What was found
STIFFENER IN BETWEEN FLOORBEAMS AT BS 538, B10 TO LBL 25, WL 208 IS CRACKED ON THE INBOARD FORWARD SIDE. REMOVED CRACKED SUPPORT REPLACED WITH NEW SUPPORT IAW SRM 51-40-02. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STIFFENER IN BETWEEN FLOORBEAMS AT BS 538, B10 TO LBL 25, WL 208 IS CRACKED ON THE INBOARD FORWARD SIDE. REMOVED CRACKED SUPPORT REPLACED WITH NEW SUPPORT IAW SRM 51-40-02. (M)