As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
"3 EACH DENTS LOCATED BETWEEN FRAMES 23 TO 24 AND FRAMES 24 TO 25 LH SIDE OF FUSELAGE. RAF-01 3069145-02 HAS BEEN GENERATED.-PERFORMED REPAIR INSTRUCTION ON DENT EXTERNAL SKIN LOC ON FR 23 PLUS 19 INCH AND BTW STRG 24-25 LH UPPER FUSELAGE IAW EA # 53-0722-23 REV 0 AND PART 1. MEASURE OF DENTS ARE X=1.3 IN Y= 1.15 IN A= 0.051 IN D= 0.034 IN AND NT = 0.047 IN THIS REPAIR IS CATEGORY A"