What was found
INSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN AT STA 1900 TO 1921 BETWEEN STRINGERS 7L AND 8L. THE SKIN WAS REPAIRED IAW SRM 53-20-00, FIGURE 6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN AT STA 1900 TO 1921 BETWEEN STRINGERS 7L AND 8L. THE SKIN WAS REPAIRED IAW SRM 53-20-00, FIGURE 6.