What was found
CLT - DURING A Q-3 CHECK VISUAL INSPECTION FOUND A SMALL CRACK .250 INCH AT RIVET HOLE FUSELAGE FRAME 380 BETWEEN S8L AND S9L. CUT OUT DAMAGED AREA AND REPAIRED WITH FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING A Q-3 CHECK VISUAL INSPECTION FOUND A SMALL CRACK .250 INCH AT RIVET HOLE FUSELAGE FRAME 380 BETWEEN S8L AND S9L. CUT OUT DAMAGED AREA AND REPAIRED WITH FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (X)