Aviation Crash Map

Schumacher CHALLENGER II N441MS

21 June 2014 · St. Joesph, Illinois, United States · No injuries

Summary

On 21 June 2014 at about 00:35 local time, a Schumacher CHALLENGER II registered N441MS was involved in an accident near St. Joesph, Illinois, United States. 2 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 00:35
Classification
Accident
Location
St. Joesph, Illinois, United States
Coordinates
40.0792, -88.0572
Aircraft
Schumacher CHALLENGER II
Registration
N441MS
Category
Airplane
Year built
2004
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Sidney → Sidney
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
CEN14LA309

People

Nobody was injured.

On board Died Serious Minor Uninjured
2 0 0 0 2

Probable cause

The total loss of engine power due to a lack of lubrication following the in-flight failure of the mechanical oil injection pump. Contributing to the accident was the temporary obscuration of the pilot's forward visibility due to sun glare during the forced landing, which resulted in a collision with power lines.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot reported that, during cruise flight about 1,200 ft mean sea level, the engine experienced a sudden and total loss of power. He was unsuccessful in reestablishing engine power and selected a nearby soybean field for a forced landing. The pilot stated that, as he maneuvered the airplane toward the field, the setting sun temporarily obstructed his forward visibility. The airplane subsequently collided with power lines and then entered an aerodynamic stall and impacted terrain. A postaccident engine examination revealed scoring and a lack of proper oil lubrication of the forward cylinder piston adjacent to the intake and exhaust ports. The rear cylinder piston did not exhibit scoring; however, evidence of oil starvation was observed. Further examination of the oil system revealed that the mechanical oil injection pump had seized within its housing. Additionally, the oil pump nylon drive-coupling had fractured. The oil pump was a nonserviceable component that prevented further disassembly. The pilot reported that the experimental engine was not originally equipped with a mechanical oil injection pump and that he had the engine modified with the oil pump about 50 hours before the accident. The total loss of engine power during the accident flight was due to a cylinder seizure, which resulted from a lack of lubrication following the failure of the mechanical oil injection pump.

Quoted verbatim from the NTSB record.

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