What was found
DURING REMOVAL OF SHEAR CLIP AT FRAME 73 (REFER TO NON-ROUTINE E687963) FOUND ANGLE THAT ATTACHES LT PYLON RIB 5 TO FUSELAGE TO BE CRACKED. C/A-REPLACED ANGLE IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING REMOVAL OF SHEAR CLIP AT FRAME 73 (REFER TO NON-ROUTINE E687963) FOUND ANGLE THAT ATTACHES LT PYLON RIB 5 TO FUSELAGE TO BE CRACKED. C/A-REPLACED ANGLE IAW SRM 51-40-02.