N4469Z

Substantial
Serious

Plante Challenger IIS/N: CH2-1007-2821

Accident Details

Date
Thursday, January 21, 2021
NTSB Number
ERA21LA109
Location
Minneola, FL
Event ID
20210121102543
Coordinates
28.626120, -81.800110
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

Failure of the engine/propeller drive belt.

Aircraft Information

Registration
Make
PLANTE
Serial Number
CH2-1007-2821
Engine Type
Reciprocating
Model / ICAO
Challenger IIMP20
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
CHALLENGER II

Registered Owner (Current)

Name
GARRETT JEFFREY L
Address
6809 SCYTHE AVE
City
ORLANDO
State / Zip Code
FL 32812-3821
Country
United States

Analysis

On January 21, 2021, about 0945 eastern standard time, an experimental amateur-built Challenger II, N4469Z, was substantially damaged when it was involved in an accident near the Florida Flying Gators Ultralight Airport (3FD4), Minneola, Florida. The student pilot/owner was seriously injured. The airplane was operating as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot stated that he was on final approach when the airplane “abruptly” turned right 45° and the flight controls no longer felt normal. He added power to go around and immediately decided it was best to make a forced landing in a field east of the airport, and reduced power. The pilot said it was a challenge to maneuver the airplane and, in an attempt, to avoid trees, the airplane stalled. It then impacted terrain, resulting in substantial damage to the fuselage and both wings.

A postaccident examination of the airplane and its two-stroke engine revealed that the belt that connected the engine output sprocket to the propeller drive sprocket was broken and laying across the empennage. Detailed examination of the belt revealed that it had a transverse fracture that intersected a tooth root at the interior side and had a more jagged transverse path through the glass reinforcement core strands, features consistent with a tensile overload failure. The edges of the belt appeared rubbed with exposed core strands in several areas consistent with lateral travel or tracking. The interior surfaces of the drive belt generally appeared free of significant wear, though fiber damage was observed on the interior surface where the tooth peaks were damaged on approximately 12 of the 120 total teeth.

The pilot purchased the airplane in October 2020. He said that the previous owner had installed the belt. The pilot estimated the belt had accrued about 70 hours when it failed.

Markings on the exterior surface of the belt indicated the belt was a PowerGrip GT3 960-8MGT-50 synchronous belt manufactured by the Gates Corporation. The Gates PowerGrip GT3 Drive Design Manual includes a “Safety Policy” for primary in-flight aircraft systems that states, “Do not use Gates belts, pulleys or sprockets on aircraft, propeller or rotor drive systems or in-flight accessory drives. Gates belt drive systems are not intended for aircraft use.”

In June 2015, the Federal Aviation Administration (FAA) issued an InFO (Information for Operators) bulletin (No. 15007), titled Gates Products Not Designed or Intended for Aircraft Use. It stated:

Operators and repair facilities should familiarize themselves with the information contained within this InFO and with Gates Catalog Aircraft Policy in order to be aware of and reduce the risk of accidents caused by belts not intended for aircraft use. However, if Gates products are used, operators and repair facilities should be aware of main drive belt breaks on aircraft utilizing a hydraulic cog belt tensioner and the proper measurement of tension when the tensioner reaches the desired parameters and also adhere to the manufacturers recommended life limits and inspection cycles.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA21LA109