N7094T

Substantial
None

KOLB FIRESTARS/N: 522

Accident Details

Date
Friday, December 11, 2020
NTSB Number
ERA21LA075
Location
Durham, NC
Event ID
20201216102419
Coordinates
36.024094, -78.716475
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A total loss of engine power due to fuel starvation as the result of a degraded fuel primer check valve.

Aircraft Information

Registration
Make
KOLB
Serial Number
522
Engine Type
2-cycle
Year Built
1994
Model / ICAO
FIRESTARFK9
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
FIRESTAR II

Registered Owner (Current)

Name
PARKHURST THOMAS G
Address
277 GEORGE WADE RD
City
GUILFORD
State / Zip Code
NY 13780-3124
Country
United States

Analysis

On December 11, 2020, about 1300 eastern daylight time, a Kolb Firestar II, N7094T, was substantially damaged when it was involved in an accident near Durham, North Carolina. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that, about 20 minutes into the flight, the engine started losing power. The airplane was about 500 ft above ground level; the engine monitoring system did not indicate an engine problem. The pilot’s attempts to increase engine power were unsuccessful, and the airplane continued to lose altitude.

The pilot decided to conduct a forced landing on a lake. During the landing flare, the wheels contacted the water surface and the airplane immediately flipped forward and came to rest upside down and partially submerged. The pilot egressed and swam to the surface, where he was rescued by an individual on a personal watercraft.

The airplane sustained substantial damage to the wings and fuselage. The tail separated about 2 ft aft of the fuel tank and the leading outboard edges of the wings were crushed and torn open. The airplane remained submerged until the following day, when it was recovered and transported to the owner’s hangar for further examination. The owner performed the examination and discovered that the fuel primer bulb was missing the fuel input primer spring. (see figure 1.)

Figure 1 - Primer bulb illustration.

The owner’s observation of the check “ball” valve and lack of spring tension kept the ball from seating properly during normal operations. The owner reported that the system should ideally be installed in a vertical position, but on the accident airplane, it was installed horizontally (see figure 2). Without the spring, gravity would not be adequate to keep the check ball from migrating inside the primer inlet fuel line.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA21LA075