Gusty Crosswind at Venice
Loss of directional control during landing rollout in a Piper Arrow — the decision to go around comes too late
The scenario
Departing Venice Municipal Airport (KVNC), Venice, FL — Runway 22, landing in a gusty afternoon crosswind. Field elevation 18 ft MSL. You are a commercial pilot with roughly 800 hours total, current and proficient in the Piper Arrow PA-28R-200. This is a personal flight; you are familiar with KVNC.
The weather is VFR: scattered clouds 3,500 ft, visibility 10 SM, wind from 310° at 18 gusting to 28 knots. Runway 22's magnetic heading is 225°, so the crosswind component is roughly 18 knots steady, gusting to 28. The Piper Arrow's demonstrated crosswind capability is 15 knots. You are above the demonstrated limit, and the gusts are pushing you well beyond it.
You are on short final to Runway 22, gear down, flaps 40°, airspeed 75 KIAS (Vref). The runway is 5,640 ft long — plenty of length. You have been flying the Arrow for three years; you are comfortable with the airplane. The wind is gusty but not extreme. You decide to land.
Aircraft: Piper PA-28R-200, solo, within limits. Constant-speed prop, retractable gear, fuel-injected Lycoming IO-360. Gear is down and locked; prop is set to high RPM. Flaps are full (40°). You are stable on the glide slope at 75 KIAS.
Pilot: You — commercial pilot, 800 hours, current. You have landed in crosswind before. Your personal minimums are 20 knots demonstrated crosswind (higher than the airplane's published 15 knots). The gusts are at 28 knots, but you are committed to the landing. You have not briefed a go-around or discussed abort criteria with yourself.
- {'label': 'Field', 'value': 'KVNC · Venice'}
- {'label': 'Runways', 'value': '4/22 · 13/31'}
- {'label': 'Elevation', 'value': '18 ft'}
- {'label': 'Aircraft', 'value': 'PA-28R'}
- {'label': 'Dominant phase', 'value': 'Landing / Takeoff'}
The decision
Before we get into the decision tree — what do you know about crosswind landing limits and go-around decision-making in the Piper Arrow? (Pick all that apply; this records your baseline.)
What the record shows
What the NTSB files show
NTSB CEN21LA269 (2021): A Piper PA-28R-180 on a personal flight experienced loss of directional control during the takeoff roll. The pilot failed to maintain directional control and struck runway signs and lights. The probable cause was the pilot's failure to maintain directional control during the takeoff roll. This accident shows that loss of directional control in the Piper Arrow is not limited to landing — it can occur on takeoff as well, and the consequences are equally severe.
NTSB WPR25LA178 (2025): A Piper PA-28R-200 on a test flight following annual inspection experienced brake system failure during landing rollout due to a hydraulic fluid leak. The aircraft exited the runway and collided with a fence. The probable cause was a failure of the brake system during landing due to a hydraulic fluid leak. This accident demonstrates that even a well-maintained Arrow can experience brake failure during the landing rollout phase — a critical moment for directional control.
NTSB CEN23LA417 (2023): A Piper PA-28RT-201 experienced partial retraction of the right main and nose landing gear during landing rollout, causing the right wing to scrape the runway and the aircraft to exit the runway. The cause of the gear retraction could not be determined despite extensive testing. This is a particularly insidious failure mode in the Piper Arrow: the gear can partially retract during the landing rollout phase, causing a wing strike and runway excursion. The pilot has no control over this failure once it begins.
NTSB GAA17CA105 (2016): A Piper PA-46 (a complex aircraft similar to the Arrow) experienced loss of directional control during landing rollout in gusting crosswind conditions that exceeded the aircraft's demonstrated crosswind capability. The probable cause was the pilot's loss of directional control during the aborted landing in gusting crosswind conditions. The key lesson: recognize when crosswind conditions exceed aircraft limits and commit to a go-around early rather than attempting recovery during rollout.
NTSB ERA21LA119 (2021): A Cessna 172R on a personal flight veered left off the runway during landing in gusting crosswind conditions and struck the ground with the propeller and left wing tip. The probable cause was the pilot's failure to maintain directional control during landing in a gusting crosswind. The teaching point: evaluate whether personal minimums and tactical adjustments (flap reduction, speed increase) are adequate for actual conditions; recognize the point at which to abandon the landing and go around.
The real accidents cited above occurred at other airports and in other aircraft — NOT at Venice Municipal Airport (KVNC). KVNC has its own accident history dominated by loss-of-control inflight (24.4%), forced landing (12.2%), spatial disorientation (12.2%), hard landing (12.2%), and loss-of-control ground (12.2%). The scenario is localized to KVNC to make the runway selection and crosswind decision real and consequential for you as a pilot here.
The consistent thread across all these events: loss of directional control during landing rollout in crosswind conditions is a recurring failure mode in complex aircraft like the Piper Arrow. The decision to land must be made BEFORE touchdown, based on a clear assessment of whether crosswind conditions are within demonstrated limits. Once the wheels are on the runway, directional control becomes a ground-handling problem — and the margin for error is zero.
Key lesson — At KVNC, a non-towered field with multiple runways, runway selection is your responsibility. The Piper Arrow's demonstrated crosswind capability is 15 knots — this is not a suggestion, it is a limit. When gusts push the crosswind component above this limit, the decision to go around must be made on short final, BEFORE touchdown. Personal minimums higher than demonstrated capability are a trap. Once the wheels are on the runway, directional control becomes a ground-handling problem, and the margin for error is zero. Recognize the point at which to abandon the landing and go around — or divert to a runway with more favorable wind alignment.
Debrief — teaching points
Demonstrated crosswind capability is a limit, not a suggestion.
The Piper Arrow PA-28R-200 has a demonstrated crosswind capability of 15 knots. This is the maximum crosswind component the manufacturer has tested and certified the airplane can handle safely. When wind conditions exceed this limit — as they do when you have an 18-knot steady crosswind gusting to 28 — you are operating outside the airplane's tested envelope. Personal minimums higher than demonstrated capability (e.g., 'I can handle 20 knots') create a false sense of security and delay the go-around decision. The demonstrated limit is the limit.
The go-around decision must be made on short final, BEFORE touchdown.
Once the main gear touches the runway, directional control becomes a ground-handling problem, not an airborne one. Your control authority is limited. A gust or loss of control during the rollout phase will push you off the runway. The decision to land must be made BEFORE touchdown, based on a clear assessment of whether crosswind conditions are within limits. If they are not, go around. Do not attempt to recover directional control during the rollout phase — that is a losing battle.
Gust component adds to effective crosswind.
When wind is gusting, the gust component (peak gust minus steady wind) adds to the effective crosswind. A wind of 18G28 knots is not the same as a steady 18-knot wind. The gust component is 10 knots, which adds to the steady 18-knot crosswind to create peak crosswind conditions of 28 knots. This is nearly double the demonstrated crosswind limit. Understand the difference between steady wind and gusting wind, and assess the peak crosswind component, not just the steady component.
Runway selection is your responsibility at a non-towered field.
KVNC is a non-towered field with two runways: 04/22 and 13/31. Runway selection is your responsibility — there is no tower to assign a runway. When wind conditions create an excessive crosswind on one runway, the other runway may offer a more favorable wind alignment. In this scenario, Runway 22 has an 18-knot crosswind in a 310° wind, while Runway 13 would have a headwind component instead. Evaluate both runways and choose the one with the smallest crosswind component. If you are already committed to an approach and the crosswind is excessive, go around and set up for the other runway.
Aggressive control inputs during rollout can worsen directional control.
During the landing rollout phase, the airplane is transitioning from airborne to ground-based control. Aggressive aileron and rudder inputs can cause the wing to rise and the airplane to drift off the centerline — the opposite of what you intend. Use smooth, progressive control inputs during rollout. If the airplane is drifting, reduce aileron input and apply rudder smoothly. Let the airplane settle. Aggressive inputs are a trap.
The Piper Arrow's retractable gear adds complexity to crosswind landings.
The Piper Arrow's retractable gear is a system that requires management during landing. NTSB CEN23LA417 shows that the gear can partially retract during the landing rollout phase, causing a wing strike and runway excursion. While this is a rare failure, it underscores that the Arrow is a complex aircraft. Ensure the gear is down and locked before landing, and be aware that gear-related failures can occur during the rollout phase. After landing, do not retract the gear until the airplane is fully stopped and you have confirmed directional control.
Built from the real accident record
Scenario built from NTSB WPR25LA178 (2025 PA-28R brake failure / runway excursion), CEN24LA288 (2024 PA-28R gear-up landing), CEN23LA417 (2023 PA-28RT gear retraction during rollout), CEN21LA269 (2021 PA-28R loss of directional control on takeoff), and regional crosswind-loss-of-control precedents GAA17CA105, ERA21LA119, GAA19CA170, ERA10CA448. Localized to KVNC.
NTSB reports: WPR25LA178 · CEN24LA288 · CEN23LA417 · CEN21LA269 · GAA17CA105 · ERA21LA119 · GAA19CA170 · ERA10CA448
ACS tasks: PA.I.F — Weather Information · PA.I.G — Cross-Country Flight Planning · PA.III.D — Crosswind Takeoff and Landing · PA.I.H — Human Factors · PA.V.A — Preflight Inspection
Relevant FARs: §91.3 · §91.13 · §91.103
Step through the full decision tree, make the calls, and see where each choice leads — then debrief it with your CFI.
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