What was found
LOWER EXTERNAL FUSELAGE AT STA 536.25 BETWEEN LONGERONS 24L AND 25L SKIN WITH DENT. DAMAGED SKIN WAS REPAIRED PER MD-80 DWG SG0953002 VIEW C1 SHEET 1 AND 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER EXTERNAL FUSELAGE AT STA 536.25 BETWEEN LONGERONS 24L AND 25L SKIN WITH DENT. DAMAGED SKIN WAS REPAIRED PER MD-80 DWG SG0953002 VIEW C1 SHEET 1 AND 4.