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DEN01LA130 · Cessna 172RG

28 Jul 2001 · Gunnison, CO, United States

Cessna 172RG · Accident: in flight collision with terrain/water en route

From Gunnison Crested Butte Regional Airport (GUC) to Austin Bergstrom International Airport (AUS)

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Event

NTSB case
DEN01LA130
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
0 · 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 172RG

Aircraft type
Cessna 172
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
N401TA
Operator
Unknown
Onboard fatalities
Unknown
Route
From Gunnison Crested Butte Regional Airport (GUC), Gunnison, COTo Austin Bergstrom International Airport (AUS), Austin, TX
Aircraft age
Not recorded
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 · climb to cruise
First occurrenceThe 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
In flight collision with terrain/water
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

  • Pilot in command › In-flight planning/decision, improper
  • Pilot in command › Proper climb rate, not attained

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

According to the pilot, after takeoff, he climbed to 9,700 feet msl in order to cross the mountains. The airplane then encountered a "300 foot updraft, and then a 2,000 foot downdraft." He decided to "land the plane without the use of the landing gear on the side of the mountain." One of the passengers said it was the pilot's first mountain flying experience. He remembered the airplane was at 80 knots and 8,300 feet as they approached a mountain. He said the pilot pulled back on the control yoke in an attempt to gain sufficient altitude to clear the peak but the airplane was slow in responding and "we literally came straight down" and "the belly [struck the ground] pretty hard." According to rescue personnel, the accident site was at 8,510 feet. The straight line distance between the airport and the accident site was 9 nm. The difference in accident elevation and airport elevation (8,510 - 7,673) was 837 feet. The computed climb rate was 93 feet per nm. Estimated airplane weight was 2,670 pounds at takeoff (maximum certificated gross weight is 2,650 pounds). The altimeter setting was 30.49 inches of mercury, and the computed pressure altitude was 7,103 feet msl. Referring to the Cessna 172RG "Maximum Rate of Climb" chart and interpolating, it was computed that the airplane was capable of achieving a climb rate of 464 fpm (feet per minute) and, at a climb speed of 79 knots, it was capable of climbing 352.4 feet per nm.

Probable cause

the pilot's failure to attain the proper climb rate, and his improper inflight planning/decision to attempt to cross mountainous terrain at an inadequate altitude. Contributing factors were the downdraft and the pilot's total lack of experience in mountain flying.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record DEN01LA130
Event ID
20010807X01621
Case number
DEN01LA130
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
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, coordinates. 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: c1d4be20cd02d0798eaaa14f778721526f05d106698008c35215dc993952e0e8; retrieved 2026-09-21T09:57:25.178Z.