N7094T is a 1994 Kolb FIRESTAR II. It is a fixed-wing single-engine aircraft with 2 seats, powered by a Rotax 503 DCDI rated at 52 horsepower. The registration is active, with the registrant based in Guilford, NY. Its experimental airworthiness certificate was issued in Nov 2007. It has been registered to its current owner since Aug 2021. This page also carries 1 NTSB event.
- 32 years old
- Only 8 Kolb FIRESTAR II here
2021
2007
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N7094T's record changes.
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.
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