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Accidents · NTSB CEN19LA179 · Final report

Piper PA28 accident near Cottrellville Township, Michigan, June 21, 2019

On June 21, 2019 at about 11:00 pm local time, a 1969 Piper PA28, registered N2360R, was substantially damaged in an accident during approach (VFR pattern base) near Cottrellville Township, Michigan (Marine City Airport). It was a personal flight under general aviation rules (Part 91). 1 person was seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The partial loss of engine power due to carburetor icing and the pilot’s failure to use carburetor heat in weather conditions conducive to serious carburetor icing. The reason for the pilot’s inability to advance the throttle for the go-around could not be determined with the available evidence.

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

What the record shows

Date
June 21, 2019 · about 11:00 pm local time
Place
Cottrellville Township, Michigan · Marine City Airport · map
Type
Accident
Injuries
1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Piper PA28 180, built 1969 · all PA28s on the register
Registration
N2360R · registry record · serial 28-5496
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 the airport traffic pattern at the conclusion of a personal flight when the airplane got too low while on the base leg. The pilot attempted to increase engine power by moving the throttle forward, but the throttle control remained stuck near an idle power setting regardless of how hard he pushed the throttle. The engine continued to run smoothly, but it did not produce enough power to maintain altitude. The pilot did not recall the final moments of the flight. The airplane sustained substantial damage to both wings and the fuselage when it crashed in a field. Postaccident examination revealed that the throttle control was stuck halfway between the idle stop and maximum power due to impact related damage; the throttle control and its associated control cable moved freely after the engine exhaust was removed, the intake airbox was bent into a normal position, and the throttle control cable was disconnected from the carburetor throttle arm. The carburetor heat was found in the off position and the friction lock for the engine controls was fully engaged. The fully engaged friction lock by itself would not prevent the pilot from moving the throttle control with sufficient force. An engine examination did not reveal any preimpact anomalies that would have precluded normal operation during the flight. The weather conditions at the time of the accident were conducive to a serious accumulation of carburetor icing with the engine at glide (descent) power. It is likely that the airplane had a partial loss of engine power due to carburetor icing. A significant accumulation of carburetor ice could have restricted the carburetor’s butterfly valve and, as a result, and restricted normal throttle movement. However, any carburetor ice had likely melted before the postaccident examination and, thus, prevented a conclusive determination on why the pilot was unable to increase the throttle for the go-around.

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 approach (VFR pattern base)
  2. Collision with terrain or object (not controlled flight into terrain) during approach (VFR pattern base)
  3. Loss of engine power (partial) during approach (VFR pattern base)
  4. Fuel related during approach (VFR pattern base) defining event

The NTSB's findings

  • Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › Conducive to carburetor icing › Effect on equipment
  • Aircraft › Aircraft systems › Ice/rain protection system › Intake anti › ice, deice › Not used/operated
  • Personnel issues › Action/decision › Action › Lack of action › Pilot
  • Personnel issues › Action/decision › Info processing/decision › Identification/recognition › Pilot

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 530 hours in all; 6 in the last 90 days; 6 in the last 30 days
  • Last flight review: July 19, 2017
  • Medical certificate: BasicMed
  • Seat: left
  • Injury: serious injuries

The aircraft

  • Airframe total time: 3,099.5 hours
  • Last inspection: annual inspection, July 19, 2018; 4.5 hours since
  • Maximum gross weight: 2,400 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming O-360-A4A (piston); 3,100 hours total

The flight

  • Departed from: PTK Pontiac MI at 10:38 pm
  • Destination: 76G Marine City MI
  • Flight plan: none
  • Runway 04, 3,070 ft by 60 ft

Weather at the time

  • Light: daylight
  • Wind: from 070° at 11 knots
  • Visibility: 10 statute miles
  • Sky: a few clouds at 5,500 ft
  • Temperature: 68°F (20°C), dew point 57°F (14°C)
  • Altimeter: 29.99 inHg
  • Observation at 10:56 pm from MTC, 12 miles away

Weather report (METAR): METAR KMTC 212256Z 07011KT 10SM FEW055 SCT250 20/14 A2999 RMK AO2A SLP159 T01990138=

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 July 22, 2022. 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.