# Incident 20030630012899I: Beech 58, Windsor Locks, CT, June 30, 2003

- Type: FAA incident report (Accident/Incident Data System), as reported
- Date: June 30, 2003, 09:54 local time
- Place: Windsor Locks, CT
- Airport: Bradley International
- Damage: Minor damage
- Phase of flight: Level Off Touchdown
- Operating rules: Air taxi and commuter (Part 135)
- Operator: BSYA
- Location: 41.9390° N, 72.6843° W: Placed by OpenAirDocs at BRADLEY INTL (BDL), within about a mile (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=41.9390&lon=-72.6843&mi=10
- Aircraft: N95BB, a cancelled registration (https://openairdocs.org/deregistered/N95BB-2017-01-05) (OpenAirDocs)
- Registry model: Beech 58 (registry code 1152740, https://openairdocs.org/model/beech-58) (OpenAirDocs)
- Registry engine: Continental IO-520 series (registry code 17032, https://openairdocs.org/engine/continental-io-520-series) (OpenAirDocs)
- Reported make and model: BEECH 58
- Reported engine: CONT IO520C
- People aboard: 1
- Fatal injuries: 0
- Pilot flight hours: 1,840 total, 17 in this make and model, 17 in the last 90 days
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20030630012899I

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

(-23) US CHECK FLIGHT 145 OPERATED BY AIRNET SYSTEMS, LANDED AT BRADLEY (BDL) GEAR UP AT 0954 ON 06-30-03 RUNWAY 15. FLIGHT ORIGINATED OUT OF TETERBORO, N.J. AND WAS ENROUTE TO UTICA, N.Y. ON APPROACH INTO UTICA, PILOT REPORTED NO POSITIVE INDICATION OF LANDING GEAR DOWN AND LOCKED. TOWER AT UTICA REPORTED LANDING GEAR NOT FULLY EXTENDED AFTER LOW PASS. EMERGENCY GEAR EXTENSION PROCEDURES PERFORMED AS PER PILOT'S OPERATING MANUAL BUT NO HELP. PILOT ELECTED TO DIVERT INTO BRADLEY AND REQUESTED RUNWAY FOAM FOR GEAR UP LANDING. AIRCRAFT CIRCLED THE AIRPORT WHILE GROUND CREWS FOAMED RUNWAY 15. AIRCRAFT MISSED FOAMED AREA OF RUNWAY 15 AND LANDED GEAR UP WITH NO INJURIES AND MINOR DAMAGE. INITIAL TROUBLESHOOTING REVEALED FAILED LANDING GEAR ACTUATOR ASSEMBLY. OPERATOR WILL SUBMIT FAA FORM 8010-4 MALFUNCTION OR DEFECT REPORT AFTER CORRECTIONS.

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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