What was found
DURING D-CK, FOUND CRACK IN STIFFENER, AFT SIDE OF AFT PRESSURE BULKHEAD AT FOUR O'CLOCK POSITION JUST OUTBD OF DOOR JAMB APPROX .25 INCH IN LENGTH. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 53-01, SHEET 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CK, FOUND CRACK IN STIFFENER, AFT SIDE OF AFT PRESSURE BULKHEAD AT FOUR O'CLOCK POSITION JUST OUTBD OF DOOR JAMB APPROX .25 INCH IN LENGTH. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 53-01, SHEET 4.