What was found
FUSELAGE SKIN AT LOWER EDGE OF RIGHT COCKPIT WINDOW OPENING IS CORRODED. REMOVED CORROSION AND RESTORED PROTECTIVE TREATMENT. FABRICATED AND INSTALLED STEPPED DOUBLER .032 THICK. AIRCRAFT RETURNED TO SERVICE. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN AT LOWER EDGE OF RIGHT COCKPIT WINDOW OPENING IS CORRODED. REMOVED CORROSION AND RESTORED PROTECTIVE TREATMENT. FABRICATED AND INSTALLED STEPPED DOUBLER .032 THICK. AIRCRAFT RETURNED TO SERVICE. (M)