★ PTS mapping: This lesson aligns to FAA-S-8081-20A (Nov 2023), Area of Operation VI — Landings and Approaches to Landings (per Lesson→Area map). It is a PTS, so items are Tasks/elements (no ACS K/R/S codes); read the exact Task lettering and tolerances from the current published PTS.
Match approach angle and groundspeed to the situation, manage ETL, and decide go-around early.
A normal approach is a stabilized, constant-angle descent (commonly visualized around a moderate glide angle) with airspeed and groundspeed bled off progressively so that you arrive over the intended termination point at a slow walking pace, ready to terminate to a hover or to the surface. The keys are a constant apparent angle to the spot, a smooth and continuous deceleration, and coordinated power as you cross effective translational lift (ETL) and settle into ground effect. Avoid arriving fast (overshoot/overflight) or slow and high (power-demanding, near the height-velocity avoid region).
| Approach | When to use | Cautions |
|---|---|---|
| Normal | Unobstructed approach to a known surface | Default; maintain constant angle and deceleration. |
| Steep | Obstacles on final / confined area | Higher power required near termination; watch settling-with-power (VRS) at low airspeed with high rate of descent and power. |
| Shallow | High density altitude / low-power margin / soft or unknown surface | Longer ground run if running landing; verify obstacle clearance and surface ahead. |
At ATP level, the angle is a deliberate energy and performance decision: a steep approach trades a steeper geometry for obstacle clearance but demands more power and risks VRS if you let the rate of descent grow with little airspeed; a shallow approach preserves power margin and translational lift but needs more clear distance.
In a crosswind, keep the aircraft tracking the intended ground path — typically a crab into the wind on the approach transitioning to into-wind pedal/cyclic as you decelerate, so the nose and track are controlled through the termination. Anticipate the loss of ETL on short final: as airspeed decays below the translational-lift threshold the helicopter loses the efficiency of clean airflow, sink increases, and required power rises sharply — lead it with collective. A gusty crosswind raises the workload at exactly the moment power demand peaks, so plan the power and the go-around option before you need them.
A go-around is a normal maneuver, not a failure. Decide early: if the approach is unstable, the power margin is marginal, the surface or wind is not what you expected, or the termination cannot be made safely, initiate the go-around while you still have airspeed and altitude to convert. Smoothly add power, lower the nose to regain airspeed through ETL, establish the climb, and re-enter the pattern. The trap is the late, low, slow rejection with no energy left — at ATP standard you brief the go-around criteria before final and act on them without hesitation.
Curated reference clip — “The Key To A Nice Normal Helicopter Approach” · Helicopter Online Ground School LLC (YouTube), verified via oEmbed. Embedded with the creator's player; we don't host or alter it.
✈️ Your test aircraft: the R-44 fill-in values cover its single-engine, piston, VFR figures. Approach-to-landing technique transfers, but the airspeeds, power margins, and limits are aircraft-specific. ATP-H practical tests are normally flown in a turbine and/or multi-engine, IFR-capable helicopter — use your actual test aircraft's data (OEI/IFR/limits/performance as relevant) from its RFM/POH for items marked aircraft-specific. For OEI tasks: the single-engine R-44 has no OEI case — a power loss is an autorotation; OEI continued-flight applies only to multi-engine test aircraft.