Pierce, NE, USA
N109BZ
Zimmerman Glastar
The airplane nosed over during a precautionary landing to a meadow near a grass airstrip. The pilot reported he entered the downwind leg and the engine temperature rose to 260 degrees Fahrenheit. The pilot stated he "had a choice [to] continue around the pattern with an overheating engine, or land immediately." The pilot decided to land the airplane in a grass meadow rather than on the mowed grass airstrip. During landing rollout, the nose gear subsequently became stuck in the grass and nosed over. The airplane had 8.6 hours of total flight hours since receiving a FAA airworthiness certificate. The pilot noted he had experienced problems with the engine cooling system prior to the accident flight. Engine and control surface continuity was confirmed. The reason for the high engine temperature was not determined. The pilot stated, "In hindsight, I wish I wouldn't have flown with a questionable engine."
On June 7, 2003, at 0745 central daylight time, an amateur-built Glastar, N109BZ, piloted by a private pilot, sustained substantial damage when it nosed over during a precautionary landing near Pierce, Nebraska. Visual meteorological conditions prevailed at the time of the accident. The personal flight was operating under the provisions of 14 CFR Part 91 without a flight plan. The pilot was uninjured. The local flight departed at 0720. The purpose of the flight was to test the airplane's engine in the traffic pattern. The pilot reported he entered the downwind leg and the engine temperature rose to 260 degrees Fahrenheit (F). The pilot stated he "had a choice [to] continue around the pattern with an overheating engine, or land immediately directly into a 15 [mile per hour] headwind, in a flat meadow [with] 12 inch tall grass." The pilot reported he chose to land in the meadow rather than continue on downwind and land on the mowed grass airstrip. The pilot reported the nose gear became stuck in the tall grass during landing rollout and the aircraft nosed over. The pilot reported the airplane had flown a total of 8.6 hours since receiving an Federal Aviation Administration (FAA) airworthiness certificate. He reported he had experienced trouble with the engine cooling system on previous flights. The pilot stated the engine's maximum temperature is 230 degrees F. The pilot indicated he had experienced engine temperatures between 250 and 260 degrees F while at low airspeeds, idling, or during taxi tests. The pilot stated, "In hindsight, I wish I wouldn't have flown with a questionable engine, but I figured I had to get [the airplane] in the air and get more air going through the radiators to test [the engine's] cooling abilities." A FAA airworthiness inspector conducted an on-scene inspection of the airplane. The inspection revealed engine and control surface continuity. The inspection of the engine cooling system did not reveal the reason for the high engine temperatures.
The pilot's operation of the airplane with known deficiencies in equipment and his selection of unsuitable terrain for landing. Factors contributing to this accident were the overtemperature of the engine cooling system, the long grass, and the collapse of the nose landing gear strut.
Source: NTSB Aviation Accident Database
Aviation Accidents App
In-Depth Access to Aviation Accident Reports
