AIR TRACTOR INC AT 301 near Pearsall, TX — 2014-06-12
- Date
- 2014-06-12
- Location
- Pearsall, TX, USA
- Aircraft
- AIR TRACTOR INC AT 301
- Registration
- N8593S
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Initial climb
Probable cause
The failure of the No. 1 cylinder rod at the link pin. Contributing to the accident was oil starvation to the rod bearing due to the improper flushing of the oil cooler, which allowed metal and other debris in the oil to clog the drain and the led to the piston’s failure.
NTSB narrative
The pilot reported that, while returning to the airport after spraying a cornfield, he noticed that the engine cylinder head temperature was high. After landing, he checked the engine cylinders for discrepancies and found none, so he decided to continue the spraying operations at the cornfield. As the pilot pulled up the airplane from a spray run, the engine started to vibrate and lose power. He subsequently made a forced landing in a nearby field, which resulted in the airplane sustaining substantial damage to both wings. During postaccident examination, a considerable amount of metal was found in the oil drain. The No. 2 cylinder front spark plug was loose. After removing all of the spark plugs, an attempt was made to rotate the engine, but it seized. After removing the No. 1 cylinder, it was discovered that the piston rod had broken at the link pin; no other rods were broken. The No. 1 cylinder link pin was scored, and there was evidence of oil starvation at the rod bearing. According to the operator, the engine had accrued about 100 hours since it had received extensive maintenance, including the replacement of the crankshaft. It is likely that the oil cooler was not properly flushed when the crankshaft was replaced and that metal and other debris remained in the oil, clogged the drain, and caused the piston to fail.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot could have opted not to continue spraying after high cylinder head temperature.
NTSB coding
Evidence available
- Photos
- 7 docket documents
Docket documents7
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- E-Mail from Troy Fieldsother
- Photo 1 – N8593 sitting on blocks after it was recovered from the accident sitephotos
- Photo 2 – A close-up view of the engine and propeller. Note the lower propeller blade is bent aft 90 degreesphotos
- Photo 3 – Removal of the no. 1 cylinder head revealed a broken connecting rod. Note the damage to the cylinder skirtphotos
- Photo 4 - Further disassembly revealed the upper segment of the connecting rod still attached to the wrist pinphotos
- Addendum to NTSB Accident Reportreport
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