What was found
ENGINE 2 FAN BLADE LE HAS BETWEEN 3" - 4" DEFORMATION BELOW MID SPAN SHROUD. R & R ENG 2 FAN BLADE, NR 16 OLD MOMENT, .174 NEW MOMENT, .174 IAW 72-31-02-804-076-1400. VIBRATION SURVEY TUBE DONE ON TASK CARD A72-999-01-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ENGINE 2 FAN BLADE LE HAS BETWEEN 3" - 4" DEFORMATION BELOW MID SPAN SHROUD. R & R ENG 2 FAN BLADE, NR 16 OLD MOMENT, .174 NEW MOMENT, .174 IAW 72-31-02-804-076-1400. VIBRATION SURVEY TUBE DONE ON TASK CARD A72-999-01-02.