What was found
(CAN) ENGINE VIBRATION AND POWER LOSS WHILE GLIDER IN TOW. CRACK AROUND NR 2 CYLINDER. CYLINDER HAD BEEN OVERHAULED SUBJECT TO FREEDOM FREE PROCESS AND CERMICROME PLATING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) ENGINE VIBRATION AND POWER LOSS WHILE GLIDER IN TOW. CRACK AROUND NR 2 CYLINDER. CYLINDER HAD BEEN OVERHAULED SUBJECT TO FREEDOM FREE PROCESS AND CERMICROME PLATING.