What was found
FUSELAGE SKIN DENTED AT FRAME BETWEEN LONG 18 & 19L STA 237. INSTALLED DOULBER REPAIR AT BS 237 BETWEEN LONGERON 18L AND 19L IAW SRM B717 53-00-01 FIG 204. MATERIAL USED 2024-T3 .032 X 4.0 X 4.5 INCHES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DENTED AT FRAME BETWEEN LONG 18 & 19L STA 237. INSTALLED DOULBER REPAIR AT BS 237 BETWEEN LONGERON 18L AND 19L IAW SRM B717 53-00-01 FIG 204. MATERIAL USED 2024-T3 .032 X 4.0 X 4.5 INCHES.