What was found
WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FUSELAGE FRAME SHEAR TIE IS CRACKED NEAR THE RADIUS UPPER END BETWEEN S20R AND S21R, BS 294.5. REMOVED DAMAGED AREA PER SRM 51-40-3. FABRICATED ANGLE AND REPAIRED PER SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FUSELAGE FRAME SHEAR TIE IS CRACKED NEAR THE RADIUS UPPER END BETWEEN S20R AND S21R, BS 294.5. REMOVED DAMAGED AREA PER SRM 51-40-3. FABRICATED ANGLE AND REPAIRED PER SRM 51-30-2.