What was found
LEFT NACELLE FRAME 1 CRACKED OUTBOARD OF TORQUE MOUNT. ENGINE VIBRATION/TORSION. SB 120-54-0036 IS BEING INCORPORATED. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT NACELLE FRAME 1 CRACKED OUTBOARD OF TORQUE MOUNT. ENGINE VIBRATION/TORSION. SB 120-54-0036 IS BEING INCORPORATED. (X)