What was found
FUSELAGE SKIN DAMAGED LOCATION IS THE RIGHT ALT STATIC PORT. INSTALLED PERMANENT FLUSH REPAIR DOUBLER AT RIGHT STATIC PORT PER SRM 53-04 12C AND EA MD80-53-011714.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DAMAGED LOCATION IS THE RIGHT ALT STATIC PORT. INSTALLED PERMANENT FLUSH REPAIR DOUBLER AT RIGHT STATIC PORT PER SRM 53-04 12C AND EA MD80-53-011714.