Piper PA28 accident near Aurora, Utah, November 25, 2012
On November 25, 2012 at about 8:00 pm local time, a 1982 Piper PA28, registered N8314E, was substantially damaged in an accident during enroute (climb to cruise) near Aurora, Utah. It was a personal flight under general aviation rules (Part 91). 3 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's failure to maintain clearance with terrain while maneuvering in a remote mountainous region. Contributing to the accident was the pilot's improper decision to traverse the remote mountainous area in high-density altitude conditions with the airplane near its maximum gross weight. Contributing to the delay in the search and rescue (SAR) was the lack of a 406-MHz ELT signal, which would have allowed SAR responders to initiate a more timely search and find the accident site more quickly.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- November 25, 2012 · about 8:00 pm local time
- Place
- Aurora, Utah · map
- Type
- Accident
- Injuries
- 3 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Piper PA28 181, built 1982 · all PA28s on the register
- Registration
- N8314E · no longer on the register · serial 28-8390016
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
Family members reported to the Federal Aviation Administration that the airplane was overdue on the cross-country flight. One week after the initial notification, the wreckage was located in the upper end of a canyon about 11 nautical miles west of the departure airport at an elevation of 8,992 feet mean sea level (msl) in a grove of trees. A ridge, which was located directly in front of and on the airplane's flightpath about 950 feet from the wreckage site, was measured at 9,186 feet msl. Evidence at the accident site indicated that the airplane initially impacted the trees on a southeasterly heading in a level attitude and that its left wing subsequently impacted a tree. The impact rotated the airplane counter-clockwise, and it subsequently came to rest upright on a northwesterly heading about 150 feet from the first point of impact. The airplane was found relatively intact except for the separation of the left wing. A postcrash fire consumed the cabin and cockpit areas; the pilot had refueled before departure. Postaccident examination of the airframe and engine revealed no mechanical anomalies that would have precluded normal operation. Although no hazardous weather conditions were reported in the area at the time of the accident, unexpected turbulent conditions can occur in mountain canyons. Further, the density altitude was calculated to be 9,663 feet, which would have adversely affected the airplane's performance. A family member, who was a pilot, reported that, before the accident pilot departed on the first leg of the three-leg flight, he assisted him in calculating the airplane's weight and balance for each leg. He reported that, for each calculation, he used the estimated weight of each passenger, the baggage, the two dogs, a rifle, and full fuel and that, although the airplane was right at its maximum gross takeoff weight for each leg, it was within its weight and balance limits. He stated that the accident pilot had made this same cross-country flight three or four times previously but that he did not know the extent of the pilot's mountain-flying experience. The pilot's decision to fly in a canyon in high-density altitude conditions near the airplane's maximum gross weight likely contributed to the accident. The airplane was likely equipped with a 121.5/243-MHz emergency locator transmitter (ELT). Due to fire damage, it could not be determined whether the ELT switch was in the armed position or whether the ELT activated immediately after impact. Regardless, the 121.5-MHz signal would only have been detected by other aircraft flying in the remote area because satellite monitoring for 121.5-MHz ELT signals ceased in February 2009. Search and Rescue (SAR) operations, which commenced the day following the accident, took 7 days. During this time period, the Civil Air Patrol from three states flew a total of 86 missions, and local law enforcement agencies conducted additional SAR missions. SAR operations were protracted due to the lack of flight following services, ELT signal and radar data, and a digital emergency signal from a 406-MHz ELT or other satellite emergency notification device and the fact that the white airplane crashed and fragmented in a snowy, forested area, which made visual detection difficult. Two passengers initially survived the accident. They were found at the accident site wearing t-shirts and jeans; however, they were observed with warm weather coats before their departure on the day of the accident. It could not be determined whether any survival equipment was on board the airplane, but none was observed at the accident site; any survival gear may have been consumed by the postcrash fire. No evidence indicated that the survivors attempted to make an overnight shelter. The temperatures at the accident site, which was in a snow-covered area, were reportedly in the high teens to low 20s the night of the accident. The autopsy for both passengers indicated that the cause of death included hypothermia. Therefore, the two passengers did not survive the first night after the accident due to exposure to the cold temperature and the generally inclement weather conditions. It is not known whether an immediate 406-MHz ELT signal would have allowed SAR responders to reach the scene of the accident before the deaths of the two passengers; however, such a signal detection would have initiated an immediate search and greatly enhanced the opportunity for the accident site to be located more quickly.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Loss of lift during enroute (climb to cruise) defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Attain/maintain not possible
- cause Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
- Aircraft › Aircraft oper/perf/capability › Aircraft capability › Maximum weight › Not specified
- Environmental issues › Physical environment › Terrain › Mountainous/hilly terrain › Contributed to outcome
- factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
- factor Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › High density altitude › Effect on operation
- factor Aircraft › Aircraft oper/perf/capability › Aircraft capability › Maximum weight › Incorrect use/operation
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 200 hours in all; 200 in this make and model
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: left
- Injury: fatal
Dual student
- Certificate: student
- Medical certificate: Class 3
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 3,916 hours
- Last inspection: annual inspection, October 6, 2012
- Maximum gross weight: 2,550 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-360-A4M (piston); 3,916 hours total
- Fire on the ground
The flight
- Departed from: FOM Fillmore UT at 7:45 pm
- Destination: GCC Gillette WY
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 290° at 4 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 54°F (12°C), dew point 27°F (-3°C)
- Altimeter: 30.02 inHg
- Observation at 7:59 pm from FOM, 11 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
