NTSB CAROL · Event
Event ATL95LA069
Registry · N19PF
FAA Aircraft Registry record.
Make / Model
CESSNA 177B
Year of manufacture
1972 · 23 years old at event
Engine
LYCOMING O-360-A1F6 (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20200728
ADS-B equipped
Yes — Mode-S A1671D
Registrant of record
TAC'S ENTERPRISE LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S POORLY PLANNED APPROACH WHICH RESULTED IN THE LOSS OF CONTROL OF THE AIRCRAFT BECAUSE OF GUSTY WIND CONDITIONS.
Factual narrative
On March 23, 1995, about 1520 eastern standard time, an Aero Tek Zuni, N19PF, collided with the ground during an approach to the Morganton-Lenoir Airport, Morganton, North Carolina. The glider was operated under the provisions of 14 CFR Part 91, and visual flight rules. A flight plan was not filed for the local personal flight. The private pilot had minor injuries, and the glider was substantially damaged. Origination of the flight was Morganton, about 1430, on the same day. According to a sailplane instructor who witnessed the accident, the glider began the turn from downwind to base during the approach to runway 21. He stated that the airspeed was approximately 60 knots, but should have been much higher, considering the gusty wind conditions at the time of the accident. As he watched, the bank angle increased to approximately 60 to 70 degrees and the nose of the glider fell to an almost vertical position. The glider then disappeared from his view behind some trees. The glider subsequently impacted trees and the ground. The pilot stated that, while turning base to final at approximately 350 feet, the glider hit a windshear. As a result of the windshear, the glider lost altitude and airspeed and the right wing was lifted. The pilot reported that the glider was blown from the intended course to land on runway 21 to above the trees to the east of the runway. The pilot reported moderate turbulence. A mountain wave soaring event was underway at the Morganton-Lenoir Airport. Wind conditions were reported to be strong and gusty, 15 knots with gusts to 25 knots. The glider was turning into a headwind as it made the turn onto the left base for runway 21. An inspection of the aircraft revealed no indication of a mechanical failure. The right wing was located about 30 yard from the main wreckage. The marks on the wing revealed that it broke off when the glider first impacted the trees. The left wing and empennage were separated but located with the fuselage. THE GLIDER IMPACTED THE TREES TO THE EAST OF THE AIRPORT DURING AN APPROACH TO RUNWAY 21. THE PILOT REPORTED THAT THE GLIDER HIT WINDSHEAR. AS A RESULT OF THE WINDSHEAR, THE GLIDER WAS IN A 60 TO 70 DEGREE BANK TO THE RIGHT AND THE GLIDER HAD LOST AIRSPEED AND ALTITUDE. A SAILPLANE INSTRUCTOR WHO WITNESSED THE ACCIDENT STATED THAT THE AIRSPEED WAS APPROXIMATELY 60 KNOTS BUT SHOULD HAVE BEEN MUCH HIGHER CONSIDERING THE GUSTY WIND CONDITIONS AT THE TIME OF THE ACCIDENT. AN INSPECTION OF THE GLIDER REVEALED NO INDICATIONS OF A MECHANICAL FAILURE. THE PILOT REPORTED MODERATE TURBULENCE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_ATL95LA069.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (loss of control, turbulence). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2026 · arXiv preprint
Direct Numerical Simulations of Ice-Ocean Boundary Turbulence
Turbulent heat and freshwater transport at ice-ocean interfaces controls glacier and iceberg melt rates, yet the underlying physics remains poorly constrained.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
Political Turbulence and Aviation Safety: A Cross-National Analysis of Political Stability's Effects on Aviation Accidents
To what extent does political stability affect aviation safety? This research aims to link domestic political conditions and public safety through the consideration of aviation accident frequency.
- arXiv 2025 · arXiv preprint
Explainable LiDAR 3D Point Cloud Segmentation and Clustering for Detecting Airplane-Generated Wind Turbulence
Wake vortices - strong, coherent air turbulences created by aircraft - pose a significant risk to aviation safety and therefore require accurate and reliable detection methods.
- arXiv 2024 · arXiv preprint
Does small-scale turbulence matter for ice growth in mixed-phase clouds?
Representing the glaciation of mixed-phase clouds in terms of the Wegener-Bergeron-Findeisen process is a challenge for many weather and climate models, which tend to overestimate this process because…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
Browse the full corpus — academia portal ↗