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WPR14FA252 · Cessna 175

18 Jun 2014 · Moab, UT, United States

Cessna 175 · Accident: loss of control in flight en route

From Durango La Plata County Airport (KDRO) to Brigham City Regional Airport (KBMC)

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Event

NTSB case
WPR14FA252
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
1 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Cessna 175

Aircraft type
Cessna 175
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N7043M
Onboard fatalities
Unknown
Route
From Durango La Plata County Airport (KDRO), Durango, COTo Brigham City Regional Airport (KBMC), Brigham City, UT
Aircraft age
About 56 years (built 1958)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
En route · change of cruise level
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Loss of control in flight
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Aircraft › Aircraft oper/perf/capability
  • Environmental issues › Physical environment
  • Personnel issues › Action/decision
  • Personnel issues › Psychological
  • Personnel issues › Task performance

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

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.

Probable cause

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.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record WPR14FA252
Event ID
20140619X70017
Case number
WPR14FA252
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: ee498eafa8d73b4bf847540937eec96eb4ba97a5d4d420706c01905e48256956; retrieved 2026-09-14T17:20:04.162Z.