CHI03LA152

NTSB accident investigation · Zimmerman Glastar · Pierce, NE · June 7, 2003

Accident · No injuriesLimited investigationFinal report
Date
June 7, 2003, 07:45 local (12:45 UTC)
Place
Pierce, NE
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N109BZZimmerman Glastar
Weather
Visual (VMC) · Day
Status
Completed · report December 30, 2003
Report
Approved by Office Director
Parties
FAA- Lincoln FSDO
FAA report
20030607030229A
Case key
57157

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

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.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionApproach - vfr pattern - downwind
Operation with known deficiencies in equipment - performedPilot in commandCause
Cooling system - overtemperatureFactor
Forced landingEmergency descent/landing
Precautionary landing - performedPilot in command
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - grassFactor
Unsuitable terrain or takeoff/landing/taxi area - selectedPilot in commandCause
Nose overLanding - roll
Landing gear,nose gear strut - collapsedFactor

Analysis

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."

Factual narrative

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.

Aircraft

Registration
N109BZ
Reported as
Zimmerman Glastar
Category
Airplane, amateur-built
Serial number
5782
Airframe hours
8.6
Engine
Subaru EJ251AXWAB-61, 165 horsepower, reciprocating
Damage
Substantial damage
Flight
Flight test · Part 91
Airworthiness certificate
Special, Experimental (Special)
Departed
PVT · Pierce, NE
Airport
PVT · Private Strip, runway 02, 2,000 × 40 ft, grass/turf

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
45
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Unknown
Last flight review
April 22, 2003
Seat
Left
Flight hours
267 total · 9 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
310° at 9 knots
Visibility
10 statute miles
Lowest ceiling
8,000 ft overcast
Temperature
55 °F, dew point 48 °F
Altimeter
29.87 inHg
Observed at
OFK, 14 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.