Nature of condition: O
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CGO2003F00007

## Discrepancy

FOUND CRACK/ DELAMINATED AREA IN PRODUCTION LAP JOINT BETWEEN MOLDED HALVES OF CLOSEOUT PANEL AT APPROX 6 OCLOCK POSITION BELOW SPINNER CUT-OUT AND ABOVE OIL COOLER EXIT DUCT.  AREA USUALLY DIRTY/GREASY, HAVE TO CLEAN THOROUGHLY AND FLEX PARTS TO INSPECT ADEQUATELY.  SUSPECT CAUSAL FACTOR NORMAL AIRFRAME/PROPELLER VIBRATION LEVELS AND/OR HEAT THIS LOCATION.  FIELD REPAIR FR-SS-00044 AND RETURNED TO SERVICE.  SUGGEST CLOSE INSPECTION OF THIS AREA DURING SCHEDULED INSPECTIONS ONCE AIRCRAFT APPROACHES 2000 HOUR TTAF.

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