What was found
AFT FUSELAGE HAD 7 EXTERNAL SKIN CRACKS FROM CANTED STA 1197 TO 1208, LONGERON 13 LEFT TO LONGERON 14 LEFT. CRACK LENGTHS FROM .5 TO .75 INCHES. REPAIRED AREA IAW DC-9 SRM 53-01 AND 53-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE HAD 7 EXTERNAL SKIN CRACKS FROM CANTED STA 1197 TO 1208, LONGERON 13 LEFT TO LONGERON 14 LEFT. CRACK LENGTHS FROM .5 TO .75 INCHES. REPAIRED AREA IAW DC-9 SRM 53-01 AND 53-10.