What was found
FUSELAGE CRACK ON UPPER CROWN AREA. CRACK MEASURES 10.75 INCHES. LOCATED AT STA 426 STRINGER S4L AND ABOVE FIRST PAX WINDOW LT SIDE. ACCOMPLISHED HFEC INSP OF CUT OUT PER NDT, ALSO ACCOMPLISHED EXISTING FASTENER HOLES PER NDT PART 6. NO CRACK INDICATIONS NOTED AT THIS TIME. MFG & INSTALLED STRUCTURAL FILLERS, DOUBLER AND TRIPLER, DRILL, ALODINE AND PRIME PER UA-EVA-80084. ACCOMPLISHED INSP OF REPAIR PARTS AS REQUIRED PER EVA 80084.