What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
The PIC stated that on September 23, 2019 at approximately 1400 local, he had a stabilized approach to runway 08 at kbdu in Boulder, CO. The pilot stated and it was confirmed that winds were calm at the time of the accident. The pilot stated that the landing was normal and then for an unknown reason he lost directional control of the aircraft resulting in a ground loop. Visual observations of the aircraft show expected ground loop damage.
Slight scuff marks on the left hand main tire outboard sidewall and minor damage to the outboard wheel half rim.
Damage at the left hand wing tip with the trailing edge of the wing tip bend upward with probable damage to the aft spar.
Torn fabric on the lower surface of the trailing edge of the wing tips exposing the internal structure of the wing.
Visible wrinkling in the upper left wing fabric, trailing edge of the wing inboard of the upper aileron cable feed through.
Damage to the left hand aileron, visible crease at the aileron upper cable attach point with the outboard of the attach point deflecting upward.
Minor scrap damage to the lower outboard trailing edge of the left hand elevator, and
Damage to the rudder with the lower 1/3 of the rudder deflecting to the right.
No other notable observations after looking at the tailwheel, brakes, rudder pedals, heel brakes and master cylinders.
As the FAA filed it
THE PIC STATED THAT ON SEPTEMBER 23, 2019 AT APPROXIMATELY 1400 LOCAL, HE HAD A STABILIZED APPROACH TO RUNWAY 08 AT KBDU IN BOULDER, CO. THE PILOT STATED AND IT WAS CONFIRMED THAT WINDS WERE CALM AT THE TIME OF THE ACCIDENT. THE PILOT STATED THAT THE LANDING WAS NORMAL AND THEN FOR AN UNKNOWN REASON HE LOST DIRECTIONAL CONTROL OF THE AIRCRAFT RESULTING IN A GROUND LOOP. VISUAL OBSERVATIONS OF THE AIRCRAFT SHOW EXPECTED GROUND LOOP DAMAGE.
SLIGHT SCUFF MARKS ON THE LEFT HAND MAIN TIRE OUTBOARD SIDEWALL AND MINOR DAMAGE TO THE OUTBOARD WHEEL HALF RIM.
DAMAGE AT THE LEFT HAND WING TIP WITH THE TRAILING EDGE OF THE WING TIP BEND UPWARD WITH PROBABLE DAMAGE TO THE AFT SPAR.
TORN FABRIC ON THE LOWER SURFACE OF THE TRAILING EDGE OF THE WING TIPS EXPOSING THE INTERNAL STRUCTURE OF THE WING.
VISIBLE WRINKLING IN THE UPPER LEFT WING FABRIC, TRAILING EDGE OF THE WING INBOARD OF THE UPPER AILERON CABLE FEED THROUGH.
DAMAGE TO THE LEFT HAND AILERON, VISIBLE CREASE AT THE AILERON UPPER CABLE ATTACH POINT WITH THE OUTBOARD OF THE ATTACH POINT DEFLECTING UPWARD.
MINOR SCRAP DAMAGE TO THE LOWER OUTBOARD TRAILING EDGE OF THE LEFT HAND ELEVATOR, AND
DAMAGE TO THE RUDDER WITH THE LOWER 1/3 OF THE RUDDER DEFLECTING TO THE RIGHT.
NO OTHER NOTABLE OBSERVATIONS AFTER LOOKING AT THE TAILWHEEL, BRAKES, RUDDER PEDALS, HEEL BRAKES AND MASTER CYLINDERS.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N4785F · 3
Matched to the same aircraft by N-number and date.