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Accidents · NTSB WPR15LA032 · Final report

Cessna T210M accident near Jacksonville, Oregon, November 2, 2014

On November 2, 2014 at about 10:56 pm local time, a 1977 Cessna T210M, registered N1593M, was substantially damaged in an accident during enroute (cruise) near Jacksonville, Oregon. It was a personal flight under general aviation rules (Part 91). 1 person had minor injuries. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A loss of engine power during cruise flight due to the failure of the No. 6 connecting rod, which resulted from oil starvation.

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

What the record shows

Date
November 2, 2014 · about 10:56 pm local time
Place
Jacksonville, Oregon · map
Type
Accident
Injuries
1 person had minor injuries.
Weather
visual conditions (good weather)
Aircraft
Cessna T210M M, built 1977 · all T210Ms on the register
Registration
N1593M · no longer on the register · serial 21061949
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot reported that, during cruise flight, the engine began running roughly with smoke developing inside the cabin, followed by oil covering the windshield. The pilot stated that the engine continued to run and that his attempts to increase the power setting resulted in severe shaking and more smoke. The pilot initiated a forced landing in a nearby field. During the landing roll, the nosewheel landing gear dug into mud, and the airplane subsequently nosed over. Postaccident examination of the engine revealed that the Nos. 5 and 6 connecting rods were liberated from the crankshaft. The No. 6 connecting rod was thermally discolored and fractured, which was likely caused by oil starvation to the No. 6 connecting rod journal and bearing. The No. 5 connecting rod was also fractured; however, the connecting rod and bearing did not exhibit thermal discoloration or distress; the fracture likely resulted due to damage sustained when the No. 6 connecting rod fractured. The Nos. 1 and 2 connecting rods also exhibited thermal discoloration and distress, which likely resulted from the engine's continued operation after the liberation of the No. 6 connecting rod.

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 engine power (total) during enroute (cruise) defining event
  2. Collision with terrain or object (not controlled flight into terrain) during landing (landing roll)
  3. Nose over/nose down during landing (landing roll)

The NTSB's findings

  • cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip engine power section › Failure
  • Environmental issues › Physical environment › Terrain › Wet/muddy › Contributed to outcome
  • cause Aircraft › Fluids/misc hardware › Fluids › Oil › Fluid level

Pilot

  • Certificate: private
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 4,300 hours in all; 1,300 in this make and model; 75 in the last 90 days; 25 in the last 30 days; 4,250 as pilot in command
  • Last flight review: January 13, 2014
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: minor injuries

The aircraft

  • Airframe total time: 5,308.3 hours
  • Last inspection: annual inspection, April 11, 2014; 111 hours since
  • Maximum gross weight: 3,803 lb
  • Landing gear: retractable
  • Engine: Cont Motor TSIO-520 SER (piston); 0 hours total

The flight

  • Departed from: Grants Pass OR at 10:20 pm
  • Destination: Long Beach CA
  • Flight plan: IFR

Weather at the time

  • Light: daylight
  • Wind: from 330° at 4 knots
  • Visibility: 10 statute miles
  • Sky: scat at 5,000 ft
  • Temperature: 55°F (13°C), dew point 37°F (3°C)
  • Altimeter: 30.22 inHg

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.