What was found
LOWER FUSELAGE HAS CRACK IN SKIN AT STA 100 AT LONGERON 35 & 36R. CRACK IS PROBABLY INDUCED BY CORROSION. COMPLIED WITH STEPS 1-11 OF EVA D853-00412. FABRICATED FILLER, DOUBLER AND INSTALLED REPAIR. MAJOR REPAIR
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE HAS CRACK IN SKIN AT STA 100 AT LONGERON 35 & 36R. CRACK IS PROBABLY INDUCED BY CORROSION. COMPLIED WITH STEPS 1-11 OF EVA D853-00412. FABRICATED FILLER, DOUBLER AND INSTALLED REPAIR. MAJOR REPAIR