What was found
HOLE IN FUSELAGE FWD OF MID LAV SERVICE PANEL. HOLE IS LOCATED 2 INCHES ABOVE STRINGER 226 AT APPROX STA 691. HOLE MEASURES .75 INCH IN DIAMETER. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HOLE IN FUSELAGE FWD OF MID LAV SERVICE PANEL. HOLE IS LOCATED 2 INCHES ABOVE STRINGER 226 AT APPROX STA 691. HOLE MEASURES .75 INCH IN DIAMETER. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER.