What was found
STRESS PANEL NR 688JT FOUND DELAMINATED. HOT BOND REPAIRED AS PER SRM 51-40-06 FIGURE 17A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRESS PANEL NR 688JT FOUND DELAMINATED. HOT BOND REPAIRED AS PER SRM 51-40-06 FIGURE 17A.