NTSB CAROL · Event
Event CHI01LA277
Registry · N9297Z
FAA Aircraft Registry record.
Make / Model
BUCKEYE DREAM MACHINE
Engine
ROTAX 503 SERIES (52 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20071206
ADS-B equipped
Yes — Mode-S ACE2FE
Registrant of record
YODER CALVIN J
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Ground crew personnel improperly connected the tow winch cable prior to takeoff which resulted in one side of the winch cable coming disconnected. Factors associated with the accident were the ditch and the tree branch which the airplane contacted.
Factual narrative
On August 4, 2001, at 1500 eastern daylight time, a Blanik L-13 glider, N9297Z, collided with a tree during an initial takeoff run at the Marlette Township Airport, Marlette, Michigan. The certified flight instructor (CFI) received a serious injury and the student pilot was not injured. The glider received minor damage. The 14 CFR Part 91 instructional flight was operating in visual meteorological conditions without a flight plan. The local flight was originating when the accident occurred. The CFI reported, "The slack out - go - signal was given from the operations trailer and take-off power was applied to the winch, whereupon the left hook of the winch harness released, uncommanded, from the center of gravity attachment. The uneven force caused the glider to yaw to the left and head for the ditch on the west side of the runway. I applied right aileron and full right rudder, but was unable to keep the glider from floating into the ditch." The CFI reported the glider ended up bridging the ditch on a heading of east. He reported that the ditch was full of broken and cut down brush and saplings. During the impact, a broken branch penetrated the left side of the cockpit and impaled itself in the CFI's right calf. The CFI remained hospitalized for five days following the accident. Members of the glider club reported that they had hooked both the left and right side cables prior to the takeoff. Inspection of the tow winch by an inspector from the Federal Aviation Administration Detroit Flight Standards District Office failed to reveal any mechanical failure/malfunction. The CFI reported that during the takeoff the left hook of the winch harness released, uncommanded, from the center of gravity attachment. The glider yawed to the left toward a ditch on the west side of the runway. The CFI applied right aileron and full right rudder in an attempt to avoid the ditch however the glider continued into the ditch. The glider came to rest bridging the ditch on a heading of east. He reported that the ditch was full of broken and cut down brush and saplings. During the impact, a broken branch penetrated the left side of the cockpit and impaled itself in the CFI's right calf. The CFI remained hospitalized for five days following the accident. Members of the glider club reported that they had hooked both the left and right side cables prior to the takeoff. Inspection of the tow winch failed to reveal any mechanical failure/malfunction. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_CHI01LA277.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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