20020602010469A

Accident · No damage

FAA accident report · Cndair CL-600-2B19 · Atlanta, GA · June 2, 2002

Date: June 2, 2002 · 22:42 local
Place: Atlanta, GA
Airport: The William B Hartsfield Atla
Operating rules: Air carrier (Part 121)
Operator: ASOA
Damage: No damage
Aircraft: N849AS
NTSB investigation: NTSBATL02FA113
Reported as: Cndair CL6002B19

N849ASRegistration cancelled Dec 9, 2025 · Bombardier CL-600-2B19S/N 7347 · Built 1999 Airframe modelBombardier CL-600-2B19 Engine modelGE CF34 seriesTurbo-fan

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry 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.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-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.

As the FAA filed it

(-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.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

NTSB ATL02FA113Accident · No injuriesField investigationFinal reportAtlanta, GAFailure 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 reasons.Jun 3, 2002 · Substantial damage