# Accident 20020602010469A: Cndair CL6002B19, Atlanta, GA, June 2, 2002

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: June 2, 2002, 22:42 local time
- Place: Atlanta, GA
- Airport: The William B Hartsfield Atla
- Damage: No damage
- Operating rules: Air carrier (Part 121)
- Operator: ASOA
- Location: 33.6453° N, 84.4331° W: From the FAA
- Nearby events: https://openairdocs.org/map.md?lat=33.6453&lon=-84.4331&mi=10
- Aircraft: N849AS, a cancelled registration (https://openairdocs.org/deregistered/N849AS-2025-12-09) (OpenAirDocs)
- Registry model: Bombardier CL-600-2B19 (registry code 1390008, https://openairdocs.org/model/bombardier-cl-600-2b19) (OpenAirDocs)
- Registry engine: GE CF34 series (registry code 30015, https://openairdocs.org/engine/ge-cf34-series) (OpenAirDocs)
- Reported make and model: CNDAIR CL6002B19
- NTSB investigation: [NTSB ATL02FA113](https://openairdocs.org/ntsb/ATL02FA113) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20020602010469A

## Narrative

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

(-23) DURING LANDING ROLL-OUT THE LH M/L/G FITTING SHEARED OFF. AT THIS TIME THE CAUSE IS UNKNOWN. THE AIRCRAFT WAS CARRYING 50 PASSENGERS AND BAGS. EVERYONE WAS SAFELY EVACUATED THRU EITHER THE PASSENGER ENTRY DOOR OR THE RH OVERWING EXIT. THE LH M/L/G HAS BEEN REMOVED FROM THE AIRCRAFT FOR TRANSPORT TO THE NTSB METALLURGIST.

## The NTSB's investigation of this event (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ATL02FA113](https://openairdocs.org/ntsb/ATL02FA113), Jun 3, 2002: Bombardier CL600-2B19 (N849AS), Atlanta, GA, substantial damage. Probable cause: Failure of the left main landing gear fitting due to a fatigue crack that emanated from multiple origins at the external surface of the wall at the shock strut radius run out area for undetermined…

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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