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DEN01LA022 · Cessna 210C

13 Dec 2000 · Boulder, CO, United States

Cessna 210C · Accident: total loss of engine power (non-mechanical) during initial climb

From 1V5 · CO to Centennial Airport (APA)

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Event

NTSB case
DEN01LA022
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
0
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 210C

Aircraft type
Cessna 210
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
N969RJ
Operator
Unknown
Onboard fatalities
Unknown
Route
From 1V5 · COTo Centennial Airport (APA), Englewood, CO
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
Initial climb
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
Total loss of engine power (non-mechanical)
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Fuel contamination
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Fluid, fuel › Contamination, water
  • Pilot in command › Refueling, not performed

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

NTSB narrative

The airplane had sat dormant for almost 8 years, and extensive checks and servicing were performed to prepare it for a ferry flight to a nearby airport where it was scheduled to undergo an annual inspection. FAA issued a ferry permit. The airplane was placed in a heated hangar the night before the flight. When the pilot preflighted the airplane the next morning, 'a little water' was found in the gascolator and 'a tiny amount' was found in the right wing sump. He chose not to have the fuel drained and the airplane serviced with fresh fuel. He later told a local newspaper that he had drained the fuel system and thought he had removed all the water, 'but apparently it was not enough.' He was unsuccessful in trying to start the engine. After it was preheated, the engine started, and he performed 'an extended time warm up and extended pretakeoff run-up.' Shortly after taking off, the engine lost 'complete power.' The pilot enriched the mixture and turned the auxiliary fuel pump first to LOW, then to HIGH. Power returned momentarily, then the engine lost power again. The pilot did not have a chance to switch fuel tanks, but concentrated instead on the forced landing. The airplane 'skimmed the tops of hills, went through a fence, nosed over, and tumbled 2 or 3 times.' Later examination of the engine disclosed the plunger in the fuel manifold was frozen in position, and there was ice in the chamber under the screen.

Probable cause

Total loss of engine power due to fuel contamination (water), and failure of the pilot to have the airplane completely refueled. A factor was unsuitable terrain on which to make a forced landing.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record DEN01LA022
Event ID
20010110X00074
Case number
DEN01LA022
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. 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: b338049ce90945f8eeccd2ddf719a002fb3d634ef7e858686315728bc4283158; retrieved 2026-09-22T12:17:15.218Z.