What was found
INSPECTION TYPE:C U/D RIGHT CREW DOOR SILL AREA I/B VERTICAL WEB AND ANGLE FOUND CRACKED. CRACK LENGTH .5 INCH. VERTICAL WEB AND ANGLE REPLACED PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C U/D RIGHT CREW DOOR SILL AREA I/B VERTICAL WEB AND ANGLE FOUND CRACKED. CRACK LENGTH .5 INCH. VERTICAL WEB AND ANGLE REPLACED PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.