What was found
DENT ON FUSELAGE LEFT SIDE BETWEEN PRESSURE RELIF VALVE AND ELEV.STATIC PORT ABOUT 36" BELOW PUNCTURE THROUGH FUSELAGE SKIN AT APPROX STA 1445 AND 1" ABOVE S-25L REMOVED DAMAGE TO THE AFFECTED SKIN AERA STA 1445 AND STR 25 L REF 53-00-01. INSPECTION WILL NEED TO VERIFY SKIN THICKNESS AFTER REMOVAL OF DAMAGE. CRACKS.. SKIN THICKNESS AT REMOVAL AREA IS 0.43" DAMAGE TO SKIN (APPROX. 3" X 3") . NO INDICATION OF SKIN PERFORMED HEFC AND SKIN THICKNESS INSPECTION AFTER REMOVAL OF CUT OUT DAMAGED AERA REF SRM 53-00-01 REPAIR 29 PARA 4 A-D. PERFORMED HFEC OF DAMAGE CUTOUT. NO CRACKS DETECTED. REF. NDT PART 6 51-00-16 COMPLIED WITH SRM 53-00-01 REPAIR 29, PAR4 E-G. VERIFIED STEPS (4) E THRU G (NDT) HFEC AND HOLE PROBE INSP. REF. REPAIR 29 SRM 53-00-01 AND NDT PART 6 51-00-16 0.063" 2024-T3 P.O.# 8546450 AND THE -3 REPAIR FILLE