Cessna 175 accident near Moab, Utah, June 18, 2014
On June 18, 2014 at about 1:36 pm local time, a 1958 Cessna 175, registered N7043M, was destroyed in an accident during enroute (change of cruise level) near Moab, Utah. It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s decision to approach rising mountainous terrain at too low an altitude to clear it and his subsequent attempt to climb, which exceeded the airplane’s critical angle-of-attack and resulted in a stall/spin.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 18, 2014 · about 1:36 pm local time
- Place
- Moab, Utah · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Cessna 175, built 1958 · all 175s on the register
- Registration
- N7043M · no longer on the register · serial 55343
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The airline transport pilot was conducting a personal cross-country flight in the accident airplane behind another airplane. Radar data showed that the accident airplane was trailing about 2 to 3 miles behind the lead airplane and that both airplanes were proceeding northwest at 9,400 ft mean sea level (msl). The lead pilot reported that the flight route included flying through a mountain pass at an of elevation 10,150 ft msl. The lead airplane exited the pass to the west, and the lead airplane pilot then lost communications with the accident airplane pilot. The next day, a search and rescue helicopter pilot located the airplane wreckage on the eastern slope of the pass about 1/2 mile below the mountain pass ridge, in a steep wooded valley, at an elevation of 9,804 ft msl. An on-scene examination was conducted; broken tree tops, vertical witness marks on three trunks, and the compact nature of the wreckage footprint were consistent with the airplane impacting terrain in a near-vertical descent after a low-altitude stall/spin. A postaccident fire destroyed a majority of the airplane. No preimpact mechanical failures or malfunctions were found that would have precluded normal operation. The terrain rises 1,100 ft vertically over a distance of 2 miles as the mountain pass is approached in the direction that the accident airplane was traveling. The airplane's maximum climb rate at 10,000 ft was calculated to be about 650 ft per minute at 83 mph, which was not sufficient to climb the airplane over the rising terrain at the point that the pilot started the ascent and this led to his exceedance of the airplane's critical angle-of-attack and the airplane entering a stall/spin.
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 control in flight during enroute (change of cruise level) defining event
The NTSB's findings
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Environmental issues › Physical environment › Terrain › Mountainous/hilly terrain › Decision related to condition
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
- cause Personnel issues › Psychological › Attention/monitoring › Monitoring environment › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Not attained/maintained
- cause Personnel issues › Task performance › Planning/preparation › Flight planning/navigation › Pilot
- cause Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
Pilot
- Certificate: airline transport pilot
- Ratings: multi-engine land; single-engine land; instrument: airplane
- Flight time: 4,300 hours in all
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: unk
- Injury: fatal
The aircraft
- Last inspection: inspection type not recorded
- Maximum gross weight: 2,348 lb
- Seats: 4
- Landing gear: fixed
- Engine: Franklin 6A&6V335 SER (piston); 0 hours total
- Fire on the ground
The flight
- Departed from: KDRO Durango CO at 12:30 pm
- Destination: KBMC Brigham City UT
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: at 5 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 64°F (18°C), dew point 25°F (-4°C)
- Altimeter: 29.98 inHg
- Observation at 1:53 pm from KCNY, 20 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 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.
