What was found
DURING INSPECTION CHECK, FOUND A CRACK (1.5 INCHES) ON TOP PANEL PLATING OUTBOARD OF STA XCW 69.5 AND STRINGER 1 RT. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-039 AND SRM 57-2-1 FIG 18A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION CHECK, FOUND A CRACK (1.5 INCHES) ON TOP PANEL PLATING OUTBOARD OF STA XCW 69.5 AND STRINGER 1 RT. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-039 AND SRM 57-2-1 FIG 18A.