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Accidents · NTSB CEN18LA031 · Final report

Cessna T210N accident near Grayslake, Illinois, November 12, 2017

On November 12, 2017 at about 11:30 pm local time, a 1979 Cessna T210N, registered N5300A, was substantially damaged in an accident during approach near Grayslake, Illinois (Campbell airport). It was a business flight under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was instrument conditions (cloud, fog or low visibility).

The NTSB's probable cause their words, unchanged

The failure of the No. 4 connecting rod due to inadequate oil lubrication for reasons that could not be determined because the postaccident engine examination did not reveal any anomalies that would have caused a lack of lubrication.

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

What the record shows

Date
November 12, 2017 · about 11:30 pm local time
Place
Grayslake, Illinois · Campbell · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
instrument conditions (cloud, fog or low visibility)
Aircraft
Cessna T210N, built 1979 · all T210Ns on the register
Registration
N5300A · registry record · serial 21063356
Damage
Substantial damage
Flight
Business flight · general aviation rules (Part 91)

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

While en route on an instrument flight rules cross-country flight, the pilot noticed that the engine oil pressure had decreased; the oil pressure gauge was indicating in the yellow range, but the other engine instruments were showing normal indications. During the descent to landing, when the airplane was about 2,500 ft mean sea level, the pilot heard a "loud bang" from the engine, and smoke filled the cockpit. After declaring an emergency and requesting vectors from air traffic control to the nearest airport, the pilot executed an emergency landing just short of the runway in a wet, grassy area; the airplane slid, came to rest upright on the runway, and sustained substantial damage. A postaccident examination of the engine revealed two large holes in the crankcase and mechanical damage on the inside of both crankcase halves. The No. 4 connecting rod, which exhibited thermal damage signatures, had separated from the crankshaft and thus punctured the holes in the crankcase. The No. 4 connecting rod bearings were significantly damaged consistent with lack of lubrication, and all of the connecting rod bearings displayed smear-type signatures consistent with lubrication distress. Gouging was found inside the oil pump consistent with the passage of hard particles during engine operation; it is likely that the metal pieces from the damaged engine passed through the oil pump and created the gouges. The turbocharger's oil scavenge check valve spring was found broken, which resulted in the check valve not closing automatically; it would not restrict oil traveling from the turbo to the scavenge pump. The pilot reported a normal oil level before the flight and no signs of oil leaking. Further, according to the engine manufacturer, an open check valve would not have any effect on oil consumption during engine operation; thus, it was not a factor in this accident. The reason for the lack of lubrication could not be determined.

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 approach defining event
  2. Off-field or emergency landing during landing

The NTSB's findings

  • cause Aircraft › Fluids/misc hardware › Fluids › Oil › Fluid level

Pilot

  • Certificate: flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 1,544 hours in all; 42 in this make and model; 213 in the last 90 days; 1,464 as pilot in command
  • Last flight review: November 7, 2017
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 3,996 hours
  • Last inspection: annual inspection, November 1, 2016
  • Seats: 6
  • Landing gear: retractable
  • Engine: Continental Motors IO-550-P (piston); 1,030 hours total
  • Operator: Runzel Brothers Aviation LLC

The flight

  • Departed from: PIR Pierre SD at 8:35 pm
  • Destination: PWK Chicago/Prospect Heights/Wheeling IL
  • Flight plan: IFR
  • Runway 09, 3,270 ft by 40 ft

Weather at the time

  • Light: night
  • Wind: from 320° at 5 knots
  • Visibility: 3 statute miles
  • Sky: broken clouds at 600 ft
  • Temperature: 37°F (3°C), dew point 37°F (3°C)
  • Altimeter: 30.37 inHg
  • Observation at 11:52 pm from KPWK, 15 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

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

10 documents, released by the NTSB on December 17, 2019. 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.