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Aviation safety reports, made easier to study

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NTSB Report

March 22, 2000 · Lockwood Eagle II · N5576K

Marengo, IL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 22, 2000
Injury Outcomes
1 injury (1 serious injury)
Location
Marengo, IL
Aircraft
Lockwood Eagle II
Tail Number
N5576K
Injuries
Serious
Aircraft Damage
Destroyed
NTSB Number
CHI00LA093

The aerobatic airplane impacted terrain following departure from a private grass strip. The left wing was separated from the airplane and the left horizontal stabilizer was destroyed. The propeller displayed bending and twisting with rotational scratching on the spinner. There were no mechanical anomalies with the airplane.

NTSB Probable Cause

The pilot's failure to maintain aircraft control.

Full Narrative

On March 22, 2000, at 0955 central standard time, a Lockwood Christen Eagle II, N5576K, owned and piloted by an airline transport pilot, was destroyed on impact with terrain after takeoff from runway 27 (2,600 feet by 130 feet, grass) at the Walpole private airstrip, located approximately 3 miles south-southwest of Marengo, Illinois. Visual meteorological conditions prevailed at the time of the accident. The pilot received serious injuries. The 14 CFR Part 91 personal flight was not operating on a flight plan. The local flight was originating at the time of the accident. The pilot stated that he topped the fuel off on November 22, 1999, and last flew the airplane on December 23, 1999 for 25 minutes after which he did not refuel the airplane. Prior to the accident flight, he checked the fuel and stated that it was 3 inches down from the top or 20 gallons. He also stated that he had no memory of the entire flight. Fuel records provided by the owner of the airstrip indicate that the airplane was last fueled on November 22, 1999, with 12.3 gallons. The wreckage was approximately 450 feet south of the airstrip. A northeasterly ground scar of approximately 225 feet contained a section of the left wing and landing gear strut. The left horizontal stabilizer was deformed upward and parallel with the side of the fuselage. The right wing was attached to the fuselage and the right horizontal stabilizer was in its horizontal position. The propeller was separated from the engine and exhibited twisting and curling. The spinner exhibited scratching in the rotational direction. The mechanical wobble pump was operated and a liquid consistent with aviation fuel was expelled from the pump. The crankshaft was rotated and air was expelled from each cylinder. Engine continuity was established. Flight control continuity was established to the flight controls. The Federal Aviation Administration and Textron Lycoming were parties to the investigation.

Flight

Event TypeAccident
Event Time09:55 CST
Nearest AirportWALPOLE (0nm S)
Runway27
Runway Length2600 ft
Runway Width130 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftLockwood Eagle II
Tail NumberN5576K
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO360-A1D · Reciprocating · 200
Seats2

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 67 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind250° @ 3 kt
Visibility9 sm
CeilingOvercast 2000 ft
Temperature / Dew Point52 / 43 C
Altimeter30.00 inHg
Observation Time15:54
Weather SourceWFAC

Appendix: Source Data