What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Aircraft departed dfw and when climbing between 13,000 and 14,000 feet the aircraft struck a large bird of unknown type. The crew heard a loud noise and bird remains covered the first officer's windshield. The crew elected to return to the airport, but stated they did not declare an emergency due to no other malfunctions of the aircraft. Upon examination of the aircraft there was damage to the right side nose area. The bird caused the right side nose avionics panel to depart the aircraft. The panel latches were broken in the impact causing the panel to depart. The aircraft sustained skin damage above the right side pitot tube between fuselage station(fs) 210 and fs 220 between stringer 13A and 14A in the rvsm area. The frame was damaged at fs 193 between bl 13 and bl 22. Lastly, there was skin deformation noted aft of right hand fs 193 between bl 22 and stringer 14A. The aircraft is currently undergoing repair to return to service.
As the FAA filed it
AIRCRAFT DEPARTED DFW AND WHEN CLIMBING BETWEEN 13,000 AND 14,000 FEET THE AIRCRAFT STRUCK A LARGE BIRD OF UNKNOWN TYPE. THE CREW HEARD A LOUD NOISE AND BIRD REMAINS COVERED THE FIRST OFFICER'S WINDSHIELD. THE CREW ELECTED TO RETURN TO THE AIRPORT, BUT STATED THEY DID NOT DECLARE AN EMERGENCY DUE TO NO OTHER MALFUNCTIONS OF THE AIRCRAFT. UPON EXAMINATION OF THE AIRCRAFT THERE WAS DAMAGE TO THE RIGHT SIDE NOSE AREA. THE BIRD CAUSED THE RIGHT SIDE NOSE AVIONICS PANEL TO DEPART THE AIRCRAFT. THE PANEL LATCHES WERE BROKEN IN THE IMPACT CAUSING THE PANEL TO DEPART. THE AIRCRAFT SUSTAINED SKIN DAMAGE ABOVE THE RIGHT SIDE PITOT TUBE BETWEEN FUSELAGE STATION(FS) 210 AND FS 220 BETWEEN STRINGER 13A AND 14A IN THE RVSM AREA. THE FRAME WAS DAMAGED AT FS 193 BETWEEN BL 13 AND BL 22. LASTLY, THERE WAS SKIN DEFORMATION NOTED AFT OF RIGHT HAND FS 193 BETWEEN BL 22 AND STRINGER 14A. THE AIRCRAFT IS CURRENTLY UNDERGOING REPAIR TO RETURN TO SERVICE.