What was found
PHX - DURING SCHEDULED D-CHECK, THE FUSELAGE LOWER LOBE AREA ON THE 986.5 FRAME WEB BETWEEN STRINGER 18L AND 21L WAS FOUND TO BE CORRODED. REPAIRED PER SRM 51-10-1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PHX - DURING SCHEDULED D-CHECK, THE FUSELAGE LOWER LOBE AREA ON THE 986.5 FRAME WEB BETWEEN STRINGER 18L AND 21L WAS FOUND TO BE CORRODED. REPAIRED PER SRM 51-10-1. (M)