What was found
CORRODED CRACK ON RT FUSELAGE AT STA. 1085-1088 BETWEEN S-12 AND S-13.INSTALLED FUSELAGE SKIN REPAIR BETWEEN BS 1080-1100 AND STRINGERS 12R-14R. REPAIR SKETCH 1-211756245. DOA-300064-NM FORM 8100-9 DATED 22 JULY 2006.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORRODED CRACK ON RT FUSELAGE AT STA. 1085-1088 BETWEEN S-12 AND S-13.INSTALLED FUSELAGE SKIN REPAIR BETWEEN BS 1080-1100 AND STRINGERS 12R-14R. REPAIR SKETCH 1-211756245. DOA-300064-NM FORM 8100-9 DATED 22 JULY 2006.