What was found
DURING ROUTINE C-CHECK INSPECTION FOUND MAIN CABIN SKIN CRACKED AT BS 1096 STRINGER 1. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AT BS 1096 STR 1, ALODINED AND PRIMED, IAW SRM 53-30-3 FIG 4, 51-10-2, 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C-CHECK INSPECTION FOUND MAIN CABIN SKIN CRACKED AT BS 1096 STRINGER 1. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AT BS 1096 STR 1, ALODINED AND PRIMED, IAW SRM 53-30-3 FIG 4, 51-10-2, 51-30-2.