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Dynamic hydroplaning speed: what the estimate tells you

Published by PilotDeskSources, testing & corrections

Dynamic hydroplaning occurs when water pressure beneath a moving tire reduces or eliminates contact between the tire and runway. The familiar tire-pressure equation estimates a minimum speed associated with the start of dynamic hydroplaning under the test relationship. It does not predict whether a particular landing will hydroplane, how much braking will remain, or how much runway an airplane needs.

The distinction matters: a calculated speed is a study reference, while landing performance depends on the actual runway, contaminant, aircraft, tires, loading, speed, technique, and approved procedures.

The FAA estimate at 24 and 36 PSI

The FAA Airplane Flying Handbook gives the minimum dynamic hydroplaning speed estimate as:

Vp (knots) ≈ 8.6 × √(main-tire pressure in PSI)

For a main tire inflated to 24 PSI, √24 is about 4.90. Multiplying by 8.6 gives about 42 knots, matching the handbook's example. At 36 PSI, the same calculation gives 8.6 × 6 = 51.6 knots, or about 52 knots.

Some training material rounds 8.6 to 9 for mental arithmetic. That shortcut gives 54 knots at 36 PSI. Keep the rounded result labeled as a rough rule; use the FAA coefficient when quoting the handbook relationship.

What the relationship assumes

This is an estimate for dynamic hydroplaning onset. It does not describe every wet-runway loss of friction. The FAA handbook explains that dynamic hydroplaning is associated with a water layer around one-tenth of an inch or deeper, where a wedge of water can form under a tire. Actual onset and persistence depend on water depth, speed, tire pressure, tread and runway characteristics.

A thin film can still be hazardous through viscous hydroplaning, especially on smooth or rubber-polished pavement. Reverted-rubber hydroplaning is a different mechanism involving a locked or slowly rotating tire and heat from a prolonged skid. Neither is captured by the pressure equation. Hydroplaning that has already started may persist well below the estimated onset speed.

How to use the estimate in training

  1. Confirm that the question is about dynamic hydroplaning and use the correct main-tire pressure units.
  2. Calculate the square root, multiply by 8.6, and keep the result in knots.
  3. State the result as an approximate minimum onset estimate, not a guaranteed threshold.
  4. Explain that water depth, pavement, tire condition, speed, and other hydroplaning types are outside this one-variable calculation.

For example, an answer of approximately 42 knots at 24 PSI does not mean that a runway is safe below 42 knots, that braking will be normal below that speed, or that hydroplaning must occur above it. It only demonstrates the pressure-based relationship under the handbook's stated context.

Operational decisions require runway and aircraft data

When standing water, slush, or another contaminant is reported, use the current runway-condition information and the aircraft's applicable approved landing-performance data and procedures. Consider the complete landing plan, including approach and touchdown speed, runway available, wind, slope, braking reports, and any operator or aircraft limitations. Do not use this equation to calculate stopping distance or to replace a landing-distance assessment.

The FAA's active AC 91-79B, Aircraft Landing Performance and Runway Excursion Mitigation, covers runway-condition assessment and landing-performance risk management. Check the current advisory circular and the source data applicable to the operation.

Sources and related tools

This explanation follows the FAA Airplane Flying Handbook, Chapter 9 (hydroplaning types and the 8.6 × √PSI relationship). See the hydroplaning calculator for the arithmetic, and PilotDesk Sources & Methods for how the site distinguishes estimates from approved aircraft data.

Training reference only. The equation does not establish a safe speed, braking capability, or landing distance. Use current runway reports and the applicable approved aircraft information for operational decisions.