What was found
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 996 FRAME ANGLE AT THE T-CAP BETWEEN LONGERONS 26R TO 27R. REPAIRED PER EA 99-102943.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 996 FRAME ANGLE AT THE T-CAP BETWEEN LONGERONS 26R TO 27R. REPAIRED PER EA 99-102943.