What was found
PIT - DURING Q-3 CHECK INSPECTION, FOUND 1.50 INCH CRACK IN CUSP MEMBRANE, STA 596, LONGERON 18R. MFG NEW SECTION OF WEB MEMBRANE AND INSTALLED PER SRM 53-01. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-3 CHECK INSPECTION, FOUND 1.50 INCH CRACK IN CUSP MEMBRANE, STA 596, LONGERON 18R. MFG NEW SECTION OF WEB MEMBRANE AND INSTALLED PER SRM 53-01. (X)