What was found
DURING CHECK-C MAINT FOUND COCKPIT FLOOR PANEL ATTACH ANGLE CRACKED AT STA 121, LBL 2 INCHES. INSTALLED NEW ANGLE PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT FOUND COCKPIT FLOOR PANEL ATTACH ANGLE CRACKED AT STA 121, LBL 2 INCHES. INSTALLED NEW ANGLE PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-05.