Gusts on Final to Runway 10
Crosswind conditions exceed demonstrated capability — the decision to go-around comes too late
The scenario
Departing Lakeland Linder International Airport (KLAL), Lakeland, FL — Runway 10, on a personal flight. Field elevation 142 ft MSL. You are a commercial pilot with roughly 800 hours total time, 200 hours in complex aircraft (retractable gear, constant-speed prop). This is your second visit to KLAL; you are not intimately familiar with the field.
Current conditions: Wind 110° at 18 gusting to 28 knots. Runway 10 is aligned 090° (true). The crosswind component is roughly 17 knots steady, gusting to 27 knots. The Piper Arrow PA-28R has a demonstrated crosswind capability of 12 knots (per POH). You are at or above the demonstrated limit, and the gusts exceed it significantly.
You are on a 12-mile final to Runway 10, 1,200 ft AGL, gear down, flaps 20°, airspeed 90 KIAS (Vy — best rate of climb speed, slightly above approach speed of 75 KIAS). The tower has cleared you to land. The wind is noticeably pushing the airplane; you are holding a 15° crab angle to maintain runway alignment.
Aircraft: Piper Arrow PA-28R, solo, within weight and balance limits. Fuel adequate. Gear is down and locked (three green lights). Constant-speed prop is set to high RPM. Flaps are at 20°. The airplane is configured for landing.
Pilot: You — a commercial pilot, current, 800 hours total, 200 hours complex. You have landed in crosswind conditions before, but not in gusts this strong. Your personal minimums are 15 knots demonstrated crosswind. Today's conditions are at or above that limit. You did not brief a go-around decision point before entering the approach.
- {'label': 'Field', 'value': 'KLAL · Lakeland Linder'}
- {'label': 'Runways', 'value': '5/23 · 10/28'}
- {'label': 'Elevation', 'value': '142 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 landings in the PA-28R and when to go-around? (Pick all that apply; this records your baseline.)
What the record shows
What the NTSB files show
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, which resulted in a runway excursion. This scenario's crosswind loss-of-control is a different failure mode, but the outcome — runway excursion — is the same.
NTSB CEN21LA269 (2021): A Piper PA-28R on a personal flight experienced loss of directional control during the takeoff roll and struck runway signs and lights. The probable cause was the pilot's failure to maintain directional control. While this event occurred on takeoff rather than landing, the mechanism — loss of directional control in gusty conditions — is identical to the landing scenario.
NTSB GAA17CA105 (2016): A Piper PA-46 experienced loss of directional control during landing rollout in gusting crosswind conditions that exceeded the aircraft's demonstrated crosswind capability. The pilot did not recognize when conditions exceeded the aircraft's limits and did not commit to a go-around early. The airplane exited the runway and was damaged.
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 pilot did not recognize that the gusts exceeded the aircraft's demonstrated capability.
NTSB GAA19CA170 (2019): A Piper PA-11 tailwheel aircraft lost directional control during landing roll in gusting crosswind conditions, veered off the runway, struck a ditch, and came to rest inverted. The probable cause was the pilot's failure to maintain directional control during the landing roll. The pilot did not recognize the loss of directional control early enough to recover.
NTSB ERA10CA448 (2010): A Cessna 182E landed on a runway with a direct crosswind during landing rollout. The crosswind pushed the aircraft off the runway to the left, causing it to nose over. The probable cause was inadequate compensation for crosswind conditions. The pilot did not assess the runway's suitability independently.
The consistent thread across all these events: pilots did not recognize when crosswind conditions exceeded the demonstrated capability of the aircraft. The demonstrated crosswind capability (12 knots for the PA-28R) is not a personal-minimums threshold — it is the limit tested by the manufacturer. Gusts that exceed that limit are a signal to go-around or divert. The decision window is on downwind or base, when you have altitude and airspeed. By the time you are on short final or in the flare, your options are severely limited.
At KLAL, the off-field environment off Runway 10 (heading 090°) is low-density development and open areas — not ideal for an excursion, but not a cliff or water. The runway is 8,500 ft long, so there is plenty of pavement. But the lesson is the same: recognize the limit, go-around early, and either try a different runway or divert.
Key lesson — The PA-28R has a demonstrated crosswind capability of 12 knots. Gusts that exceed that limit are a signal to go-around or divert — not to push through and hope for the best. The decision must be made early, on downwind or base, when you have altitude and airspeed. By short final, your options are limited. By the flare, you are committed. Know your aircraft's limits, recognize when conditions exceed them, and make the decision early.
Debrief — teaching points
Demonstrated crosswind capability is a hard limit, not a personal-minimums threshold.
The PA-28R's demonstrated crosswind capability of 12 knots is the maximum crosswind tested by the manufacturer under controlled conditions. It is not a personal-minimums guideline — it is the limit of the aircraft's control authority. Gusts that exceed that limit are a signal to go-around or divert. The NTSB precedents (GAA17CA105, ERA21LA119, GAA19CA170, ERA10CA448) all show pilots who did not recognize this distinction and pushed through conditions that exceeded the aircraft's capability.
The decision to go-around must be made early — on downwind or base — not on short final.
On downwind or base, you have altitude (1,500–2,000 ft AGL), airspeed (90+ KIAS), and options. You can request a different runway, divert, or circle and try again. By short final (300 ft AGL), your options are severely limited. By the flare (100 ft AGL), you are committed. The decision window is early. If you are not comfortable with the crosswind conditions on downwind, go-around then — not on short final.
A crab angle of 15° or more is a warning sign that crosswind conditions are becoming unmanageable.
A crab angle is the angle between the airplane's heading and the runway heading needed to maintain runway alignment. A crab angle of 15° or more indicates that the crosswind component is significant and the airplane is being pushed laterally. This is a warning sign. If you find yourself holding a 15° crab angle on final approach, the conditions are marginal or beyond your demonstrated capability. Consider a go-around.
During the flare and touchdown, the airplane is at its slowest airspeed and most vulnerable to loss of control.
At 60–70 KIAS in landing configuration (flaps 20°, gear down), the PA-28R is near stall speed (Vs0 = 55 KIAS). The control authority is minimal. A gust that lifts a wing or pushes the airplane laterally cannot be easily corrected. The flare is the most vulnerable phase of the landing. If you are not confident in your directional control by the time you reach the flare, it is too late to recover — you are committed to landing.
Headwind component helps, but it does not change the crosswind limit.
A headwind component does reduce ground speed and increase control authority slightly. But it does not change the fundamental problem: if the crosswind component exceeds the demonstrated capability, the aircraft cannot be reliably controlled. A 15-knot crosswind with a 10-knot headwind is still a 15-knot crosswind. The headwind helps, but it does not eliminate the risk.
Loss of directional control on the ground is a ground loop — a survivable but damaging outcome.
If the airplane drifts off the runway and the landing gear catches on rough terrain, the airplane can pivot on one gear and roll over. This is a ground loop. It is survivable, but it results in a complete loss of the aircraft. The NTSB precedents show that ground loops are often the outcome of a crosswind landing that goes wrong. The lesson: prevent the ground loop by going-around early, not by trying to recover from a drift during rollout.
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 / distraction), CEN23LA417 (2023 PA-28RT gear retraction / runway excursion), CEN21LA269 (2021 PA-28R loss of directional control on takeoff), and regional crosswind-loss-of-control precedents GAA17CA105 (2016 PA-46 crosswind excursion), ERA21LA119 (2021 C172R crosswind loss of control), GAA19CA170 (2019 PA-11 tailwheel crosswind), and ERA10CA448 (2010 C182E crosswind nose-over). Localized to KLAL.
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.V.A — Preflight Inspection · PA.V.B — Cockpit Management · PA.VII.A — Normal Takeoff and Climb · PA.VII.B — Normal Approach and Landing · PA.VII.C — Go-Around / Rejected Landing · PA.IX.C — Emergency Approach and Landing
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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