- Date
- August 21, 2023, 10:48 local (15:48 UTC)
- Place
- Durant, OK
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Enroute
- Aircraft
- N3589XPiper PA31
- Defining event
- Enroute: Powerplant sys/comp malf/fail
- Weather
- Visual (VMC) · Day
- Status
- Completed
- Report
- Approved by Office Director
- Investigation class
- Class 3
- NTSB office
- Central Region
- Parties
- FAA FSDO
- FAA report
- 20230821012859A
- Case key
- 192908
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The loosening of a connecting rod cap nut for reasons that could not be determined, which resulted in a mechanical failure of the engine and an in-flight fire.
Findings · 1
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
While in flight, the pilot heard and felt a bang from the right side of the airplane. He saw that the right engine nacelle had a hole in it and the engine was on fire. He secured the engine and diverted to a nearby airport. While on final approach for landing, the engine fire reignited. The pilot landed the airplane, taxied clear of the runway, shut down the left engine, and egressed. The engine fire continued to burn and consumed the right engine and a majority of the fuselage. Examination revealed that the right engine’s No. 2 cylinder was displaced from the engine case but remained attached via the injector manifold vent tube and injector lines. All eight of the No. 2 cylinder’s attach bolts were broken off at the case. The connecting rod cap was found lodged in the bottom of the piston. One connecting rod bolt was found broken off flush in the connecting rod; the top portion was not located. The other connecting rod bolt remained in the connecting rod cap with the nut also not located. One side of the lower connecting rod flange was bent back towards the piston, capturing the nut and remaining portion of the broken bolt. Neither bearing half could be identified in the remaining material. Numerous impact marks were noted on the piston, cylinder, and case. A review of maintenance records found that the engine was last overhauled about 4 ½ years before the accident and had accrued about 900 hours since the overhaul. Based on the available information, it is likely that the nut that secured one side of the connecting rod cap became loose, resulting the separation of the cap and subsequent damage to the No. 2 cylinder. Since the nut could not be located, the reason it did not remain secure could not be determined.
Factual narrative
On August 21, 2023, about 1048 central daylight time, a Piper PA-31-350 airplane, N3589X, was substantially damaged when it was involved in an accident near Durant, Oklahoma. The pilot was not injured. The airplane was operated under Title 14 Code of Federal Regulations Part 91 as an aerial observation flight. The pilot reported that, while in flight, he heard and felt a bang from the right side of the airplane. He saw that the right engine nacelle had a hole in it and the engine was on fire. He then shut down and secured the engine, which appeared to stop the engine fire, and diverted to a nearby airport. While on final approach for landing, the engine fire reignited. The pilot landed the airplane, taxied clear of the runway, shut down the left engine, and egressed. The engine fire continued to burn and consumed the right engine and a majority of the fuselage. An engine examination revealed that the No. 2 cylinder was displaced from the engine case but remained attached via the injector manifold vent tube and injector lines. All eight of the No. 2 cylinder’s attach bolts were broken off at the case. The connecting rod cap was found lodged in the bottom of the piston. One connecting rod bolt was found broken off flush in the connecting rod; the top portion was not located. The other connecting rod bolt remained in the connecting rod cap with the nut also not located. One side of the lower connecting rod flange was bent back towards the piston, capturing the nut and remaining portion of the broken bolt. Neither bearing half was identified. Numerous impact marks were noted on the piston, cylinder, and case. A review of maintenance records found that the engine was last overhauled on March 20, 2019, and installed on the airplane on October 1, 2020. The airplane had accrued about 900 hours since the overhaul.
Aircraft
- Registration
- N3589X
- Reported as
- Piper PA31 (350)
- Category
- Airplane
- Serial number
- 31-8052138
- Built
- 1980
- Airframe hours
- 22,698.4
- Engines
- Lycoming TSIO-540, 350 horsepower, reciprocatingLycoming TSIO-540, 350 horsepower, reciprocating
- Damage
- Substantial damage
- Fire
- Both
- Flight
- Aerial observation · Part 91
- Operator
- Marc Inc
- Registered owner
- Marc Inc
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · August 11, 2022
- Departed
- KRVS · Tulsa, OK
- Destination
- KDUA · Durant, OK
- Airport
- DUA · Durant Rgnl/Eaker Fld, runway 17, 6,800 × 100 ft, asphalt
- Equipment
- ADS-B
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 36
- Injuries
- None
- Certificate
- Commercial
- Airplane ratings
- Multi-engine land, Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 1, Without waivers/limitations
- Last flight review
- October 7, 2022
- Seat
- Left
- Flight hours
- 3,300 total · 1,400 in this make and model · 3,189 as pilot in command · 130 in the last 90 days · 49 in the last 30 days · 9 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 100° at 7 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 93 °F, dew point 66 °F
- Altimeter
- 30.12 inHg
- Observed at
- KDUA
- METAR
- KDUA 211535Z AUTO 10007KT 10SM CLR 34/19 A3012 RMK AO2
Docket · 5
The files NTSB released with the investigation on May 9, 2024, on NTSB’s docket system: statements, records, photos and specialists’ reports. 52.6 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.