BFO89LA052
1989-07-01 · MCHENRY, Maryland, United States · Minor · 1 aircraft · Status: Completed
Airport 2G4
Aircraft involved
Probable cause & findings
THE PILOT LANDED HARD AND COLLAPSED THE LANDING GEAR WHEN HE FAILED TO ARREST HIS DESCENT RATE DURING LANDING. AFTERWARDAS HE TRIED TO MAKE A GO-AROUND THE PILOT DID NOT OBTAIN ADEQUATE FLYING SPEED, THE AIRCRAFT STALLED AND COLLIDED WITH THE GROUND.
Factual narrative
THE PLT MADE THE LNDG APCH WITH FULL FLAPS AT AN AIRSPEED OF APRX 90 KTS. ACCORDING TO THE PLT, HE ENCOUNTERED WIND SHEAR AT THE RWY THRESHOLD, LANDED HARD, AND BOUNCED SEVERAL TIMES. THE LANDING GEAR COLLAPSED. THE PLT TRIED TO MAKE A GO-AROUND BUT WAS UNABLE TO CLIMB OUT OF GROUND EFFECT OR GAIN FLYING SPEED. THE ACFT STALLED AND COLLIDED WITH THE GROUND LEFT OF THE RWY. RWY 26 WAS USED. THE LOCAL WINDS WERE REPORTED AT 260 DEGS AT 5 KTS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1989_BFO89LA052.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (wind shear, stall, go-around). All research papers
- NASA NTRS 2019 · Conference Paper Optimal recovery from microburst wind shear
The flight path of a twin-jet transport aircraft is optimized in a microburst encounter during approach to landing. The objective is to execute an escape maneuver that maintains safe ground clearance …
- NASA NTRS 2013 · Conference Paper Optimal nonlinear estimation for aircraft flight control in wind shear
The most recent results in an ongoing research effort at Princeton in the area of flight dynamics in wind shear are described.
- 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.