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Accidents · NTSB LAX08LA153 · Final report

Cessna P210N accident near Peach Springs, Arizona, May 23, 2008

On May 23, 2008 at about 6:50 pm local time, a Cessna P210N, registered N4753K, was substantially damaged in an accident during enroute (cruise) near Peach Springs, Arizona. It was a personal flight under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A loss of engine power due to induced catastrophic internal failure of the engine as a result of the displacement and rotation of the number 2 main bearing that resulted in a fatigue fracture of the crankshaft.

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

What the record shows

Date
May 23, 2008 · about 6:50 pm local time
Place
Peach Springs, Arizona · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Cessna P210N · all P210Ns on the register
Registration
N4753K · no longer on the register · serial P21000284
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

During an instrument flight rules cross-country flight at 16,000 feet msl, the pilot reported to air traffic control that he had a total loss of engine power and was attempting to land at an airport about 12 miles from his current position. The pilot was unable reach the airport, and while trying to land on the desert floor, one of the main landing gear wheels hit a cactus and the airplane nosed over. During the recovery of the airplane, internal components of the engine where found in the debris field. The time recorded on the engine at the last annual inspection was 978 hours since major overhaul. A review of the airplane logbooks revealed that a top overhaul was completed on March 21, 2007, which included all 6 cylinders being removed, overhauled, and replaced. The engine failure occurred 120 hours since completion of the top overhaul. During the engine examinations, thermal discoloration of the crankshaft main journals and damage to various other internal components were noted. The crankshaft was fractured just forward of the number 2 main bearing. The number 2 main bearing was not located; however, the bearing support exhibited evidence of bearing shift, tang slot elongation, and rotation. The crankshaft main bearings and the connecting rod bearings were also damaged as a result of oil starvation, due to the number 2 main bearing rotation. The crankcase itself had been compromised just above the numbers 3 and 4 cylinders. The crankshaft was metallurgically examined at a laboratory. The crankshaft chemistry, case depth, surface hardness, and core hardness met specifications. The fracture initiated at the surface adjacent to the number 2 main bearing and progressed toward the number 3 rod journal in fatigue.

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. Powerplant sys/comp malf/fail during enroute (cruise) defining event
  2. Loss of engine power (total) during enroute (cruise)
  3. Off-field or emergency landing during emergency descent

The NTSB's findings

  • cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip engine power section › Failure

Pilot

  • Certificate: private
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 3,090 hours in all; 2,018 in this make and model; 17 in the last 90 days; 7 in the last 30 days; 3,090 as pilot in command
  • Last flight review: July 25, 2007
  • Medical certificate: Class 3 (without waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 2,950 hours
  • Last inspection: annual inspection, October 4, 2007; 36 hours since
  • Maximum gross weight: 4,000 lb
  • Seats: 6
  • Landing gear: retractable
  • Engine: Cont Motor TSIO-520 SER (piston); 0 hours total

The flight

  • Departed from: GCN Grand Canyon AZ at 6:00 pm
  • Destination: IFP Bullhead City AZ
  • Flight plan: IFR

Weather at the time

  • Light: daylight
  • Wind: from 240° at 20 knots
  • Visibility: 20 statute miles
  • Sky: broken clouds at 8,000 ft; scat at 6,000 ft
  • Temperature: 45°F (7°C), dew point 34°F (1°C)
  • Altimeter: 29.76 inHg
  • Observation at 6:30 pm from PRC, 54 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

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.