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Accidents · NTSB DEN03FA025 · Final report

Cessna 421 accident near Akron, Colorado, December 25, 2002

On December 25, 2002 at about 5:06 pm local time, a Cessna 421, registered N421D, was destroyed in an accident near Akron, Colorado (Akron/Washington County 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 fractured connecting rods and the pilot not maintaining aircraft control following the engine failure. Factors contributing to the accident were the low altitude, the pilot not maintaining minimum controllable airspeed following the engine failure, the pilot's inability to feather the propeller following the engine failure, oil exhaustion, the seized pistons, and the repair station's improper maintenance on the airplane's engines.

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

What the record shows

Date
December 25, 2002 · about 5:06 pm local time
Place
Akron, Colorado · Akron/Washington County · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Cessna 421 · all 421s on the register
Registration
N421D · no longer on the register · serial 421-0045
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot reported to Denver Air Route Traffic Control Center (ZDV) that his left engine had an oil leak and he requested to land at the nearest airport. ZDV informed the pilot that Akron (AKO) was the closest airport and subsequently cleared the pilot to AKO. On reporting having the airport in sight ZDV terminated radar service, told the pilot to change to the advisory frequency, and reminded him to close his flight plan. Approximately 17 minutes later, ZDV contacted Denver FSS to inquire if the airplane had landed at AKO. Flight Service had not heard from the pilot, and began a search. Approximately 13 minutes later, the local sheriff found the airplane off of the airport. Witnesses on the ground reported seeing the airplane flying westbound. They then saw the airplane suddenly pitch nose down, "spiral two times, and crash." The airplane exploded on impact and was consumed by fire. An examination of the airplane's left engine showed the number 2 and 3 rods were fractured at the journals. The number 2 and 3 pistons were heavily spalded. The engine case halves were fretted at the seam and through bolts. All 6 cylinders showed fretting between the bases and the case at the connecting bolts. The outside of the engine case showed heat and oil discoloration. The airplane's right engine showed similar fretting at the case halves and cylinder bases, and evidence of oil seepage around the seals. It also showed heat and oil discoloration. An examination of the propellers showed that both propellers were at or near low pitch at the time of the accident. The examination also showed evidence the right propeller was being operated under power at impact, and the left propeller was operating under conditions of low or no power at impact. According to the propeller manufacturer, in a sudden engine seizure event, the propeller is below the propeller lock latch rpm. In this situation, the propeller cannot be feathered. Repair station records showed the airplane had been brought in several times for left engine oil leaks. One record showed a 3/4 inch crack found at one of the case half bolts beneath the induction manifold, was repaired by retorquing the case halves and sealing the seam with an unapproved resin. Records also showed the station washed the engine and cowling as the repair action for another oil leak.

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

Pilot

  • Certificate: private
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 1,230 hours in all; 22 in this make and model; 3 in the last 90 days; 2 in the last 30 days; 1,069 as pilot in command
  • Last flight review: June 21, 2002
  • Medical certificate: Class 2
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 3,564.1 hours
  • Last inspection: annual inspection, April 10, 2002; 22.1 hours since
  • Maximum gross weight: 6,500 lb
  • Seats: 8
  • Landing gear: retractable
  • Engine 1: Continental GTSIO-520-D (piston); 0 hours total
  • Engine 2: Continental GTSIO-520-D (piston); 0 hours total
  • Fire on the ground

The flight

  • Departed from: APA Englewood CO at 4:33 pm
  • Destination: MHE Mitchell SD
  • Flight plan: IFR
  • Runway 11, 7,000 ft by 100 ft

Weather at the time

  • Light: daylight
  • Wind: from 310° at 5 knots
  • Visibility: 5 statute miles
  • Sky: clear
  • Temperature: 21°F (-6°C), dew point 18°F (-8°C)
  • Altimeter: 30.04 inHg
  • Observation at 4:53 pm from AKO, 1 miles away

Injuries

FatalSeriousMinorNone
Crew1
Passengers1

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.