What was found
DURING C CHECK, ONE FASTENER HOLE HAD CRACKS COMMON TO RHS STA 800 FRAME INNER CHORD ANGLE AND STRAP AT STA 16R. DAMAGE TRIMMED OUT AND INSTALLED REPAIR STRAPS AND FILLERS PER SRM 51-10-02, BOEING SR1D1-181882088, SRM 53-10-04, ECRA 477-51-111-1.