What was found
DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: LEFT AND RIGHT NACELLE FRAME 10 WEB, INBD AND OUTBD SIDES DAMAGED. PERFORMED REPAIRS IAW COMAIR ENGINEERING ORDER 54-005.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: LEFT AND RIGHT NACELLE FRAME 10 WEB, INBD AND OUTBD SIDES DAMAGED. PERFORMED REPAIRS IAW COMAIR ENGINEERING ORDER 54-005.