What was found
INSPECTION FOUND A 1/8" CRACK IN STRINGER 16L AND 16R AT FASTENER AREA FWD OF LIGHT ASSEMBLY STA 500C AFT. A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-00-03, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1/8" CRACK IN STRINGER 16L AND 16R AT FASTENER AREA FWD OF LIGHT ASSEMBLY STA 500C AFT. A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-00-03, FIGURE 201.