What was found
THE LT FUSELAGE HAD PUNCTURE HOLE 21 INCHES BELOW CAPTAIN SLIDING WINDOW. REPAIRED PER SRM 53-30-3, FIG 13 SHEET 3. CHECK-C 9-7-99 MCI.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE LT FUSELAGE HAD PUNCTURE HOLE 21 INCHES BELOW CAPTAIN SLIDING WINDOW. REPAIRED PER SRM 53-30-3, FIG 13 SHEET 3. CHECK-C 9-7-99 MCI.