What was found
CRACK IN RADIUS OF FRAME TO SKIN ANGLE, FORWARD OF F/O WINDSHIELD, APPROX FS 83 BY 9.0. STOP DRILLED CRACK, FABRICATED AND INSTALLED TWO ANGLE REPAIR PER SRM 53-03 FIG 34. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN RADIUS OF FRAME TO SKIN ANGLE, FORWARD OF F/O WINDSHIELD, APPROX FS 83 BY 9.0. STOP DRILLED CRACK, FABRICATED AND INSTALLED TWO ANGLE REPAIR PER SRM 53-03 FIG 34. (M)