What was found
INSPECTION FOUND A 4" CRACK IN #4 L/E SLAT PANEL AT O/B ACTUATOR. REPAIRED IAW SRM 57-43-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 4" CRACK IN #4 L/E SLAT PANEL AT O/B ACTUATOR. REPAIRED IAW SRM 57-43-01.