What was found
FUSELAGE SKIN DENTED AT FRAME STA 218 BETWEEN LONGERON 17L AND 18L. INSTALLED REPAIR AT FUSELAGE SKIN AT FRAME STA 218 BETWEEN 17L AND 18L IAW SRM B717 53-00-01 FIG 201. MATERIAL USED 2024.T3 .050 14 X 15.5 INCHES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DENTED AT FRAME STA 218 BETWEEN LONGERON 17L AND 18L. INSTALLED REPAIR AT FUSELAGE SKIN AT FRAME STA 218 BETWEEN 17L AND 18L IAW SRM B717 53-00-01 FIG 201. MATERIAL USED 2024.T3 .050 14 X 15.5 INCHES.