What was found
Fuselage Skin damaged from BS 460 to 480 from between Stringer 38R and 39R by cargo container during loading operation. Stringers 38R and 39R at this location deformed by container. Damaged skin area trimmed out. Damaged area of stringer 38R trimmed out. Stringer 39R was straightened. Area NDT inspected after straightening. No cracks found. Repair doublers, fillers and stringer repair sections fabricated and installed per standard practices. Briles fasteners used in fuselage skin repair IAW SRM 53-00-03 Figure 204