WPR14CA344
2014-08-13 · PINE BLUFFS, Wyoming, United States · None · 1 aircraft · Status: Completed
Airport 82V
Current FAA registration · N2830X
- Make / Model
- CESSNA 177
- Year of manufacture
- 1967 · 47 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20000523
- ADS-B equipped
- Yes — Mode-S A2DB8E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate flare and failure to maintain aircraft control while landing.
Factual narrative
The pilot reported that during the landing flare he experienced what he believed to be wind shear or a dust devil. Just before the airplane touched down it lifted about 20 to 40 feet when the wind suddenly shifted to a tailwind and the airplane stalled. The pilot stated that the right wing dropped and the airplane entered an approximate 45 to 60 degree angle of bank. The pilot corrected the bank angle and leveled the wings but failed to apply full power to completely recover from the stall. The airplane subsequently impacted the runway nose down, bounced, then settled to the runway. The firewall and fuselage were substantially damaged. The pilot reported no preimpact mechanical malfunction or failures with the airplane that would precluded normal operation. . The pilot reported that during the landing flare he experienced what he believed to be wind shear or a dust devil. Just before the airplane touched down it lifted about 20 to 40 feet when the wind suddenly shifted to a tailwind and the airplane stalled. The pilot stated that the right wing dropped and the airplane entered an approximate 45 to 60 degree angle of bank. The pilot corrected the bank angle and leveled the wings but failed to apply full power to completely recover from the stall. The airplane subsequently impacted the runway nose down, bounced, then settled to the runway. The firewall and fuselage were substantially damaged. The pilot reported no preimpact mechanical malfunction or failures with the airplane that would precluded normal operation. . Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Dust devil/whirlwind-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2014_WPR14CA344.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
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Related research
Matched on aircraft type or causal vocabulary (wind shear, stall). 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 …
- 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…