Aviation Crash Map

Cessna U206G N891LL

25 August 2016 · Cave-In-Rock, Illinois, United States · Serious injuries

Summary

On 25 August 2016 at about 15:05 local time, a Cessna U206G registered N891LL, operated by State of Illinois, was involved in an accident near Cave-In-Rock, Illinois, United States. 2 people were on board and one was seriously injured, one had minor injuries. 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 15:05
Classification
Accident
Location
Cave-In-Rock, Illinois, United States
Coordinates
37.4775, -88.2144
Aircraft
Cessna U206G
Registration
N891LL
Category
Airplane
Year built
1986
Engines
1
Operator
State of Illinois
Operating rule
Public Use
Phase of flight
Not recorded
Route
Springfield → Springfield
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
CEN16LA335

People

1 person was seriously injured.

On board Died Serious Minor Uninjured
2 0 1 1 0

Probable cause

A total loss of engine power due to air entering the fuel system for reasons that could not be determined based on available information. Contributing to the accident was the pilot’s inability to restart the engine due to the check valve assembly design.

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

Read the full NTSB narrative

The airline transport pilot and camera operator were conducting an aerial mapping flight. While level at 3,500 ft above ground level, the turbo propeller-equipped airplane experienced a total loss of engine power. The pilot attempted to restart the engine three times without success. During the subsequent forced landing, the airplane struck a berm, which damaged both wings. Examination of the engine revealed that fuel would not flow to the fuel nozzle until air pressure was bled upstream of the check valve assembly, located between the engine fuel control and the fuel nozzle. After the air pressure was bled and the fuel pump purged, normal fuel flow resumed, indicating that air had entered the fuel system. Because of the check valve assembly design, an in-flight engine restart was not possible after air entered the fuel line, and there was no procedure to clear air from the fuel line while in flight. Examination of the engine and fuel system could not establish a reason for air entering the fuel line.

Quoted verbatim from the NTSB record.

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All 134 records for this type

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