NTSB CAROL · Event
Event CHI97LA247
Registry · N5066X
FAA Aircraft Registry record.
Make / Model
CHAMPION 7KCAB
Year of manufacture
1968 · 29 years old at event
Engine
LYCOMING IO-320 SERIES (150 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19681211
ADS-B equipped
Yes — Mode-S A6537A
Registrant of record
CHANDELLE LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain directional control of the airplane during landing, and his excessive use of brakes, which resulted in a nose over. Factors relating to the accident were: the crosswind condition, and the pilot's lack of experience in the make and model of airplane.
Factual narrative
On August 5, 1997, at 1355 central daylight time (cdt), a Champion 7KCAB, N5066X, operated by a private pilot, sustained substantial damage when on landing, control of the airplane was lost. The airplane subsequently nosed over coming to rest on its back. Visual meteorological conditions prevailed at the time of the accident. The aerial towing flight was being conducted under 14 CFR Part 91. No flight plan was on file. The pilot reported no injuries. The local flight originated at Hampshire, Illinois, at 1345 cdt. In his written statement, the pilot said that he was landing after towing and releasing a glider. "I landed to the west, runway 27, on the Sky Soaring [airport] grass strip and was slowing down to a speed at which the rudder had lost effectiveness. The airplane started a slight ground loop toward the right (north), which I corrected by use of the left heel brake. But, the airplane was still headed 15 to 20 degrees right of the runway centerline, toward a glider tied down on the north side of the field. I stepped on both heel brakes to stop the forward movement, and the airplane nosed over and ended on its back." The Federal Aviation Administration (FAA) inspector who examined the airplane, found the right wing broken at the wing root. The right wing tip was crushed in and aft. Both wing struts were bent inward. The engine cowling was bent upward and broken open. The engine and engine mounts were bent up and aft. One of the two propeller blade was bent aft at the tip. The spinner was crushed inward. The windscreen was cracked and pushed inward. The top of the rudder was crushed inward slightly. Flight control continuity was confirmed. No anomalies were found with the engine, engine controls, brakes or any other airplane system. The pilot was landing after towing and releasing a glider. The wind was from 020 degrees at 7 knots. The pilot said, 'I landed to the west, runway 27, on the Sky Soaring [airport] grass strip and was slowing down to a speed at which the rudder had lost effectiveness. The airplane started a slight ground loop toward the right (north), which I corrected by use of the left heel brake. But, the airplane was still headed 15 to 20 degrees right of the runway centerline, toward a glider tied down on the north side of the field. I stepped on both heel brakes to stop the forward movement, and the airplane nosed over and ended on its back.' Examination of the wreckage revealed no anomalies. The pilot had only about 7 hours in this make and model of airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_CHI97LA247.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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