DEN03LA011
2002-10-21 · Fort Collins, Colorado, United States · Minor · 1 aircraft · Status: Completed
Airport FNL
Current FAA registration · N41807
- Make / Model
- BELLANCA 7KCAB
- Year of manufacture
- 1973 · 29 years old at event
- Engine
- LYCOMING IO-320 SERIES (150 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19731002
- ADS-B equipped
- Yes — Mode-S A4F450
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper recovery from a bounced landing, and his failure to maintain airspeed resulting in a stall.
Factual narrative
On October 21, 2002, at approximately 1810 mountain daylight time, a Bellanca 7KCAB, N41807, registered to Swain Aviation LLC, and operated by The Flying School, both of Fort Collins, Colorado, was destroyed when it nosed over following an attempted go-around during a touch-and-go landing at Fort Collins-Loveland Municipal Airport (FNL), Fort Collins, Colorado. The private pilot, the sole occupant on board, received minor injuries. Visual meteorological conditions prevailed. No flight plan had been filed for this local flight being conducted under Title 14, CFR Part 91. The flight originated at approximately 1730. According to the pilot, he was doing touch-and-go landings on runway 15. On this approach, he made a 3-point landing and bounced. He settled the airplane back down for a second 3-point landing, but there was a "lack of directional ground control and some drift to the right of centerline." He added full power for a go-around, but the controls felt "mushy," and there was a "lack of aileron control." The airplane drifted to the right, struck the runway with its right wingtip, and nosed over. The airplane sustained substantial damage to both the left and right wing spars, empennage, forward fuselage, both main landing gear attachment points, rudder and left horizontal stabilizer. The reported weather conditions at 1815 was wind, 070 degrees at 07 knots; visibility, 10 statute miles; sky condition, clear; temperature, 11 degrees C.; dew point, 03 degrees C.; altimeter setting, 30.00. According to these conditions, a landing on runway 15, would result in an 80 degree left-hand crosswind. According to the pilot, he was doing touch-and-go landings on runway 15. On this approach, he made a 3-point landing and bounced. He settled the airplane back down for a second 3-point landing, but there was a "lack of directional ground control and some drift to the right of centerline." He added full power for a go-around, but the controls felt "mushy," and there was a "lack of aileron control." The airplane drifted to the right, struck the runway with its right wingtip, and nosed over. The airplane sustained substantial damage to both the left and right wing spars, empennage, forward fuselage, both main landing gear attachment points, rudder and left horizontal stabilizer. The winds were, 070 degrees at 07 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_DEN03LA011.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (stall, go-around). All research papers
- 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 …
- NASA NTRS 2025 · Conference Paper A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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.
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Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
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