What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
On September 3, 2025, at approximately 1210 central daylight time, privacy data omitted, a Gulfstream G-150, privacy data omitted, was substantially damaged during landing when it overran runway 34 at chicago executive airport, IL, and impacted the emergency arresting system (emas) and perimeter fencing. The pilot and copilot were uninjured and there were no passengers on board. The aircraft was operated uner part 91 flight. The wx was reported as wind 260 at 10 gust 17 visibility 10SM light rain overcast 9,500 tempurature 21 dewpoint 16 altimeter 2979.
Substantial damage to the aircraft was noted on the belly lower fuselage skin and critical structural frame due to the nose landing gear collapsing aft into the fuselage. Additional damage noted was on the left wing leading edge, landing gear doors, nose landing gear, main landing gear wheel wells, and upper fuselage.
As the FAA filed it
ON SEPTEMBER 3, 2025, AT APPROXIMATELY 1210 CENTRAL DAYLIGHT TIME, ^PRIVACY DATA OMITTED^, A GULFSTREAM G-150, ^PRIVACY DATA OMITTED^, WAS SUBSTANTIALLY DAMAGED DURING LANDING WHEN IT OVERRAN RUNWAY 34 AT CHICAGO EXECUTIVE AIRPORT, IL, AND IMPACTED THE EMERGENCY ARRESTING SYSTEM (EMAS) AND PERIMETER FENCING. THE PILOT AND COPILOT WERE UNINJURED AND THERE WERE NO PASSENGERS ON BOARD. THE AIRCRAFT WAS OPERATED UNER PART 91 FLIGHT. THE WX WAS REPORTED AS WIND 260 AT 10 GUST 17 VISIBILITY 10SM LIGHT RAIN OVERCAST 9,500 TEMPURATURE 21 DEWPOINT 16 ALTIMETER 2979.
SUBSTANTIAL DAMAGE TO THE AIRCRAFT WAS NOTED ON THE BELLY LOWER FUSELAGE SKIN AND CRITICAL STRUCTURAL FRAME DUE TO THE NOSE LANDING GEAR COLLAPSING AFT INTO THE FUSELAGE. ADDITIONAL DAMAGE NOTED WAS ON THE LEFT WING LEADING EDGE, LANDING GEAR DOORS, NOSE LANDING GEAR, MAIN LANDING GEAR WHEEL WELLS, AND UPPER FUSELAGE.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.