NTSB CAROL · Event
Event NYC83LA007
Registry · N50BS
FAA Aircraft Registry record.
Make / Model
GLOBE GC-1B
Year of manufacture
1946 · 36 years old at event
Engine
CONT MOTOR C145 SERIES (145 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19561016
ADS-B equipped
Yes — Mode-S A637C1
Registrant of record
SUGIONO YUDI S
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
DURING TAKEOFF, THE RIGHT SIDE OF THE CANOPY SEPARATED FROM THE AIRCRAFT AS IT WAS CLIMBING THROUGH ABOUT 150 TO 200 FT AGL. THE PILOT NOTIFIED THE TOWER OF THE SITUATION AND CLEARANCE WAS OBTAINED TO LAND ON ANY RUNWAY. ACCORDING TO THE PILOT, HE TURNED CROSSWIND TOO SOON AND BEGAN A DOWNWIND TOO CLOSE-IN WHILE AVOIDING GLIDER OPERATIONS. SUBSEQUENTLY, HE BEGAN A TIGHT 180 DEGREE TURN FROM A LOW DOWNWIND TO FINAL APPROACH. THE PILOT REPORTED THAT DURING THE TURN, THE AIRCRAFT "BEGAN TO FALL OUT OF THE SKY." HE ADDED FULL POWER AND STATED THAT PARTIAL CONTROL WAS ACHIEVED OVER A TAXIWAY. HE ELECTED TO CHOP THE POWER AND LAND. THE AIRCRAFT LANDED HARD IN A 3 POINT ATTITUDE AND WAS DAMAGED. THE PILOT BELIEVED THAT THE FRONT CANOPY PIN WAS ENGAGED BEFORE TAKE- OFF (IT WAS VISUALLY CHECKED). HOWEVER, HE NOTED THAT THE REAR PIN WAS LOCATED OUTSIDE. HE RECOMMENDED A MORE PRUDENT CHECK OF THE CANOPY ATTACHMENT (FRONT AND REAR PINS). HE HAD INSTALLED A NEW WEATHER SEAL AT THE REAR HATCH. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1982_NYC83LA007.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 (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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