What was found
FUSELAGE SUSTAINED SKIN DAMAGE FROM LADDER ON RT AFT SIDE OF FUSELAGE, BETWEEN HYDRAULIC SYSTEM #3 ACCUMULATOR SERVICING ACCESS PANEL AND AFT EQUIPMENT BAY (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SUSTAINED SKIN DAMAGE FROM LADDER ON RT AFT SIDE OF FUSELAGE, BETWEEN HYDRAULIC SYSTEM #3 ACCUMULATOR SERVICING ACCESS PANEL AND AFT EQUIPMENT BAY (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS