Tailwind · Vol I, N° 01
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Task AManeuvering During Slow Flight

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PA.VII.A.PRI· Principles

Principles & why

Principles & why: minimum controllable airspeed, the back side, and the landing-regime preview

Maneuvering during slow flight is the training regime that lets a pilot rehearse the airplane's landing behavior with altitude to spare. It also makes the back side of the power curve visceral — students who learn slow flight as a regime, not just a textbook concept, then recognize it on every approach. Three principles drive the maneuver: AoA and stall, the back-side power-curve geometry, and the control-feel transition that prepares pilots for the landing regime.

AoA, stall, and minimum controllable airspeed

A wing produces lift proportional to angle of attack (AoA) and dynamic pressure (which depends on airspeed²). For a given weight at a given altitude, the airplane must produce the same lift = weight to maintain altitude. That equation can be satisfied many ways:

  • High airspeed, low AoA (cruise).
  • Low airspeed, high AoA (slow flight).
  • Anywhere in between.

But there's a limit. AoA can't increase beyond the critical angle — typically around 16–18° for a trainer wing. At critical AoA, the airflow separates from the upper wing surface, lift drops abruptly, and the wing stalls.

The slowest airspeed at which the airplane can sustain lift = weight (so altitude can be held) is the stall speed. At that airspeed, AoA equals critical — there's no margin.

Minimum controllable airspeed is just above stall speed — typically 5–10 KIAS faster. The airplane is at high AoA but not yet stalled; the stall warning may activate intermittently. This is the regime the slow-flight maneuver trains in.

The back side of the power curve

In level flight, the power required to maintain altitude is U-shaped against airspeed:

  • Above L/D_max: power required increases with speed (you're paying parasite drag, which scales with speed²).
  • At L/D_max: power required is minimum.
  • Below L/D_max: power required increases as speed decreases — induced drag rises rapidly at low speed and high AoA.

The region below L/D_max is the back side of the power curve. The first time the soft-field takeoff (C) introduced this, and the short-field takeoff (E) reinforced it. Slow flight is the regime that lives on the back side — you're flying continuously below L/D_max.

AERODYNAMICS · PA.IV.C / PA.IV.E / PA.VII.A

The power curve

Slide the marker below L/D max and watch drag go up as you slow down.

PLATE 41 · POWER CURVE

BACK SIDEV_SV_XV_YL/D MAX · MIN DRAG406080100120140AIRSPEED · KIASTOTAL DRAG · THRUST REQUIRED
52 KIAS

Region

Back side

Slowing down increases drag. Altitude is controlled with power here.

Total drag

1.39 × minimum

Relative to the drag at L/D max, which is the least drag the airplane can produce.

Induced share

85%

The rest is parasite drag. They are equal at L/D max — that is what puts the minimum there.

Slow flight's minimum controllable airspeed lives deep in the back-side region. Slide the marker between 50 and 80 KIAS and notice how drag grows quickly as airspeed drops below L/D max. That's the "induced drag dominates at low speed" the description names; it's also why slow flight is power-managed for altitude (more drag = needs more power).

The implication for control:

  • Increasing pitch at constant power decreases airspeed (because drag rises), which steepens the descent. Same input, opposite consequence from normal flight.
  • Adding power at constant pitch flattens the descent / produces climb.

This is what "pitch for airspeed, power for altitude" means in practice on the back side. It's also exactly the same control discipline the normal landing (B) requires on final — slow flight rehearses it without a runway to focus on.

The control-feel transition

In cruise, primary controls feel light and responsive. Small inputs produce immediate effects.

In slow flight, the same inputs feel sluggish and delayed. The aerodynamic surfaces are working in slower airflow; their effectiveness drops with the square of airspeed. The student notices:

  • Elevator response slow — a pitch input takes a moment to produce a noticeable nose change.
  • Aileron response slow — banking feels heavy.
  • Rudder response strong — at high AoA, the rudder is the most authoritative axis. P-factor and torque are aggressive; rudder is the only way to coordinate them.

This is the control regime of the round-out and flare. Pilots who've practiced slow flight feel the transition into the round-out as a familiar regime; pilots who haven't, find it disorienting.

The landing-regime preview

Combining the three: slow flight is the approach-and-landing regime moved to maneuvering altitude. The airplane is:

  • Slow — at or near approach speed (V_REF range).
  • High AoA — close to (but not at) stall margin.
  • On the back side — power controls altitude, pitch controls airspeed.
  • Sluggish primary controls + active rudder — same control feel as the round-out and flare.

Practiced often, the regime becomes familiar; the landing then feels like an extension of slow flight, not a separate skill. Pilots who only meet slow flight in the round-out find the round-out frightening; pilots who meet it routinely at altitude find it predictable.

Why this maneuver matters

Beyond the landing connection, slow flight trains stall recognition. A pilot who's flown the airplane at stall warning understands the cues — buffet, mushy controls, decay rate — and recognizes them on final or during a botched takeoff. The next two tasks (B and C) extend slow flight by deliberately stalling, but the recognition framework starts here.

★ Next up

PA.VII.A.ERR · Common errors

Slow flight errors split into three families: airspeed-band errors (not slow enough, or accidentally stalling), altitude errors (the back-side power-vs-altit…