# SDR CA040211005

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 23, 2004
- Submitted: April 1, 2004
- Operation: General aviation
- Make and model: Beech C90A
- Registry model: [Beech C90A](https://openairdocs.org/model/beech-c90a) (OpenAirDocs)
- Aircraft time: 5,966 hours
- Engine: Pwa PT6A21
- Propeller: Hartzl HCB3TN3
- System (JASC): [5610 · Flight Compartment Windows](https://openairdocs.org/jasc/5610)
- Part: Windshield
- Part number: 101384025
- Condition: Failed
- Location: Cockpit
- Stage of operation: CR
- How discovered: O
- Nature of condition: O
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA040211005

## Discrepancy

(CAN) DEFECT REPORTED AS,  RT OUTER WINDSHIELD SHATTERED IN FLIGHT.  AIRCRAFT WAS ENROUTE AT FL250 WHEN THE WINDSHIELD SHATTERED WITH NO PRIOR INDICATIONS AND NO WINDSHIELD HEAT SELECTED, OAT WAS  41C.  THE AIRCRAFT DIVERTED TO HOME BASE.  UPON INSPECTION IT WAS DISCOVERED THAT THE INNER PANE HAD SHATTERED AND WINDSHIELD REPLACED WITH SUPERCEDED P/N 101-384025-24 IAW THE STRESS FREE INSTALLATION KIT INSTRUCTIONS. SCREWS TORQUED FOLLOWING SEALANT CURE TIME.

---
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.