What was found
LONGITUDINAL BOX BEAM LT SIDE OF PANEL 21A IS CRACKED AT FORWARD PRESS BULKHEAD. CRACK IS LOCATED ON TOP INBOARD CORNER. CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W EA 28-53-327.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LONGITUDINAL BOX BEAM LT SIDE OF PANEL 21A IS CRACKED AT FORWARD PRESS BULKHEAD. CRACK IS LOCATED ON TOP INBOARD CORNER. CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W EA 28-53-327.