What was found
CABIN FLOOR PANEL C-4 HAS FIBERGLASS SPLITTING WHERE RIVETS ATTACH EXPANSION JOINT. REPAIRED DAMAGED AREA''S IAW SRM 51-70-1 PARAGRAPH 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CABIN FLOOR PANEL C-4 HAS FIBERGLASS SPLITTING WHERE RIVETS ATTACH EXPANSION JOINT. REPAIRED DAMAGED AREA''S IAW SRM 51-70-1 PARAGRAPH 7.