What was found
IN TPA FOR B-2 LTR CK, .375 INCH CRACK IN COCKPIT OUTER SKIN AT LOWER FWD I/B CORNER OF L-4 WINDOW FROM BOLT HOLE TO EDGE OF WINDOW CUTOUT. REPAIRED PER SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
IN TPA FOR B-2 LTR CK, .375 INCH CRACK IN COCKPIT OUTER SKIN AT LOWER FWD I/B CORNER OF L-4 WINDOW FROM BOLT HOLE TO EDGE OF WINDOW CUTOUT. REPAIRED PER SRM 53-30-3.