What was found
DURING "M" CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 1480 HOLE NR 11. REPAIRED PER EA 63-211896 SECT I. REPETITIVE INSPECTIONS TO BE ACCOMPLISHED EVERY 5,500 CYCLES THEREAFTER PER SECT II OF EA 63-211896.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING "M" CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 1480 HOLE NR 11. REPAIRED PER EA 63-211896 SECT I. REPETITIVE INSPECTIONS TO BE ACCOMPLISHED EVERY 5,500 CYCLES THEREAFTER PER SECT II OF EA 63-211896.