ERA23LA360

NTSB accident investigation · Brown Benjamin C Challenger II · Moultonborough, NH · September 1, 2023

Accident · No injuriesClass 3 · LimitedFinal report
Date
September 1, 2023, 09:10 local (13:10 UTC)
Place
Moultonborough, NH
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N2480YBrown Benjamin C Challenger II
Defining event
Takeoff: Loss of engine power (total)
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 3
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20230901015639A
Case key
192999

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

On this page

Probable cause

A loss of engine power due to a loss of compression in one of the engine’s two cylinders.

Findings · 3

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.

Engine fuel and controlAircraft › Aircraft power plant · Incorrect service/maintenanceBrown Benjamin C CHALLENGER II: 1 caseAll aircraft: 49 casesProbable cause
AircraftAircraft › Aircraft power plant · FailureBrown Benjamin C CHALLENGER II: 1 caseAll aircraft: 151 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 reported that a few minutes after takeoff, during the initial climb, the airplane’s two-stroke engine began to slowly lose power. The pilot attempted to restart the engine but was unsuccessful. He elected to make a forced landing in small field, resulting in substantial damage to both of the airplane’s wing struts. Postaccident examination of the engine revealed that one of the engine’s two cylinders had no compression. It is likely that this lack of compression resulted in the loss of engine power reported by the pilot during the accident flight. Additionally, during the examination, a zip tie was found secured around the fuel line that provided fuel for that cylinder in a way that reduced its interior diameter. It is possible that the reduced diameter of the fuel line could have resulted in less fuel reaching the cylinder during high power operation, and that it was operating in an excessively lean condition. Operation in this state could have damaged the cylinder and resulted in the lack of compression observed during the engine examination. It could not be determined when the zip-tie was installed on the fuel line, though entries in the airplane’s maintenance logs indicated that its last condition inspection was completed about three months before the accident.

Factual narrative

On September 1, 2023, at 0910 eastern daylight time, an experimental amateur-built Challenger II, N2480Y, was substantially damaged when it was involved in an accident near Moultonborough, New Hampshire. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot, during takeoff and initial climb, the engine was producing full power without anomalies. Then, while still in the climb, the engine gradually sustained a total loss of power. The pilot attempted to make two engine restarts but was unsuccessful. The pilot performed a forced landing in a field, resulting in substantial damage to both left and right wing struts. A postaccident examination of the two-cylinder, two-stroke engine found that the airplane contained between 7 and 10 gallons of fuel with no contamination. There was evidence of spark from all of the ignition leads, and all four spark plugs were gapped within recommended specifications. The engine’s crankshaft rotated when force was applied to the propeller with no discrepancies noted. The engine contained adequate oil. The cylinders were checked for compression and the cylinder closest to the magneto had no compression. A fuel line leading to the cylinder was found with a zip-tie secured to it that reduced the interior circumference of the fuel line. According to the airplane’s maintenance logbooks, the fuel lines were installed in March 2013 and inspected in June 2019. A condition inspection of the engine was completed in June 2023, with a total time of 564.7 hours. It is unknown when the zip-tie was placed around the fuel line.

Aircraft

Registration
N2480Y
Reported as
Brown Benjamin C Challenger II
Category
Airplane, amateur-built
Serial number
CH20394-4139
Built
1996
Engine
Rotax 503 DCI, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental light sport (Special)
Airport
4MB · Moultonborough

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
74
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3
Flight hours
410 total · 0 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
220° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
57 °F, dew point 52 °F
Altimeter
30.29 inHg
Observed at
LCI, 11 nm away
METAR
KLCI 011256Z AUTO 22005KT 10SM CLR 14/11 A3029 RMK AO2 SLP255 T01440106

Docket · 4

The files NTSB released with the investigation on April 1, 2025, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.6 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.