What was found
DURING INSPECTION, FOUND 10" CRACK IN BODY STA. 663 VAPOR WEB FIBERGLASS PANEL BETWEEN RBL 31 & 37, BETWEEN WL 150 AND WL 158. REPAIRED CRACK IN VAPOR WEB PANEL IAW SRM 51-70-04, REPAIR 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND 10" CRACK IN BODY STA. 663 VAPOR WEB FIBERGLASS PANEL BETWEEN RBL 31 & 37, BETWEEN WL 150 AND WL 158. REPAIRED CRACK IN VAPOR WEB PANEL IAW SRM 51-70-04, REPAIR 10.