# SDR GLBA20060995

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 11, 2007
- Submitted: September 19, 2007
- Operation: Air carrier
- Aircraft: [N251GL](https://openairdocs.org/aircraft/N251GL), registered now
- Make and model: Beech 1900D
- Registry model: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (OpenAirDocs)
- Aircraft serial: UE251
- Aircraft time: 23,366 hours, 28,623 cycles
- Engine: Pwa PT6A67D
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Cracked
- Location: Bs 177
- 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/GLBA20060995

## Discrepancy

FUSELAGE FRAME CRACKED AT F.S. 177.3 AT STRINGER 9AR APPROXIMATELY 1.1 INCH IN LENGTH. MAINTENANCE REPAIRED FUSELAGE FRAME CRACK AT STRINGER RELIEF HOLE AT FS 177.3 STRINGER 9R IAW SRM 51-70. REPAIR DIMENSIONS APPROX 5 INCH BY 2.5 INCH, 2024 T-3 .080. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1.

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