What was found
PUNCTURE IN FUSELAGE SKIN CAUSED BY GROUND EQUIPMENT 3.5 IN BY 3 IN AT STA 218, STR 21. CLASS 3 REPAIR INSTALLED. REMOVED CLASS 3 REPAIR AND INSTALLED CLASS 2 REPAIR PER DRM 53-04, FIG 12. CHECK-C 10-2-99 STL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PUNCTURE IN FUSELAGE SKIN CAUSED BY GROUND EQUIPMENT 3.5 IN BY 3 IN AT STA 218, STR 21. CLASS 3 REPAIR INSTALLED. REMOVED CLASS 3 REPAIR AND INSTALLED CLASS 2 REPAIR PER DRM 53-04, FIG 12. CHECK-C 10-2-99 STL.