What was found
FUSELAGE SKIN AT BS 1554 BETWEEN STRINGERS 24L & 25L AT VACUUM OUTFLOW NOZZLE THE SKIN IS CORRODED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN AT BS 1554 BETWEEN STRINGERS 24L & 25L AT VACUUM OUTFLOW NOZZLE THE SKIN IS CORRODED.