N519SP

Substantial
Serious

STEPHEN D PHILLABAUM HELICYCLES/N: 5-19

Accident Details

Date
Sunday, October 1, 2023
NTSB Number
WPR24LA009
Location
Deer Park, WA
Event ID
20231010193215
Coordinates
47.894536, -117.439800
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A loss of engine power due to fuel starvation resulting from contamination of the fuel system during low-level flight.

Aircraft Information

Registration
Make
STEPHEN D PHILLABAUM
Serial Number
5-19
Engine Type
Turbo-shaft
Year Built
2018
Model / ICAO
HELICYCLEFK9
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
1
FAA Model
HELICYCLE

Registered Owner (Current)

Name
PHILLABAUM STEPHEN D
Address
2121 W DENISON RD
City
DEER PARK
State / Zip Code
WA 99006-9333
Country
United States

Analysis

On October 1, 2023, about 1320 Pacific daylight time, an experimental amateur-built Helicycle, N519SP, was substantially damaged when it was involved in an accident near Dear Park, Washington. The pilot was seriously injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he had not flown helicopter in over 3 months, and he performed several practice liftoffs to a hover and landings before departing to the northeast to fly a modified airport traffic pattern. He continued his left turn to the west with the intent of terminating the approach to a hover. The pilot reported that during the left turn and about 50 ft agl he “added power to increase airspeed and altitude” when the engine lost power. He lowered the collective, rolled out of the turn and attempted to arrest the descent, but the helicopter landed hard, resulting in substantial damage to the tailrotor driveshaft and tailrotor gearbox. NTSB investigators did not travel to the accident site.

Postaccident examination of the helicopter’s fuel system, showed that the experimental amateur-built helicopter was equipped with three polypropylene fuel tanks. The main fuel tank was fabricated with a vent and two fuel lines at the base of the tank; one fuel line at the left base fed into a fuel tank on the left side of the helicopter, and one fuel line on the right base of the tank fed into a fuel tank on the right side of the helicopter. The left and right side fuel tanks were equipped with fuel quantity indicators, and a cross-feed fitting that fed into the fuel filter. The anodized aluminum fuel filter was intact, disassembled, and revealed an observable quantity of foreign particulates inside the body of the filter, as well as the inflow orifice.

The left and right fuel tanks contained dirt-like debris, which was also found in the cross-feed outflow fuel fitting to the fuel filter input. The main fuel tank revealed hardened pieces of sealant affixed to arbitrary locations at the base of the tank. The pieces of sealant were too large to flow through the fuel lines into the subsequent left and right fuel tanks.

The gascolator, filter screen, O-rings, and rubber seal were intact. However, an observable quantity of dirt-like debris was trapped inside the gascolator and staining was observed inside the fuel bowl. The fuel control assembly was affixed to the fuel pump, securely mated to the accessory case, and appeared unremarkable.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR24LA009