Piper PA28 accident near Guthrie Center, Iowa, November 9, 2018
On November 9, 2018 at about 11:15 pm local time, a 1979 Piper PA28, registered N91770, was substantially damaged in an accident during enroute (cruise) near Guthrie Center, Iowa (Guthrie County Rgnl airport). It was a personal flight under general aviation rules (Part 91). 4 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
Pilot incapacitation due to carbon monoxide poisoning as a result of an undetected crack in an engine exhaust muffler, which permitted entry of exhaust gasses into the cabin via the cabin heat system.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- November 9, 2018 · about 11:15 pm local time
- Place
- Guthrie Center, Iowa · Guthrie County Rgnl · map
- Type
- Accident
- Injuries
- 4 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Piper PA28 236, built 1979 · all PA28s on the register
- Registration
- N91770 · no longer on the register · serial 287911174
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
About 45 minutes into the cross-country flight, the student pilot passenger reported to air traffic control that the pilot was having a heart attack and that he was going to take control of the airplane and divert to an airport about 20 miles away; however, another airport was much closer, and controllers received no further communications from the pilot. The student then reported over the nearby airport’s common traffic advisory frequency that he would attempt to divert there. GPS flight track data indicated that, a short time later, the airplane began to fly in an erratic manner, climbing and descending over the area of the diversion airport. The airplane subsequently collided with terrain in a wings-level attitude. All four occupants sustained fatal injuries, and toxicology testing indicated that all had high levels of carboxyhemoglobin, which is caused by the inhalation of carbon monoxide (CO), an odorless, tasteless, colorless, nonirritating gas formed by hydrocarbon combustion. Levels in both pilots and one passenger where high enough to have caused confusion, seizures, or loss of consciousness. There was no evidence the pilot had a heart attack, so his symptoms were likely due to the CO poisoning. The engine was equipped with three identical exhaust mufflers. Examination of the aft muffler revealed a crack that allowed engine exhaust gases to enter the cabin through the cabin heating system. The muffler’s crack developed as a result of corrosion and thinning of the muffler wall. The crack and small perforations in the muffler wall were likely present at the time of the last inspection, which occurred shortly before the accident; however, due to damage from impact, it could not be determined if the extent of cracking was readily visible at the time of inspection. Also, the crack could have opened just before the accident flight due to an engine backfire that occurred during startup. Use of a pressure check during an inspection could help identify cracks and small perforations that can be obscured by oxides and deposits during a visual inspection; however, the manufacturer's service manual only recommended a pressure check when a visual inspection could not be accomplished. The manufacturer and Federal Aviation Administration (FAA) both recommended that the mufflers be replaced at or near 1,000 hours time in service (TIS). Although maintenance records revealed that three mufflers were replaced over the previous 27 years, the records did not indicate if the cracked muffler was one of those that had been replaced. Review of the available records indicated that the cracked muffler likely had at least 752 hours TIS, but due to missing records, it could have had over 1,033 hours TIS. Additionally, one of the mufflers was replaced at 549 hours TIS, well before the manufacturer's recommended interval, and likely an indication of premature failure. The hazard of CO poisoning via leaks in reciprocating engine exhaust systems that are used to provide cabin heat has long been known to the industry. In 2004, the NTSB issued a safety recommendation to the FAA to require the installation of CO detectors in all single-engine airplanes such as the accident type. In response, the FAA undertook extensive research on the detection and prevention of CO exposure in general aviation aircraft, created a technical standard order specifying minimum performance standards for CO detectors, and recommended, but did not require, that all operators install CO detectors. The FAA concluded that the primary method to prevent CO contamination in the cabin is through proper inspection and maintenance of mufflers and exhaust system components and that CO detectors are a secondary method of preventing CO exposure. The FAA further stated that since a lack of a CO detector alone is not unsafe, installing a CO detector would not correct an unsafe condition. Because the FAA did not require installation of CO detectors, the safety recommendation was classified "Closed – Unacceptable Action."
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
- Powerplant sys/comp malf/fail during enroute (cruise) defining event
- Loss of control in flight during enroute (cruise)
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Aircraft › Aircraft power plant › Engine exhaust › (general) › Fatigue/wear/corrosion
- cause Personnel issues › Physical › Impairment/incapacitation › Carbon monoxide › Pilot
- cause Personnel issues › Physical › Impairment/incapacitation › Carbon monoxide › Student/instructed pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Directional control › Attain/maintain not possible
- cause Aircraft › Aircraft systems › Indicating/recording systems › (general) › Not installed/available
Pilot
- Certificate: private
- Ratings: single-engine land; instrument: airplane
- Flight time: 1,130 hours in all; 500 in this make and model; 60 in the last 90 days; 30 in the last 30 days
- Last flight review: August 10, 2018
- Medical certificate: Class 3
- Seat: left
- Injury: fatal
Dual student
- Certificate: student
- Flight time: 100 hours in all; 100 in this make and model
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 2,955 hours
- Last inspection: annual inspection, November 3, 2008; 1 hours since
- Maximum gross weight: 3,000 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-540-J3A5D (piston); 272 hours total
The flight
- Departed from: LRJ Le Mars IA at 10:18 pm
- Destination: I75 Osceola IA
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: dusk
- Wind: from 310° at 9 knots, gusting 18
- Visibility: 10 statute miles
- Sky: broken clouds at 4,400 ft; clear
- Temperature: 19°F (-7°C), dew point 10°F (-12°C)
- Altimeter: 30.40 inHg
- Observation at 11:15 pm from KADU, 18 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 | |||
| Passengers | 2 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
19 documents, released by the NTSB on November 13, 2020. 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.
