What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On final landing after several touch and go landings, student pilot and CFI thought that they blew the left tire because the right wing came up. After full stop it was noted that the upper torque link attach lugs of the right main landing gear cylinder had both broken off disconnecting the torque link assembly allowing the strut to fully open and misaligned the wheel. Other than the cylinder assembly, no other damage was incurred. The left main landing gear cylinder was dye penetrated and both attach lugs had cracks present. Visually looking at where the break occurred, it was apparent that the cracks had been there for some time and that inner-grannular corrosion had occurred. Both cylinders will be replaced. Piper service bulletin no. 1131 dated August 2003, addressing this problem, was not complied with.
As the FAA filed it
(-23) ON FINAL LANDING AFTER SEVERAL TOUCH AND GO LANDINGS, STUDENT PILOT AND CFI THOUGHT THAT THEY BLEW THE LEFT TIRE BECAUSE THE RIGHT WING CAME UP. AFTER FULL STOP IT WAS NOTED THAT THE UPPER TORQUE LINK ATTACH LUGS OF THE RIGHT MAIN LANDING GEAR CYLINDER HAD BOTH BROKEN OFF DISCONNECTING THE TORQUE LINK ASSEMBLY ALLOWING THE STRUT TO FULLY OPEN AND MISALIGNED THE WHEEL. OTHER THAN THE CYLINDER ASSEMBLY, NO OTHER DAMAGE WAS INCURRED. THE LEFT MAIN LANDING GEAR CYLINDER WAS DYE PENETRATED AND BOTH ATTACH LUGS HAD CRACKS PRESENT. VISUALLY LOOKING AT WHERE THE BREAK OCCURRED, IT WAS APPARENT THAT THE CRACKS HAD BEEN THERE FOR SOME TIME AND THAT INNER-GRANNULAR CORROSION HAD OCCURRED. BOTH CYLINDERS WILL BE REPLACED. PIPER SERVICE BULLETIN NO. 1131 DATED AUGUST 2003, ADDRESSING THIS PROBLEM, WAS NOT COMPLIED WITH.