- Location: Willard, UT
- Accident Number: WPR26FA232
- Date & Time: June 23, 2026, 22:47 Local
- Registration: N387AF
- Aircraft: Cessna 172
- Injuries: 1 Fatal
- Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203237/pdf
https://registry.faa.gov/aircraftinquiry/Search/NNumberResult?NNumberTxt=N387AF
On June 23, 2026, at about 2247 mountain daylight time, a Cessna 172S, N387AF, was
destroyed when it was involved in an accident near Willard, Utah. The pilot was fatally injured.
The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.
The instrument-rated private pilot was conducting a solo night cross-country flight as part of a
commercial flight training program. The pilot and his instructor had conducted a dual night
cross-country flight following a similar route as the accident flight about 12 days prior.
On the evening of the accident flight, a flight instructor reviewed the pilot’s plan and
dispatched the airplane. He observed the pilot using Foreflight electronic flight bag (EFB)
software to plan his route and obtain an online briefing for the visual flight rules (VFR) solo
night cross-country flight from Salt Lake City, Utah (SLC) to Idaho Falls, Idaho (IDA). According
to the route the pilot entered in Foreflight, he planned to depart SLC and perform a climbing left
turn to an enroute altitude of 8,500 ft mean sea level (msl). The pilot planned to use the
Mountain Road VFR transition northbound through SLC Class B airspace, as indicated on the
Salt Lake City Terminal Area Chart. The transition procedure required a clearance from air
traffic control (ATC) and specified navigating between several charted VFR waypoints over the
eastern edge of the city, and along the west edge of the mountain range. Upon completion of
the transition, the pilot’s planned route included a left turn to the northwest from the Ogden
Canyon VFR waypoint to the Power Station VFR waypoint, where he would then turn
northbound, and follow prominent interstate highways enroute to Idaho Falls (see figure 1).
The pilot also planned and received a Foreflight briefing for a return flight that same night.
Preliminary ADS-B data from the FAA showed that the airplane departed SLC from runway 17
at about 2225 local time, turned left, and began following the Mountain Road VFR transition
northbound, consistent with the pilot’s planned route (see figure 1). While flying the transition, the pilot communicated with a Salt Lake City Approach air traffic controller; when asked if he
wanted to receive VFR flight following services from Salt Lake Center, he responded that he
did. At about the same time he passed the Weber Canyon VFR waypoint, ATC provided the
pilot a discrete transponder code, which the pilot entered. From that waypoint, the airplane
continued north and overflew the mountain foothills, rather than turning left to navigate to the
McDay-Dee Hospital VFR waypoint as indicated in the planned flight. Upon exiting the Class B
airspace, ATC advised the pilot to maintain his own navigation at an appropriate VFR altitude,
which the pilot acknowledged and repeated back. No further communication was recorded
from the pilot.
Upon reaching the Ogden Canyon VFR waypoint, the airplane did not make the planned left turn
toward the Power Station VFR waypoint. Instead, it continued northbound, maintaining about
8,800 - 9,000 ft msl (ADS-B geometric altitude) until it impacted mountainous terrain southeast
of Willard Peak at 2247:40 (see figure 2).
The wreckage was located in an area of steep, rocky, upsloping mountainous terrain at an
elevation of about 9,130 ft msl. The slope consisted of loose shale-like rock and rock
outcroppings. The airplane came to rest on the south face of the mountain, about 375 ft from
(and about 130 ft in elevation below) the ridgeline. All components of the airframe and several
fragmented engine accessories were present in the vicinity of the primary wreckage. The
engine was located down-slope from the primary wreckage.
Fragments of the engine and its related accessories were found within the primary impact
point area, which was located about 45 ft west of the main wreckage, which consisted of the
fuselage and empennage. Additional engine-related fragments and components were found
throughout the debris field. Ground scarring was limited to the immediate vicinity of the
primary impact point. An additional impact point was identified about 35 ft east of the primary
impact point, which contained fragmented pieces of wingtip material and the right wingtip
position light.
The fuselage exhibited extensive fore-aft crushing along the longitudinal axis. The firewall and
forward fuselage structure were crushed aft to the rear seat position. Both main landing gear
were separated from the fuselage. The horizontal stabilizer was impact damaged; the vertical
stabilizer was impact damaged near its top and missing its beacon light. The wings were
separated from the fuselage, located uphill of the main wreckage and the primary point of
impact. The forward spar carry-through structure remained attached to the left wing. Crushing,
twisting, and bending were noted throughout both wings, and both fuel tanks were ruptured.
The propeller was located within the debris field about 30 ft northwest of the primary impact
point, between the wings and the fuselage. The engine crankshaft flange was separated from
the crankshaft and remained attached to the propeller hub by the attachment bolts. Both propeller blades were curled aft with substantial twisting, leading edge gouges, chordwise
scratches, and scratching throughout the cambered faces.
A line of disturbed ground was observed between the main wreckage and the engine, which
was damaged by impact forces and located about 350 ft downslope from the main wreckage.
At the time of the accident, the moon was 28° above the horizon, at an azimuth of 210°, and
72% illuminated. Some smoke and haze from regional forest fires was present. Visual
meteorological conditions and visibility greater than 10 miles were reported along the accident
airplane’s route of flight. The pilot of another airplane, who was also flying the Mountain Road
transition about 10 nautical miles behind the accident airplane, reported that the flight
conditions were VFR, the horizon and mountainous terrain were dark and mostly indiscernible,
the wind was light, and the ride northbound was smooth.
The wreckage was recovered to a secure facility for further examination.
