Full Autorotation
The most critical helicopter emergency procedure. Engine quits at altitude, you have a few seconds to convert powered flight into a controlled glide using only the rotor's stored kinetic energy and the airflow from descent. Four phases: entry, glide, flare, cushion. Practiced until reflexive, because there's no time to think when it's real.
Also called: full-touchdown autorotation, "the auto"
Phase 1 — Entry
Engine quits. Several things have to happen within seconds:
- Lower collective immediately — flat pitch on the blades preserves rotor RPM. Most rotor RPM loss happens in the first 1-2 seconds after power loss.
- Right pedal (US CCW rotor) — without engine torque, the tail rotor's leftward thrust is unbalanced. Right pedal counters.
- Establish glide attitude — pitch for best glide airspeed (typically 65 kt for training helicopters; check your POH).
- Verify rotor RPM in the green — adjust collective slightly if needed to keep RPM in the autorotation green arc. Too high or too low both reduce glide performance.
The first 3 seconds determine whether you have a flyable rotor or not. Drill the move until your hand goes down before you've finished registering the engine note change.
Phase 2 — Glide
You're now descending at roughly 1,500-2,500 fpm depending on aircraft, with rotor RPM stable in the green. Tasks during the glide:
- Pick a landing spot — within glide range, into the wind if possible, with a survivable surface (clear field, road, parking lot, even water as a last resort).
- Maneuver toward it — bank turns will increase descent rate; minimize them. Plan to arrive at the touchdown point with airspeed and altitude both in hand.
- Manage rotor RPM — small collective adjustments keep RPM in the green. Lower collective slightly to add RPM, raise slightly to bleed RPM.
- Communicate if time and workload permit — Mayday on the active frequency, squawk 7700, brief passengers.
- Pre-landing checks if there's time — fuel off, mags off (some procedures), brace passengers.
The glide phase is typically 30-90 seconds depending on entry altitude. Use it deliberately. Pilots who fixate on a touchdown spot too early often run out of altitude before they can refine the plan.
Phase 3 — Flare
At approximately 50-75 ft AGL (helicopter-dependent), apply aft cyclic to flare. The flare:
- Slows forward speed — converts forward momentum into a brief altitude gain (the helicopter "balloons" slightly).
- Slows descent rate — by trading forward speed and altitude into rotor RPM and a reduced sink.
- Preserves rotor RPM — the increased induced flow during the flare drives the rotor faster, banking energy for the cushion.
Flare timing is the hardest part of the auto. Too early: you bleed off airspeed too far above the ground, ground rush takes over, you run out of cushion. Too late: you arrive at the surface with too much forward speed and risk a tail strike or a hard landing on the skids.
The "right" flare is one where the helicopter is decelerating smoothly through 30-40 ft AGL, level at 10-15 ft, and ready for the cushion phase at 5-10 ft. Practice gets you the picture; descriptions don't.
Phase 4 — Cushion
Just before touchdown:
- Level the aircraft — if the flare ended with the nose still high, neutralize the cyclic to flat pitch attitude.
- Apply collective smoothly — convert stored rotor RPM into lift to cushion the touchdown. Not a fast yank — a smooth pull.
- Keep heading with pedals — the cushion adds collective, which without engine torque means more anti-torque demand. Right pedal as needed.
- Touch down on flat skids — rotor energy is now spent. Lower collective fully after touchdown.
- Slide if needed — if you arrived with residual forward speed, the helicopter slides. Use cyclic to maintain heading and lateral control through the slide.
The ACS standard for full autorotation: land within 200 ft of your intended point, on heading, no damage. Practiced students hit closer; checkride applicants often hit within 50 ft.
Why this is drilled so much
Engine failures happen. Flight school helicopters have engines that get more abuse than civilian-owned aircraft, and even well-maintained engines fail at single-digit-per-100,000-hour rates. Across a 30-year career, every helicopter pilot has a reasonable probability of a real engine-out event.
The full autorotation is also the maneuver most likely to be a check-pilot's "surprise" element: throttle pulled to idle without warning, often at a moment of high task load (after a max-perf takeoff, or during a confined-area scenario, or in turbulence). Recurrent training keeps the reflex sharp because the reflex perishes if not practiced.
Most training programs do "power recoveries" — entering the auto, gliding briefly, then rolling throttle back on for a powered termination — far more often than full touchdown autos. Full touchdowns wear the helicopter and are riskier; power recoveries can be done dozens of times per training cycle. Both are necessary.
Common mistakes
- Hesitating on collective entry — the most consequential error. Even a half-second of full collective without engine drive bleeds critical RPM.
- Forgetting right pedal — without it, the helicopter yaws left, complicating glide attitude.
- Picking the touchdown spot too early — committing to the first option, then having to fly back to it as conditions develop.
- Over-banking turns — increases descent rate, costs altitude.
- Flaring too high — Phase-1 students often flare 80-100 ft AGL, then run out of energy before the cushion.
- Cushioning too late — arriving at the surface still descending fast.
- Pulling collective fully early — uses up rotor RPM before touchdown, dropping hard the last few feet.