What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
The student pilot was rptdly on her 4th solo flt practicing touch and go landings on rwy 11 when the acft landed hard on the lt main ldg gear. The acft taxied back to the ramp without further incident after the ldg.
The student plt rptd that she had encountered a 'gust of wind' during the ldg flare that tilted the acft to the right. The acft then touched down on the lt main gear as she was attempting to correct for that.
The flight school chief plt reptd coi wind conditions at the time as calm. The nearest wx station about 8 miles se of coi was patrick afb (cof). The 1156Z kcof METAR also reptd the winds as calm.
Initial inspection of the acft revealed that the upper torque link assy attach point on the lt MLG strut had fractured and separated. Further inspection of the acft after lt wing removal revealed that the lt wing upper main spar had sustained damage where it attaches to the fuselage carry-through spar at the wing root. One of the fuselage attachment bolts was also found to be bent.
As the FAA filed it
THE STUDENT PILOT WAS RPTDLY ON HER 4TH SOLO FLT PRACTICING TOUCH AND GO LANDINGS ON RWY 11 WHEN THE ACFT LANDED HARD ON THE LT MAIN LDG GEAR. THE ACFT TAXIED BACK TO THE RAMP WITHOUT FURTHER INCIDENT AFTER THE LDG.
THE STUDENT PLT RPTD THAT SHE HAD ENCOUNTERED A 'GUST OF WIND' DURING THE LDG FLARE THAT TILTED THE ACFT TO THE RIGHT. THE ACFT THEN TOUCHED DOWN ON THE LT MAIN GEAR AS SHE WAS ATTEMPTING TO CORRECT FOR THAT.
THE FLIGHT SCHOOL CHIEF PLT REPTD COI WIND CONDITIONS AT THE TIME AS CALM. THE NEAREST WX STATION ABOUT 8 MILES SE OF COI WAS PATRICK AFB (COF). THE 1156Z KCOF METAR ALSO REPTD THE WINDS AS CALM.
INITIAL INSPECTION OF THE ACFT REVEALED THAT THE UPPER TORQUE LINK ASSY ATTACH POINT ON THE LT MLG STRUT HAD FRACTURED AND SEPARATED. FURTHER INSPECTION OF THE ACFT AFTER LT WING REMOVAL REVEALED THAT THE LT WING UPPER MAIN SPAR HAD SUSTAINED DAMAGE WHERE IT ATTACHES TO THE FUSELAGE CARRY-THROUGH SPAR AT THE WING ROOT. ONE OF THE FUSELAGE ATTACHMENT BOLTS WAS ALSO FOUND TO BE BENT.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.