What was found
CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A SMALL CRACK .25 INCH AT RIVET HOLE FUSELAGE FRAME 500A BETWEEN S8L AND S9L. CUT OUT DAMAGE FILL AND DOUBLER PER SRM 53-00-07 FIG 202. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A SMALL CRACK .25 INCH AT RIVET HOLE FUSELAGE FRAME 500A BETWEEN S8L AND S9L. CUT OUT DAMAGE FILL AND DOUBLER PER SRM 53-00-07 FIG 202. (M)