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

PPL Tester

Spin aerodynamics

Spin = stall aggravated by yaw: one wing more stalled than the other, so aircraft autorotates (automatic, self-sustaining roll) (TP 1102).

Mechanism (TP 1102): wing making less lift near stall drops.

Wing Angle of attack Result
Downgoing GREATER Loses more lift (no self-restoring, unlike ordinary angles); more stalled; drag rises sharply, adds yaw, pushes AoA up further
Upgoing REDUCED Stays less stalled; more lift; accentuates roll

Direction (TP 1102; TC sample exam Q21):

Motion (TP 1102):

Stages (TP 1102):

Stage Span Detail
Incipient Stall and start of rotation until spin axis vertical or nearly vertical Flight path swings horizontal to vertical; rotation rate builds to fully developed rate, typically 4 to 6 seconds (about two turns) in light aircraft
Fully developed Near-vertical descent Attitude, angles, motion repetitious and stabilized turn to turn; held by balance of aerodynamic and inertia forces and moments

Incipient AoA (TP 1102):

Forces and speed (TP 1102 Ex.13, Ex.14):

Entry needs a full stall, not a nose-down attitude (TP 1102):

Trap: assuming a spin needs a steep nose-down start. AoA, not pitch attitude, triggers it; entry possible from level or climbing flight.

References


Practice