CEN26LA131

NTSB accident investigation · Quad City Challenger · Van Burensburg, IL · February 28, 2026

Accident · No injuriesClass 4 · LimitedFinal report
Date
February 28, 2026, 16:00 local (22:00 UTC)
Place
Van Burensburg, IL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
UNREGQuad City Challenger
Defining event
Enroute: Part(s) separation from AC
Weather
Visual (VMC) · Day
Status
Completed · report May 7, 2026
Report
Approved by Office Director
Investigation class
Class 4 - Basic report with no Prelim publish
NTSB office
Central Region
Parties
FAA - Springfield FSDO
Case key
202584

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

Propeller separation due to failure of the propeller attachment bolts.

Findings · 2

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.

AircraftAircraft › Aircraft structures · FailureAll aircraft: 72 casesProbable cause
Misc hardware: fastenersAircraft › Fluids/misc hardware · Not specifiedAll aircraft: 58 casesProbable cause

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

The pilot/owner reported that during straight and level flight, he felt a “shudder” and heard a “thump” and the airplane’s engine over sped. He executed a forced landing to a field, but the airplane’s right main landing gear separated from the airplane. The airplane came to rest on the remaining landing gear and the right wing. Postaccident examination revealed that the airplane’s pusher propeller had separated from the engine. During the separation, the propeller struck the left wing, tearing the fabric covering and substantially damaging internal structure. The forced landing resulted in substantial damage to the fuselage lower longerons. Photographic evidence supplied by the pilot showed that the threaded portion of the 6 bolts that retained the propeller were still in the engine propeller hub. The propeller and the unthreaded portion of the propeller bolts were not recovered. The pilot reported that other than the propeller separation, there were no preexisting mechanical problems with the airplane. He noted that the accident could have been prevented by performing a better inspection under the propeller hub, noting that the propeller bolts are not visible during daily inspections. The airplane was not registered, and the pilot did not hold a Federal Aviation Administration issued pilot certificate. He reported that he thought the operation of the airplane was covered under Title 14 Code of Federal Regulations (CFR) Part 103 – Ultralight Vehicles. 14 CFR 103 details the operation of ultralight vehicles that do not require a pilot certificate, a medical certificate, or registration of the vehicle. The vehicle requirements include an empty weight of less than 254 pounds, a fuel capacity not exceeding 5 gallons, a maximum level flight speed of 55 kts., and a stall speed of no more than 24 kts. Although the airplane was not weighed following the accident, research indicated that the accident airplane may have achieved all the requirements, except the fuel limitation. The accident airplane was equipped with a 10-gallon fuel tank. As such, the airplane should have been registered, and the pilot should have been certificated.

Aircraft

Registration
UNREG
Reported as
Quad City Challenger
Category
Airplane, amateur-built
Serial number
NA
Built
1994
Engine
Hirth 3202, 55 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
None
Departed
VLA · Vandalia, IL
Equipment
Unknown

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
74
Injuries
None
Seat
Single
Restraint
3-point
Flight hours
2,000 total · 1,500 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
9,500 ft overcast
Temperature
59 °F, dew point 27 °F
Altimeter
30.01 inHg
Observed at
KTAZ, 30 nm away
METAR
METAR KTAZ 282155Z AUTO 00000KT 10SM OVC095 15/M03 A3001 RMK AO2 T01471032 PWINO=