Aviation Crash Map

Phantom Aeronautics X-1 N111JC

4 September 2019 · Van Wert, Ohio, United States · No injuries

Summary

On 4 September 2019 at about 21:35 local time, a Phantom Aeronautics X-1 registered N111JC was involved in an accident near Van Wert, Ohio, United States. One person was 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 21:35
Classification
Accident
Location
Van Wert, Ohio, United States
Nearest airport
Van Wert County (VNW)
Coordinates
40.8817, -84.6442
Aircraft
Phantom Aeronautics X-1
Registration
N111JC
Category
Airplane
Year built
1994
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Van Wert → Van Wert
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
CEN19LA303

People

Nobody was injured.

On board Died Serious Minor Uninjured
1 0 0 0 1

Probable cause

A loss of engine power due to the separation of the carburetor from the intake socket resulting from the improper installation of the intake silencer.

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

Read the full NTSB narrative

The pilot reported that the engine lost power during cruise flight. While troubleshooting, he noticed that the forward carburetor of the dual-carburetor-equipped engine had separated from the intake socket. He subsequently performed a forced landing to a field, during which the left wing spar was substantially damaged. A postaccident examination revealed that the forward intake socket did not conform to an exemplar socket provided by the engine manufacturer. In addition, the intake silencer was not supported except by the carburetors. Maintenance records indicated that the intake silencer was installed before the current owner purchased the airplane. A daily inspection checklist provided by the engine manufacturer included inspection of the sockets and silencer. The in-flight separation of the forward carburetor from the intake socket was likely the result of the improper intake silencer installation, which lacked support other than the forward and aft carburetor intake sockets.

Quoted verbatim from the NTSB record.

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