What was found
DURING HMV, A CRACK WAS FOUND ON FUSELAGE FRAME OVERWING OF THE STA Y=864 AND X=55 AT THE CABIN FLOOR STRUCTURE. FRAME WAS REPLACED IAW DWG SR09530282 REV C.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, A CRACK WAS FOUND ON FUSELAGE FRAME OVERWING OF THE STA Y=864 AND X=55 AT THE CABIN FLOOR STRUCTURE. FRAME WAS REPLACED IAW DWG SR09530282 REV C.