What was found
(CAN) INSPECTION OF CENTER FUSELAGE PRESSURE PANEL FS35-36 L/H, REVEALED CRACK INDICATION IN HOLE `B` (OUTBOARD HOLE) IN SKIN LAYER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) INSPECTION OF CENTER FUSELAGE PRESSURE PANEL FS35-36 L/H, REVEALED CRACK INDICATION IN HOLE `B` (OUTBOARD HOLE) IN SKIN LAYER.