# SDR UPS00433278

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 14, 2000
- Submitted: July 12, 2000
- Operation: Air carrier
- Aircraft: N521UP
- Make and model: Boeing 747 212B
- Registry model: [Boeing 747 212B](https://openairdocs.org/model/boeing-747-212b) (OpenAirDocs)
- Aircraft serial: 21944
- Aircraft time: 62,800 hours, 15,449 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Cracked
- Location: Fuselage
- 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/UPS00433278

## Discrepancy

INSPECTION TYPE:C, CONTROL CABIN FUSELAGE FRAME WEB IS CRACKED AT INNER FLANGE AT BS 360 STR 2A RT.  REPAIR CARRIED OUT IAW Q/NOTE 17 /2000 AND SRM 53-10-04 FIG 18.  STOP DRILLED CRACKS AND FABRICATED NEW REPAIR DOUBLERS ON NDT INSP CLEARANCE FITTED DOUBLERS.  APPROVED 8110 ISSUED FOR REPAIR.

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