What was found
DURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS 2 INCHES. CRACK LOCATED INSIDE ACCESS PANEL 311UR, AT NR 2 ENGINE INTAKE. REPAIRED PER SRM 54-12-00 PG 808.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS 2 INCHES. CRACK LOCATED INSIDE ACCESS PANEL 311UR, AT NR 2 ENGINE INTAKE. REPAIRED PER SRM 54-12-00 PG 808.