Steep Turn to Final — Sarasota Bradenton
Uncoordinated descent, critical angle of attack, and a low-altitude stall spiral — the parachute is your last resort, and it must deploy in time
The scenario
Departing Sarasota Bradenton International Airport (KSRQ), Sarasota/Bradenton, FL — Runway 14, a 9,500 ft asphalt runway heading 134° true. Elevation 30 ft MSL. You are on a local training flight in a Cirrus SR20, solo, within weight and balance limits.
It is a warm Florida afternoon in late July: OAT 32°C, dew point 24°C, altimeter 29.89 inHg. Density altitude is approximately 2,200 ft — the airplane will perform as if it is 2,200 ft higher than field elevation. Scattered clouds at 3,500 ft, visibility 10 SM. Light and variable winds, gusting to 8 knots. KSRQ tower is active (0600–0000 local); you are in Class C airspace with a 4,000 ft MSL ceiling.
You have completed a series of practice approaches and go-arounds. On your final approach to Runway 14, you are at 800 ft AGL, on a 3° glide slope, configured for landing: flaps 50%, power reduced, airspeed 85 KIAS (slightly above Vref 80 KIAS for a margin). The runway is ahead and below. The tower has cleared you to land.
At 600 ft AGL, you notice the wind has shifted slightly — it now has a left crosswind component of roughly 6–8 knots. The airplane is drifting left of the runway centerline. You correct with a shallow left turn to re-center, adding a touch of back pressure to maintain the glide slope. The turn is not steep — perhaps 15–20° of bank — but it is uncoordinated: you are turning with aileron input alone, without adequate rudder trim or coordination.
Aircraft: Cirrus SR20, solo, full fuel, within limits. 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 or Commercial pilot, current, roughly 300–400 hours total. You have 50–75 hours in the SR20. You are familiar with the airplane's handling but have not recently practiced slow-speed maneuvering or stall recovery. You have never deployed the CAPS parachute in flight. The crosswind correction felt routine — you did not consciously think about coordination or angle of attack.
- {'label': 'Field', 'value': 'KSRQ · Sarasota Bradenton'}
- {'label': 'Runways', 'value': '4/22 · 14/32'}
- {'label': 'Elevation', 'value': '30 ft'}
- {'label': 'Aircraft', 'value': 'SR20'}
- {'label': 'Dominant phase', 'value': 'Takeoff / Landing'}
The decision
Before we get into the decision tree — what do you already know about stall risk in the Cirrus SR20 on approach? (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. The CAPS parachute was deployed, but at 300 ft AGL — too late for adequate parachute inflation and deceleration before impact. The accident resulted from the pilot's failure to maintain sufficient airspeed and coordination during the approach turn.
NTSB WPR12FA235 (2012, fatal): A Cirrus SR20 on a cross-country flight 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 density altitude environment. The airplane descended inverted into terrain. Contributing factors included the pilot's 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. The flight instructor's delayed remedial action contributed to the accident.
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 student pilot's failure to adequately compensate for crosswind and the flight instructor's delayed remedial action were contributing factors.
The off-field environment off Runway 14's approach end (heading 134°) at KSRQ is dense development — buildings, roads, and structures. A stall spiral at 300–400 ft AGL over this terrain is survivable only under the parachute. The real accidents cited above occurred at other airports and in different terrain — NOT at KSRQ. However, the stall/spin mechanism is identical: uncoordinated turn, excessive angle of attack, low altitude, and delayed recognition.
The consistent thread across all these accidents: the Cirrus SR20 is a high-performance, slippery airplane with a constant-speed prop and high best-glide speed (96 KIAS). Energy management is unforgiving. A shallow turn on final approach, if uncoordinated, can exceed the critical angle of attack in seconds. The stall warning (if monitored) is the first alert. The parachute is the last resort — but it must deploy above 500 ft AGL to be effective. The primary defense is coordination, airspeed awareness, and recognition of the approach to stall before the spiral develops.
Key lesson — In the Cirrus SR20, a crosswind correction on final approach must be coordinated — aileron and rudder together. An uncoordinated turn increases the angle of attack and can cause a stall at a lower airspeed than a coordinated turn. At 600 ft AGL on final approach, the stall margin is thin. Recognize the sluggish feel or stall warning as an immediate signal to lower the nose and coordinate the turn. If a stall spiral develops, deploy CAPS immediately — do not wait for the spiral to fully develop. CAPS is most effective above 500 ft AGL; deployment below 300 ft AGL may not provide adequate deceleration before impact.
Debrief — teaching points
Stall speed increases in a turn — even a shallow one.
The stall speed in a turn is higher than the stall speed in level flight. The increase is proportional to the cosine of the bank angle. A 20° bank increases stall speed by roughly 6%; a 30° bank increases it by roughly 15%. In the SR20, Vs0 (stall, landing configuration) is 56 KIAS. In a 20° coordinated turn, the stall speed is roughly 59 KIAS. In a 30° turn, it is roughly 64 KIAS. On final approach at 85 KIAS, a 30° bank leaves only a 21 KIAS margin — and that margin shrinks if the turn is uncoordinated.
An uncoordinated turn increases angle of attack and reduces stall margin.
In an uncoordinated turn (aileron without adequate rudder), the airplane's nose is pulled up relative to the flight path. This increases the angle of attack. The stall speed in an uncoordinated turn can be 2–4 KIAS higher than in a coordinated turn of the same bank angle. A crosswind correction on final approach must be coordinated — aileron and rudder together — to avoid exceeding the critical angle of attack. The SR20's side-yoke and constant-speed prop require active, coordinated control inputs.
The stall warning is your first alert — recognize it and act immediately.
The SR20's stall warning (buffet) is the first indication that you are approaching the critical angle of attack. If you feel the buffet on final approach, immediately lower the nose to reduce angle of attack and coordinate the turn. Do not continue the descent or add back pressure — both increase angle of attack further. The stall warning is not optional; it is a command to lower the nose.
CAPS is the primary recovery tool for an unrecoverable stall in the SR20 — but it must deploy early.
The Cirrus SR20 is not certified for intentional spin recovery by control inputs. If a stall spiral develops, CAPS is your only recovery option. However, CAPS is most effective above 500 ft AGL. At 500 ft AGL with a descent rate of 17 ft/sec under the parachute, you have roughly 30 seconds before impact. At 300 ft AGL, you have roughly 18 seconds. The parachute must deploy early — before the spiral fully develops — to provide adequate deceleration. Deploy CAPS at the first sign of an unrecoverable stall, not as a last resort at 200 ft AGL.
Density altitude affects the SR20's performance — especially on approach.
At KSRQ on a warm July afternoon, density altitude is roughly 2,200 ft. The SR20 performs as if it is 2,200 ft higher than field elevation. This affects climb performance, descent rate, and landing distance — but it also affects stall speed and energy management on approach. The airplane will float longer, require more runway, and be slower to respond to control inputs. Be aware of density altitude and adjust your approach accordingly: longer final, lower descent rate, and extra margin on airspeed.
A go-around is always defensible — do not force an unstable approach to landing.
If the approach is not stable by 500 ft AGL (on glide slope, on centerline, at target airspeed, coordinated), execute a go-around. A go-around is not a failure; it is a sign of good judgment. The SR20's constant-speed prop and high best-glide speed make go-arounds straightforward: advance the throttle, reduce flaps to 20%, and climb back to pattern altitude. A stable approach is always worth the extra circuit.
Built from the real accident record
Scenario built from NTSB WPR20LA152 (2020 SR20 stall on final approach, parachute deployed too late), WPR12FA235 (2012 SR20 stall during maneuvering in high density altitude), GAA19CA099 (2018 SR20 stall during go-around), and GAA17CA253 (2017 SR20 uncontrolled roll during go-around). Localized to Sarasota Bradenton International Airport (KSRQ).
NTSB reports: WPR20LA152 · WPR12FA235 · GAA19CA099 · GAA17CA253
ACS tasks: PA.II.F — Approach and Landing · PA.II.E — Go-Around / Rejected Landing · PA.VIII.D — Stall Prevention · PA.VIII.E — Spin Awareness · PA.I.H — Human Factors
Relevant FARs: §91.3 · §91.13 · §91.303
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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