What was found
SY6 C11 CHECK, LEVEL 2 GALVANIC CORROSION IN TWO AREAS AT R4 DOOR SILL AT FRAME 68-4 INCHES, STRINGER 23R, -Y1732. REPAIRED R4 DOOR SILL AT FRAME 68-4 INCHES, STRINGER 23R, -Y1732 IAW SRM 53-41-14, FIG 201, REPAIR PRINCIPLE 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SY6 C11 CHECK, LEVEL 2 GALVANIC CORROSION IN TWO AREAS AT R4 DOOR SILL AT FRAME 68-4 INCHES, STRINGER 23R, -Y1732. REPAIRED R4 DOOR SILL AT FRAME 68-4 INCHES, STRINGER 23R, -Y1732 IAW SRM 53-41-14, FIG 201, REPAIR PRINCIPLE 5.