Steep Turn to Final — Clearwater Air Park
Uncoordinated descent, critical angle of attack, and a parachute decision at 400 feet AGL
The scenario
Departing Clearwater Air Park (KCLW), Clearwater, FL — Runway 16, a local training flight in the Cirrus SR20. Elevation 71 ft MSL; the runway is 4,108 ft, asphalt. You are a Private pilot with roughly 120 hours total time, 45 hours in the SR20. This is a familiar airplane and a familiar airport.
It is a warm Florida afternoon in late May: OAT 31°C, altimeter 29.89, density altitude approximately 2,100 ft. The wind is from 180° at 12 knots, gusting to 18 — a crosswind for Runway 16 (true heading 155°), but within limits. Visibility 10 SM, scattered clouds at 3,500 ft. A typical Florida summer day: hot, humid, and the density altitude is noticeably higher than field elevation.
You have completed a local practice area flight — slow flight, steep turns, and a few touch-and-goes. You are returning to KCLW for a full-stop landing on Runway 16. You are at 1,500 ft AGL, 8 miles northeast of the field, heading 155° (inbound). The SR20 is at 96 KIAS (best glide speed), power is at 1,500 RPM, and you are descending at 500 fpm. Fuel is ample; the airplane is within limits.
Aircraft: Cirrus SR20, solo, 2,800 lb gross weight, within CG. Constant-speed prop, fuel-injected Continental IO-360-ES, glass panel (Avidyne Perspective), CAPS parachute system armed and ready. The airplane is airworthy; nothing was written up.
Pilot: you — a Private pilot, current, roughly 120 hours total, 45 hours SR20. You have done a few crosswind landings in the SR20, but today's 12-knot crosswind gusting to 18 is at the upper end of your comfort zone. You have not flown in high density altitude conditions before. You did not brief a go-around decision or a CAPS decision before this approach.
- {'label': 'Field', 'value': 'KCLW · Clearwater Air Park'}
- {'label': 'Runways', 'value': '16/34'}
- {'label': 'Elevation', 'value': '71 ft'}
- {'label': 'Aircraft', 'value': 'SR20'}
- {'label': 'Dominant phase', 'value': 'Landing / Approach'}
The decision
Before we get into the decision tree — what do you know about stall/spin risk in the SR20, and about CAPS? (Pick all that apply; this records your baseline.)
What the record shows
What the NTSB files show
NTSB WPR20LA152 (2020, FATAL): A Cirrus SR20 flown by a student pilot on a solo cross-country flight stalled during a steep descending turn to final approach at low altitude. The pilot exceeded the aircraft's critical angle of attack during the turn, resulting in an aerodynamic stall and loss of control. The parachute was deployed too late — at approximately 400 ft AGL — to inflate and slow the descent enough for a survivable impact. The probable cause was the pilot's exceedance of the critical angle of attack during a steep and descending turn to final approach.
NTSB WPR12FA235 (2012, FATAL): A Cirrus SR20 on a cross-country flight to Bryce Canyon stalled while maneuvering over mountainous terrain at high density altitude. The pilot failed to maintain sufficient airspeed while maneuvering a heavily loaded aircraft in a high-DA environment and descended inverted into terrain. The probable cause was the pilot's failure to maintain sufficient airspeed and airplane control while maneuvering, with contributing factors including lack of experience in high-density-altitude operations.
NTSB GAA19CA099 (2018): A Cirrus SR20 on a training flight stalled during a go-around when the student pilot aggressively pitched up after being instructed to abort the landing. The student exceeded the critical angle of attack during the go-around, resulting in an aerodynamic stall. The flight instructor delayed remedial action. The probable cause was the student pilot's exceedance of the critical angle of attack during a go-around.
NTSB GAA17CA253 (2017): A Cirrus SR20 bounced during a hard landing in crosswind conditions and entered an uncontrolled roll during go-around when the student failed to compensate for wind. The probable cause was the student pilot's failure to adequately compensate for crosswind conditions during a go-around, with the flight instructor's delayed remedial action as a contributing factor.
The real accidents cited above occurred at other airports and in other aircraft types — NOT at Clearwater Air Park. KCLW has its own accident history (forced landing, loss of control in flight, gear-up landing, hard landing, and fuel starvation are the dominant patterns), but these specific stall/spin events happened elsewhere. The scenario is localized to KCLW to make the off-field environment real and consequential for you as a student here.
The consistent thread across all these events: the SR20's stall/spin risk is acute at low altitude during approach and landing, especially in crosswind conditions, high-density-altitude environments, or when the pilot is distracted or behind the airplane. The SR20 is NOT certified for intentional spin recovery by control inputs — CAPS is the primary recovery tool. Deploying CAPS requires altitude: roughly 1,000 ft AGL is the minimum safe altitude for CAPS deployment to result in a survivable impact. Below that, the parachute may not have enough time to fully inflate and slow the descent. The decision to deploy CAPS must be made early, not as a last resort at 300 ft AGL.
Off Runway 16's approach end at KCLW, the off-field environment is dense development — buildings, roads, low-density residential areas. A stall/spin at low altitude in this environment is unforgiving. The runway itself is 4,108 ft long — plenty of length for a stable approach and landing. The accident happens not because the runway is too short, but because the approach was unstable, the turn was too steep, and the angle of attack was too high.
Key lesson — In the SR20, maintain a stable approach at or above Vref (80 KIAS) with the angle of attack in the green arc. Avoid steep uncoordinated turns at low altitude. If you find yourself in a stall/spin situation below 1,000 ft AGL, deploy CAPS immediately — do not attempt control-input recovery. The SR20 is not certified for intentional spin recovery. CAPS is your only reliable recovery tool, and it requires altitude. Know your crosswind limits and personal minimums before you line up on final approach. If the approach is unstable or the crosswind is beyond your comfort zone, go around. A go-around at 1,500 ft AGL is always better than a stall at 500 ft AGL.
Debrief — teaching points
The SR20 is NOT certified for intentional spin recovery by control inputs.
Unlike some general-aviation aircraft, the Cirrus SR20 is not certified for intentional spin recovery. The POH does not provide spin-recovery procedures. If the airplane enters a stall or spin, the primary recovery tool is CAPS — the whole-airframe parachute. Attempting to recover from a spin by control inputs (opposite rudder, forward stick) is not reliable and wastes altitude. CAPS is the correct response to an unrecoverable stall or spin.
CAPS requires altitude to work — roughly 1,000 ft AGL is the minimum safe deployment altitude.
The CAPS parachute slows the descent to roughly 1,500 fpm, but it does not stop the descent. At 1,000 ft AGL, the parachute has time to fully inflate and slow the aircraft enough for a survivable impact. Below 500 ft AGL, the parachute may not have enough time to fully inflate before impact. Deploying CAPS at 300 ft AGL is a last resort, not a reliable recovery. The decision to deploy CAPS must be made early, when you recognize an unrecoverable stall or spin situation.
The angle-of-attack indicator is your primary stall-prevention tool.
The SR20's angle-of-attack indicator shows the margin to stall in real time. Keep the indicator in the green arc during approach and landing. If the indicator enters the yellow arc, you are approaching the stall — reduce back-pressure immediately to lower the angle of attack. The angle-of-attack indicator is more reliable than airspeed alone, especially in gusty or crosswind conditions where airspeed can fluctuate.
Steep uncoordinated turns at low altitude are the classic stall/spin setup.
A steep turn (bank angle > 25°) combined with back-pressure to maintain altitude increases the angle of attack. If the turn is also uncoordinated (the ball is deflected), the stall speed increases further. At low altitude (< 1,000 ft AGL), a stall in a steep uncoordinated turn is unrecoverable by control inputs — CAPS is your only option. Avoid steep turns on approach and landing. Keep bank angles shallow (< 15°) and maintain coordination (keep the ball centered).
High density altitude increases the true airspeed for a given indicated airspeed — the airplane stalls at a HIGHER indicated airspeed.
On a hot day with high density altitude (like KCLW at 2,100 ft DA), the true airspeed is higher than the indicated airspeed. This means the airplane stalls at a higher indicated airspeed than it would at sea level. For example, at 2,100 ft DA, the stall speed might be 58 KIAS instead of 56 KIAS. This is a small difference, but it matters at low altitude. Know the density altitude before you depart, and adjust your approach speeds accordingly.
Crosswind limits are personal minimums — know yours and do not exceed them.
The SR20 has a demonstrated crosswind capability, but that does not mean you should fly it at that limit on every approach. Your personal crosswind limit depends on your experience, the airplane's condition, and the runway length. A 12-knot crosswind gusting to 18 is within the airplane's capability but may be beyond your comfort zone. If the approach is unstable or the crosswind is pushing you around, go around. A go-around is not a failure — it is good airmanship.
Built from the real accident record
Scenario built from NTSB WPR20LA152 (2020 SR20 stall on final approach, CAPS deployment too late), WPR12FA235 (2012 SR20 stall during maneuvering in high-DA environment), GAA19CA099 (2018 SR20 stall during go-around, student pitch-up), and GAA17CA253 (2017 SR20 crosswind go-around loss of control). Localized to Clearwater Air Park (KCLW).
NTSB reports: WPR20LA152 · WPR12FA235 · GAA19CA099 · GAA17CA253
ACS tasks: PA.I.F — Weather Information · PA.II.C — Takeoff and Departure · PA.III.C — Approach and Landing · PA.III.D — Go-Around / Rejected Landing · PA.IV.C — Stall Prevention · PA.V.A — Aeronautical Decision Making
Relevant FARs: §91.3 · §91.13 · §91.119
Step through the full decision tree, make the calls, and see where each choice leads — then debrief it with your CFI.
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