The U.S. aircraft register, updated daily
Accidents · NTSB CEN19LA249 · Final report

Cessna A185 accident near Saginaw, Michigan, August 3, 2019

On August 3, 2019 at about 2:00 pm local time, a 1970 Cessna A185, registered N5806J, was substantially damaged in an accident during enroute near Saginaw, Michigan. It was a personal flight under general aviation rules (Part 91). 4 people had minor injuries. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

Maintenance personnel’s failure to properly align the crankshaft during an engine reassembly which led to a fatigue failure of the crankshaft and the loss of all engine power.

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

What the record shows

Date
August 3, 2019 · about 2:00 pm local time
Place
Saginaw, Michigan · map
Type
Accident
Injuries
4 people had minor injuries.
Weather
visual conditions (good weather)
Aircraft
Cessna A185 E, built 1970 · all A185s on the register
Registration
N5806J · no longer on the register · serial 18501775
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot was in cruise flight in a single-engine airplane when the engine lost power. He selected a road for the forced landing, during which the airplane impacted a power pole and electrical wires. The airplane came to rest inverted and incurred substantial damage to the airplane’s fuselage and wings. Postaccident examination revealed that the engine’s crankshaft had failed due to fatigue. The accident crankshaft was subject to a mandatory service bulletin (MSB) and subsequent Federal Aviation Administration airworthiness directive (AD) requiring inspection of the crankshaft material for metallurgical anomalies; however, this inspection was not performed on the accident airplane’s crankshaft. A detailed metallurgical examination of the crankshaft revealed that a fatigue crack had progressed through most of the crankshaft web cross section, consistent with relatively low-stress, high cycle fatigue. Because no indications of intergranular fracture or large areas of overstress fracture with the planar dimpled rupture features indicative of thermal damage on the fracture surface were noted, it is unlikely that manufacturing issues resulted in the fatigue cracking even though metallurgical testing revealed that the crankshaft material did not meet specification. Rather, the cracking likely initiated due to stray or excessive wear to the forward journal to web radius. It is further likely that a misalignment during a previous reassembly of the engine that occurred about two years prior when two cylinders were replaced resulted in the failure. Given this information, it is likely that maintenance personnel’s failure to properly align the affected crankshaft during the reassembly resulted in a low-stress high cycle fatigue failure of the crankshaft and the subsequent loss of all engine power.

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

The NTSB's findings

  • cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip engine power section › Failure
  • Personnel issues › Task performance › Maintenance › Scheduled/routine maintenance › Maintenance personnel

Pilot

  • Certificate: private
  • Ratings: single-engine land; single-engine sea; instrument: airplane
  • Flight time: 1,500 hours in all; 1,300 in this make and model; 6 in the last 90 days; 6 in the last 30 days
  • Last flight review: July 22, 2019
  • Medical certificate: Class 3
  • Seat: left
  • Injury: minor injuries

The aircraft

  • Airframe total time: 1,541.5 hours
  • Last inspection: annual inspection, August 25, 2018
  • Landing gear: fixed
  • Engine: Continental IO-520-D (piston); 1,556 hours total

The flight

  • Departed from: KFNT Flint MI at 1:30 pm
  • Destination: KSJX Beaver Island MI
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 280° at 6 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 75°F (24°C), dew point 57°F (14°C)
  • Altimeter: 30.10 inHg
  • Observation at 1:53 pm from KMBS, 9 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers3

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

8 documents, released by the NTSB on October 26, 2021. 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.