What was found
WHEN MECHANIC WAS COMPLYING WITH ASB 407-11-95, FOUND CRACK ON UPPER LT LONGERON AT FUSELAGE STA 192.0, BL 0.0 TO RBL 4.3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHEN MECHANIC WAS COMPLYING WITH ASB 407-11-95, FOUND CRACK ON UPPER LT LONGERON AT FUSELAGE STA 192.0, BL 0.0 TO RBL 4.3.