Tailwind · Vol I, N° 01
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Task CConstant-Airspeed Descents

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Recommended: finish Task BConstant-Airspeed Climbs first.

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PA.VIII.C.PRI· Principles

Principles & why

Principles & why: the mirror task, descent energy, and altitude awareness

A constant-airspeed instrument descent is the mirror task to the climb (B). The principles carry over directly: ASI primary for pitch, pitch-for-airspeed, power-for-rate, level-off anticipation by 10%. This PRI focuses on what's different from B — the descent-specific energy management and the altitude-awareness risk that makes descent's level-off more consequential than climb's.

The mirror — what carries from B

The full pedagogical chain from B applies in C without modification:

  • The primary-supporting model shifts when the flight phase changes. Straight-and-level uses altimeter as pitch primary; constant-airspeed climb/descent uses ASI.
  • Pitch controls airspeed; power controls rate of altitude change. The same axis assignment IV.B PRI introduced for the visual landing.
  • Lead the level-off by 10% of the rate. The airplane has momentum; anticipate it.

These aren't restated in C — they're the same lessons, learned in B, applied here.

BASIC INSTRUMENT SCAN · PA.VIII.A–D

Primary-supporting model — Constant-airspeed descent

Scan paused

PLATE 33 · SCAN PATTERN

ASIAirspeedPRIMARY · PITCHAIAttitudeSCAN ANCHORALTAltimeterSUPPORTINGTCTurn coord.SUPPORTINGHIHeadingPRIMARY · BANKVSIVert. speedSUPPORTINGMP/RPMPowerPRIMARY · POWER
AI → ASI → AI → HI → AI → MP

Constant-airspeed descent

Mirror of the climb. Same primary-supporting matrix; opposite direction. ASI for pitch, HI for bank, MP/RPM for power. The 10% level-off anticipation applies here too — lead the target altitude by ~10% of the descent rate.

Identical primary-supporting matrix to the climb. ASI primary for pitch, HI primary for bank, MP/RPM primary for power. Toggle between Climb and Descent to confirm — they're mirror tasks at the scan level.

Descent energy management

A descending airplane is trading altitude for time and/or speed. Three combinations:

  • Constant-airspeed descent (this task): altitude bleeds at a controlled rate; airspeed stays at target. The pilot has chosen the airspeed; the descent rate is what the airplane gives at the selected power.
  • Constant-rate descent (CFII content): descent rate is controlled by power; airspeed varies with pitch as needed to hit a vertical speed target.
  • Constant-attitude descent: pitch attitude is fixed; airspeed and rate vary together based on power.

For the PPL standard, the constant-airspeed variant is the trained discipline because it's the foundation for instrument approaches (which control airspeed for stability) and for any descent where airspeed has to stay below a flap-limit speed.

Why altitude awareness matters more in descent than climb

In a climb, busting the target altitude on the high side has consequences (airspace incursion, missed level-off, traffic conflict), but the airplane is at higher altitude — there's recovery margin and time to correct.

In a descent, busting the target altitude on the low side can mean:

  • Terrain or obstacle conflict if the target is the minimum safe altitude.
  • Airspace incursion into airspace below (Class B floor, military operations area floor).
  • Approach instability if the target is an intermediate altitude on an approach.

VIII.C.R2 (in the source manifest's risk element) explicitly names "inadvertent descent below assigned altitude or terrain" as a risk. The pilot's altitude awareness on descent is more consequential than on climb.

The discipline: the level-off anticipation rule isn't optional in descent. A late level-off (continuing past the target altitude downward) can have hard consequences.

ANTICIPATION DISCIPLINE · PA.VIII.B–D

Lead the level-off10% of rate

Lead = 70 ft

PLATE 34 · LEVEL-OFF LEAD

TargetLeadStartAltitudeTimeBegin level-offReactive overshootsAnticipated: smooth
Anticipated (lead by 10% of rate)Reactive (wait for the target)Target
700 fpm → lead 70 ft
300 fpm1200 fpm

Vertical momentum carries the airplane through the level-off transition. Lead by 10% of the descent rate — at 700 fpm, that's 70 ft above target before initiating the level-off. Pitch and power together; trim; verify on the altimeter.

Mirror of the climb: in a 700 fpm descent, begin the level-off 70 ft above target. The reactive trace overshoots BELOW the target — which is the consequence the prose just named. Anticipate.

The descent's lower power means less rudder

In the climb (B), full power + high AoA produces strong left-turning tendencies — active right rudder. In the descent, reduced power + lower AoA reduces these tendencies. The required rudder pressure is closer to that of straight-and-level (VIII.A).

A pilot transitioning from a climb to a descent in training sometimes carries over the climb's right-rudder habit, producing a right heading drift in the descent. The fix is awareness: rudder pressure changes with power setting.

What this task feeds into

VIII.C builds toward:

  • VIII.D (turns to headings) — same scan-shift principle; bank rate (turn coordinator) becomes a primary instrument.
  • VIII.E (unusual attitudes) — the descent regime is half of the unusual-attitude recovery picture (nose-low recovery).
  • Future instrument approach training at CFII / IFR rating — the constant-airspeed descent is the building block for the ILS final approach segment.

Why pair this with B as bidirectional in training

B and C are pedagogically the same lesson. Training them as a pair — climb to altitude, level off, descend back to entry, level off, repeat — builds the transitions as well as the steady-state phases. Most pilots' first 10 hood-time hours are heavy on B+C transitions because the transition is where the scan compresses and reorganizes; the steady-state phases are easier once the transitions are clean.

Mastering both halves of the climb/descent pair sets up VIII.D (turns) — which adds horizontal motion to the vertical management this pair trains.

★ Next up

PA.VIII.C.ERR · Common errors

Constant-airspeed descent errors mirror the climb's (B) error families: primary-shift errors, level-off precision errors, and scan or coordination errors. Th…