Cessna P337H accident near Laurel, Montana, May 3, 2023
On May 3, 2023 at about 1:45 pm local time, a 1980 Cessna P337H, registered N62PC, was substantially damaged in an accident during enroute (cruise) near Laurel, Montana (Laurel Muni airport). 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 partial loss of engine power to the rear engine resulting from cylinder detonation for undetermined reasons, which resulted in a forced landing and impact with terrain.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- May 3, 2023 · about 1:45 pm local time
- Place
- Laurel, Montana · Laurel Muni · map
- Type
- Accident
- Injuries
- 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Cessna P337H, built 1980 · all P337Hs on the register
- Registration
- N62PC · no longer on the register · serial P337-0345
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot was on a cross-country flight when he maneuvered the airplane to avoid clouds. The maneuvering included a descent followed by an ascent back to the previous altitude. He noted that the airplane’s performance at the cruise-climb power setting was lower than expected and five minutes later the oil pressure indicator for the rear engine began to decrease, with a corresponding increase in indicated oil temperature. The pilot diverted to a nearby airport and shut down the rear engine; however, with the rear engine shut down and the forward engine at full power, there was not enough power to maintain altitude. The airplane stalled about 10 ft above the ground and the left wing sustained substantial damage when it impacted a steel post. The airplane rotated 180° and sustained further substantial damage to the airframe after it came to rest in an irrigation ditch. Postaccident examination of the rear engine revealed that the Nos. 4 and 5 cylinders had signatures consistent with detonation in the form of erosion on the edges of the piston faces. A postaccident examination of the front engine revealed that it also exhibited erosion signatures of the piston faces and internal damage to the cylinders that likely resulted in a degradation of power. Also, the investigation could not determine the reason for the detonation, causes include improper ignition timing, high inlet air temperature, engine overheating, carbon build-up or oil in the combustion chamber, an issue with the fuel octane, or an overly lean fuel-to-air mixture. Although the magneto-to-engine timing could not be determined postaccident, there were no postaccident anomalies noted with either the magnetos or the ignition harnesses. Without an EGT gauge, the effect on the engine temperatures as a result of the pilot’s leaning procedures is unknown.
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
- Loss of engine power (partial) during enroute (cruise) defining event
The NTSB's findings
- Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng cyl section › Failure
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Attain/maintain not possible
- Aircraft › Aircraft power plant › Engine (reciprocating) › (general) › Unknown/Not determined
Pilot
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; single-engine sea; instrument: airplane
- Flight time: 3,500 hours in all; 1 in this make and model; 21 in the last 90 days; 12 in the last 30 days; 3,446 as pilot in command
- Last flight review: February 16, 2023
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: minor injuries
The aircraft
- Airframe total time: 1,470.5 hours
- Last inspection: annual inspection, November 15, 2022; 4.4 hours since
- Maximum gross weight: 4,700 lb
- Seats: 4
- Landing gear: retractable
- Engine 1: Continental TSIO-360-CB (piston); 0 hours total
- Engine 2: Continental TSIO-360-CB (piston); 103 hours total
The flight
- Departed from: BZN Bozeman MT at 12:15 pm
- Destination: BIE Beatrice NE
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 230° at 7 knots
- Visibility: 10 statute miles
- Sky: broken clouds at 22,000 ft; scat at 9,000 ft
- Temperature: 57°F (14°C), dew point 39°F (4°C)
- Altimeter: 29.88 inHg
- Observation at 7:53 am from KBIL, 11 miles away
Weather report (METAR): KBIL 031353Z 23007KT 10SM SCT090 BKN220 14/04 A2988 RMK AO2 SLP097 VIRGA S-SW CB DSNT SW ACC ALQDS T01390044
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
5 documents, released by the NTSB on May 8, 2025. 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.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Pilot 6120 | PDF, 11 pages | View Download |
| 2 | Memorandum of Record Bhanson FAA Engine Examination | PDF, 5 pages | View Download |
| 3 | Mor WPR23LA175 Tboyce Borescope Photos | PDF, 3 pages | View Download |
| 4 | Excerpt Aircraft Records | PDF, 12 pages | View Download |
| 5 | Photos | PDF, 6 pages | View Download |
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.
