# SDR CA001228020

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 8, 2000
- Submitted: January 2, 2001
- Operation: General aviation
- Make and model: Dhav DHC8101
- Engine: Pwa PW121
- System (JASC): [5313 · Fuselage Main, Longeron/Stringer](https://openairdocs.org/jasc/5313)
- Part: Doubler
- Part number: 85530184
- Condition: Cracked
- Location: Doubler
- Part time: 21,903 hours, 24,118 cycles
- Component: Fuselage Main L, Dhav, DHC8100
- 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/CA001228020

## Discrepancy

(CAN) DURING FLEET INSPECTION, REAR FUSELAGE STRUCTURE WAS FOUND CRACKED AT FRAME NR 4, STRINGER NR 4, PORT SIDE, CRACK WAS REPAIRED USING DEHAVILLAND REPAIR DWG (RD8-55-199).

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