What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On 6/29/2003, at approx 15:30 hours CDT, a Schweizer model G-164B agcat, N7501H, s/n 801B sheared off the left main gear while attempting to land on runway 35 at Oldham County Airport (E52). The pilot applied both brakes to slow the airplane. The brake pedal on the left side felt soft and only the right pedal felt firm. Airplane veered to the right and at that point the pilot again attempted braking with the left pedal. The left pedal felt firm on the second application but pilot stated it was too late to correct to the left at that point. The airplane went into the ditch located along right side of runway, at that point the left main gear sheared off at the fuselage attach point. The left brake tubing sheared off at the fuselage, aircraft nosed over, propeller struck the ground, damaging one blade. The lower left wing sustained damage to the wing tip leading and trailing edges. Minor damage to the upper wing leading edge at the wing tip. Left aft cabane strut bent at the fuselage attach point. Engine mount tubing cracked and bent. Firewall bent on right side.
As the FAA filed it
(-23) ON 6/29/2003, AT APPROX 15:30 HOURS CDT, A SCHWEIZER MODEL G-164B AGCAT, N7501H, S/N 801B SHEARED OFF THE LEFT MAIN GEAR WHILE ATTEMPTING TO LAND ON RUNWAY 35 AT OLDHAM COUNTY AIRPORT (E52). THE PILOT APPLIED BOTH BRAKES TO SLOW THE AIRPLANE. THE BRAKE PEDAL ON THE LEFT SIDE FELT SOFT AND ONLY THE RIGHT PEDAL FELT FIRM. AIRPLANE VEERED TO THE RIGHT AND AT THAT POINT THE PILOT AGAIN ATTEMPTED BRAKING WITH THE LEFT PEDAL. THE LEFT PEDAL FELT FIRM ON THE SECOND APPLICATION BUT PILOT STATED IT WAS TOO LATE TO CORRECT TO THE LEFT AT THAT POINT. THE AIRPLANE WENT INTO THE DITCH LOCATED ALONG RIGHT SIDE OF RUNWAY, AT THAT POINT THE LEFT MAIN GEAR SHEARED OFF AT THE FUSELAGE ATTACH POINT. THE LEFT BRAKE TUBING SHEARED OFF AT THE FUSELAGE, AIRCRAFT NOSED OVER, PROPELLER STRUCK THE GROUND, DAMAGING ONE BLADE. THE LOWER LEFT WING SUSTAINED DAMAGE TO THE WING TIP LEADING AND TRAILING EDGES. MINOR DAMAGE TO THE UPPER WING LEADING EDGE AT THE WING TIP. LEFT AFT CABANE STRUT BENT AT THE FUSELAGE ATTACH POINT. ENGINE MOUNT TUBING CRACKED AND BENT. FIREWALL BENT ON RIGHT SIDE.
Other reports on N7501H · 1
Matched to the same aircraft by N-number and date.