What was found
DURING POST FLIGHT INSPECTION, AN 8.5 FUSELAGE SKIN PUNCTURE WAS NOTED AT FS 288.00 TO 297.00 AT LONGERON 32R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER I/A/W SRM 53-2-1 FIG 7. SEALED AREA I/A/W SRM 51-1-11.