What was found
DURING PRE-FLIGHT INSP PERFORMED; CREW REPORTED DAMAGE TO THE FUSELAGE SKIN AT BS 2420 - BS 2440 - BETWEEN STR-25L & AMP; STR-25L CONSISTING IN DENTS/WRINKLING (REF FIGURE 1) DIMENSIONS: L:10.0 IN, W:8.0 IN, D:0.140/ L:12.0 IN. W:7.5 IN. D:0.140 THE DAMAGE IS OUT OF THE SRM 53-00-01, FIG 101 ALLOWABLE DAMAGE 1, DETAIL III.