Written with AI assistance and may contain mistakes. Verify against the official Transport Canada publications before relying on anything here.

PPL Tester

Lateral stability

Lateral stability: roll-axis stability. Aircraft tends to roll back to wings-level after a wing drops.

Four design features:

Feature What it is Effect
Dihedral Wingtip-up angle, root to tip Low wing sideslips toward the drop, meets relative wind at higher angle of attack, more lift, rises to level
Sweepback Swept wing Adds "effective dihedral": dropped wing's leading edge more square to airflow, more lift, rises
Wing location High wing vs low wing High wing adds extra effective dihedral over low wing
Keel effect / weight distribution (high wing) Fuselage hangs below wing like ship's keel below waterline, most side (keel) area above CG In a slip, airflow pressure on upper keel area plus fuselage weight swinging back like a pendulum rolls aircraft to wings-level

In turns, lateral stability pushes back toward wings-level (TP 1102):

Turn Why Bank tendency
Power-off descending Inner wing flies steeper spiral, raising its angle of attack enough to offset outer wing's speed advantage Tends to hold constant
Climbing Outer wing gets extra lift from greater speed and greater angle of attack Tends to increase, aileron needed to hold

Trap: dihedral not the only source. High-wing aircraft with little or no dihedral can still be laterally stable from wing location and keel effect alone. Also, bank does not hold in a climbing turn: it increases; aileron needed to hold.

References


Practice