What was found
CRACK IN SKIN AT CANTED FRAME STA 1303 JUST ABOVE STRINGER 14 LT SIDE. CRACK IS APPROXIMATELY 2.6 INCHES IN LENGTH. REPAIRED CRACK IN SKIN PER DC-9 SRM 53-01 FIG 4 SHEET 4 AND DC-9 TRM 53-30-01-801-663A-A. JOB COMPLETE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN SKIN AT CANTED FRAME STA 1303 JUST ABOVE STRINGER 14 LT SIDE. CRACK IS APPROXIMATELY 2.6 INCHES IN LENGTH. REPAIRED CRACK IN SKIN PER DC-9 SRM 53-01 FIG 4 SHEET 4 AND DC-9 TRM 53-30-01-801-663A-A. JOB COMPLETE.