# SDR GLBA20060957

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 20, 2007
- Submitted: June 21, 2007
- Operation: Air carrier
- Aircraft: [N253GL](https://openairdocs.org/aircraft/N253GL), registered now
- Make and model: Beech 1900D
- Registry model: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (OpenAirDocs)
- Aircraft serial: UE253
- Aircraft time: 22,515 hours, 28,303 cycles
- Engine: Pwa PT6A67D
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Blade
- Condition: Damaged
- Location: Propeller
- Stage of operation: LD
- How discovered: O
- Nature of condition: O
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/GLBA20060957

## Discrepancy

EXTENDED ROLLOUT, UPON LANDING, PILOTS REPORTED THAT DUE TO LANDING ROLLOUT BEYOND THE END OF THE RUNWAY, THE RT PROP  NR 2 ENGINE STRUCK A RECTANGULAR BOX.  PRELIMINARY DAMAGE INDICATES PROP BLADE DAMAGE AND HOLE IN FUSELAGE.  [08-01-07]  MX INSTALLED TEMP REPAIR IN RT FUSELAGE IAW SRM REF 51-70.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
