What was found
INSPECTION FOUND A 1/2" CRACK IN STRINGER 16L BETWEEN STA 500C AND 500D. REPAIRED IAW SRM 53-00-03, FIGURE 201, SHEET 6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1/2" CRACK IN STRINGER 16L BETWEEN STA 500C AND 500D. REPAIRED IAW SRM 53-00-03, FIGURE 201, SHEET 6.