JACKSONVILLE, FL, USA
N5BA
BEECH G18S
THE PLT REPORTED THAT DURING THE LANDING ROLL, WHILE ROLLING ON ALL 3 GEAR, THE TAILWHEEL FAILED & STEERED SIDEWAYS CAUSING THE ACFT TO VEER OFF THE RWY. AN INVESTIGATION REVEALED THE TAILWHEEL TRUSS AXLE HAD FAILED. A FURTHER INSPECTION REVEALED THAT 50% OF THE FRACTURE SURFACE WAS RUSTED. ADDITIONALLY, THE ACFT HAD RECEIVED A PHASE 3 INSPECTION UNDER THE COMPANIES PROGRESSIVE MAINTENANCE PROGRAM, 26 FLT HRS PRIOR TO THE ACCIDENT. THIS PHASE INSPECTION CALLED FOR INSPECTION & RETRACT TESTING OF THE LANDING GEAR SYS. COMPANY PERSONNEL STATED THAT INSPECTION OF THE TRUSS AXLE WAS NOT ACCOMPLISHED.
Source: NTSB Aviation Accident Database
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