What was found
DURING HEAVY CHECK, WAS REPORTED THAT INTERNAL DOUBLER OF FUSELAGE PANEL 192CR IS CORRODED. MAINTENANCE R & R INTERNAL DOUBLER OF FUSELAGE PANEL 192CR IAW SRM 51-41-02, 51-23-05. PN 170-13414-004 SPACER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY CHECK, WAS REPORTED THAT INTERNAL DOUBLER OF FUSELAGE PANEL 192CR IS CORRODED. MAINTENANCE R & R INTERNAL DOUBLER OF FUSELAGE PANEL 192CR IAW SRM 51-41-02, 51-23-05. PN 170-13414-004 SPACER.