The U.S. aircraft register, updated daily
Accidents · NTSB CEN21FA007 · Final report

Beech S35 accident near Telluride, Colorado, October 5, 2020

On October 5, 2020 at about 7:04 pm local time, a 1964 Beech S35, registered N4444K, was substantially damaged in an accident during enroute (climb to cruise) near Telluride, Colorado (Telluride Municipal airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot’s loss of control during the climb to cruise flight resulting in the airplane’s impact with terrain. Contributing to the accident was the pilot’s decision to not climb to a higher altitude before proceeding over high terrain.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
October 5, 2020 · about 7:04 pm local time
Place
Telluride, Colorado · Telluride Municipal · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Beech S35, built 1964 · all S35s on the register
Registration
N4444K · registry record · serial D-7422
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The airplane departed on a visual flight rules cross-country flight from a high-elevation (9,078 ft mean sea level) airport. Automated dependent surveillance-broadcast (ADS-B) data showed that the airplane proceeded east into a box canyon with rising terrain. The data showed that, before entering the box canyon, the airplane did not climb toward the west, where there was lower terrain. The data also showed that the airplane was in a gradual climb for about 8 miles into the canyon and that the airplane then made a right turn to the south just before impacting terrain. No known radio distress calls were received from the pilot. The airplane wreckage showed evidence of a nearly vertical impact. Postaccident examination found no preimpact anomalies with the airframe, engine, flight controls, and propeller. Flight control continuity was confirmed from the cockpit to all flight control surfaces. The elevation of the accident site was 11,823 ft mean sea level. The surrounding terrain to the north, east, and south was higher than the accident site elevation, with peaks ranging from about 12,000 to 14,000 ft. In addition, the calculated density altitude in the area of the accident site was about 13,604 ft, which would have diminished the airplane’s climb performance. There was no significant turbulence in the area. Thus, the pilot likely turned the airplane toward higher terrain and into the box canyon before the airplane could gain enough altitude to traverse the high terrain, resulting in a loss of control.

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

  1. Loss of control in flight during enroute (climb to cruise) defining event

The NTSB's findings

  • Personnel issues › Task performance › (general) › (general) › Pilot
  • Environmental issues › Physical environment › Terrain › Mountainous/hilly terrain › Contributed to outcome
  • Personnel issues › Task performance › Planning/preparation › Performance calculations › Pilot
  • Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › High density altitude › Contributed to outcome

Pilot

  • Certificate: airline transport pilot, flight instructor
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 5,750 hours in all; 130 in this make and model
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 5,516 hours
  • Last inspection: annual inspection, December 1, 2019; 140 hours since
  • Maximum gross weight: 3,300 lb
  • Seats: 4
  • Landing gear: retractable
  • Engine: Continental IO-520-BA (piston); 5,516 hours total

The flight

  • Destination: PWA Oklahoma City OK

Weather at the time

  • Light: daylight
  • Wind: from 260° at 10 knots, gusting 17
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 64°F (18°C), dew point 9°F (-13°C)
  • Altimeter: 30.49 inHg
  • Observation at 12:55 pm from TEX, 8 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

10 documents, released by the NTSB on December 1, 2022. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

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.