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SAMPLE SBTLanding / Go-Around

Bounce and Go-Around in Gusty Conditions

A landing bounce, a go-around decision, and wind gusts at low altitude — the Archer's weight and energy demand precision

Piper Archer · Tampa Executive Airport (KVDF) · Private · Landing / Go-Around

The scenario

Departing Tampa Executive Airport (KVDF), Tampa, FL — Runway 23, landing attempt in gusty crosswind conditions. Elevation 22 ft MSL; the field is non-towered (CTAF). You are on a personal VFR flight, solo, in a Piper Archer PA-28-181.

Conditions: winds 210° at 14 gusting to 22 knots. Runway 23 is oriented 222° magnetic (true heading 222°). The crosswind component is roughly 10–12 knots steady, with gusts pushing 18–20 knots. Visibility 8 SM, scattered clouds at 2,500 ft, temperature 24°C, dew point 18°C. Altimeter 29.98. This is marginal crosswind territory for a low-time Archer pilot — the airplane is heavier and faster than a Warrior, and it carries more energy into the landing.

You are on final approach to Runway 23, 200 ft AGL, airspeed 66 KIAS (Vref), flaps 40°, landing gear down. The wind is gusting. You are correcting for drift with a crabbed approach. The runway is ahead; you are committed to the landing.

Aircraft: Piper Archer PA-28-181, solo, within limits. Lycoming O-360-A, 180 hp, carbureted, fixed-pitch prop, fixed gear. Fuel selector on RIGHT (you switched tanks 30 minutes ago). Steam panel, vacuum system normal.

Pilot: you — a Private pilot, current, roughly 250 hours total. You have 15 hours in the Archer; most of your experience is in a Cessna 172. You have not practiced go-arounds in crosswind conditions. You did not brief a go-around procedure before this approach.

The decision

Before we get into the decision tree — what do you already know about go-arounds in the Piper Archer? (Pick all that apply; this records your baseline.)

What the record shows

What the NTSB files show

NTSB ERA21LA139 (2021): A Piper PA-28-181 on a stage check landing attempt stalled when the student pilot flared too high and failed to execute a go-around despite stall warning and instructor command. The student pilot's improper landing flare and attempted go-around resulted in an aerodynamic stall and loss of control. Contributing factor: the flight instructor's delayed remedial action. The accident was fatal.

NTSB CEN12LA337 (2012): A Piper PA-28-181 touched down too far down the runway at high speed, porpoised, and struck trees during a shallow climb-out after an aborted landing. The probable cause was the pilot's failure to attain a proper touchdown point at the proper speed, failure to initiate a proper go-around, and the airplane's inadequate climb gradient after the aborted landing. The Archer's weight and energy demand precision — a fast or high approach floats and bites runway.

NTSB CHI08CA147 (2008): A Piper PA-28-181 on an instructional flight stalled during a go-around when the student pilot improperly raised flaps and lost airspeed. The probable cause was improper flap management during the go-around and failure to maintain airspeed. The trees were a factor in the accident.

NTSB ERA20CA072 (2020, regional precedent): A Beech 23 on an instructional flight bounced during landing in crosswind conditions, became airborne, and entered a full stall during the go-around despite full power and flaps. The probable cause was the pilot's failure to maintain control during landing and the flight instructor's delayed intervention. The teaching angle: recognize when a go-around is necessary after a bounce, maintain adequate airspeed and control inputs during the initial climb-out phase, and understand how wind gusts can compound control challenges during low-speed flight.

NTSB GAA17CA103 (2016, regional precedent): A Piper PA-28-140 encountered multiple crosswind gusts during approach and go-around; the left wing dropped and contacted the ground during the go-around, causing the aircraft to cartwheel. The probable cause was the pilot's inadequate compensation for crosswind conditions during the go-around. The teaching angle: anticipate and correct for wind gusts during go-around; maintain positive control authority and wing-level attitude when encountering variable crosswind gusts at low altitude.

The real accidents cited above occurred at other airports and in similar aircraft — NOT at Tampa Executive Airport (KVDF). KVDF's own dominant accident pattern shows LOSS_OF_CONTROL_GROUND (18.4%), HARD_LANDING (18.4%), and FORCED_LANDING (15.8%) — the field's environment and traffic patterns create their own risks. The scenario is localized to KVDF to make the off-field environment real and consequential for you as a student here: off Runway 23's departure end, the environment is pasture/hay, open water, and medium development — a forced landing there is marginal to poor.

The consistent thread across all these events: a go-around in gusty crosswind conditions at low altitude is a high-risk maneuver. The Piper Archer is heavier and faster than a Warrior — it carries more energy into the landing and requires a longer, shallower approach to avoid floating. When a bounce occurs, the decision to go around must be made immediately and the go-around must be executed with precision: full power, staged flap reduction, and absolute priority on maintaining airspeed above Vs0 (45 KIAS). Improper flap management, delayed power application, or loss of airspeed in gusty conditions results in a stall at low altitude — a fatal accident.

Key lesson — A go-around in the Piper Archer in gusty crosswind conditions at low altitude is a high-risk maneuver. The Archer's weight and energy demand precision: a fast or high approach floats and bites runway. If a bounce occurs, commit to the go-around immediately, apply full power, stage flap reduction (do not raise all flaps at once), and maintain airspeed above Vs0 (45 KIAS) at all costs. A gust that drops a wing when airspeed is low results in a stall at 50 ft AGL — a fatal accident. Off Runway 23 at KVDF, the off-field environment is marginal; there is no open field to land in. Know your crosswind limits and your go-around procedure before you line up on final approach.

Debrief — teaching points

The Archer is heavier and faster than a Warrior — it carries more energy into the landing.

The Piper Archer PA-28-181 is a 180 hp, low-wing airplane with a maximum gross weight of 2,550 lbs. It is significantly heavier and faster than a Piper Warrior. A fast or high approach in the Archer floats further down the runway and bites harder on touchdown. A bounce in the Archer is more energetic than in a Warrior. Know the Archer's approach characteristics: a shallower, longer approach is required to land on the first third of the runway. If you find yourself high or fast on final, go around — do not try to salvage a bad approach with a hard landing or a bounce.

A bounce is a go-around trigger — commit immediately.

When the airplane bounces, you have a decision window of 3–4 seconds: land again or go around. The Archer's energy means a second landing attempt is risky — you may bounce again or land hard. A go-around is the safer choice. But a go-around at 20 ft AGL in gusty conditions is also risky. The key is to commit to the decision immediately: if you decide to go around, apply full power at once and establish a climb. Hesitation or a delayed power application invites a stall.

Full power immediately — delay in adding power during a low-airspeed go-around results in a stall.

When you initiate a go-around, advance the throttle to full power immediately. At 20 ft AGL with flaps 40° and airspeed 55 KIAS, you are at the edge of a stall. The engine is your only tool to generate lift and climb. A delayed power application means airspeed continues to decay — and a stall at 20 ft AGL is fatal. Full power now; manage the flaps and pitch after you have established a climb.

Stage flap reduction — do not raise all flaps at once.

When you raise flaps during a go-around, do it in stages: 40° → 20° → 0°. Raising flaps all at once causes a sudden loss of lift and a pitch-down moment that can be difficult to control at low altitude with low airspeed. Staging the reduction allows you to manage the pitch change and maintain airspeed. At 20 ft AGL with airspeed 55 KIAS, raising flaps to 0° in one motion can result in a pitch-down that you over-correct with back pressure — and a stall.

Maintain airspeed above Vs0 (45 KIAS) — it is the priority.

Vs0 for the Archer is 45 KIAS (landing configuration, flaps 40°). As you raise flaps, Vs0 decreases, but during the transition (flaps 40° → 20° → 0°) the stall speed is changing. Maintain a target airspeed of at least 60 KIAS during the go-around to ensure a margin above stall. If airspeed decays below 55 KIAS with flaps extended, a gust that drops a wing will result in a stall. Pitch attitude and back pressure are secondary to airspeed — if airspeed is decaying, lower the nose and accept a shallower climb.

Crosswind gusts at low altitude compound the risk — anticipate and correct aggressively.

A crosswind gust during a go-around can drop a wing and disrupt your pitch attitude. At 50 ft AGL with airspeed 55 KIAS, a 10-knot gust can drop the wing and induce a stall. Anticipate gusts: if the wind is gusty, be ready to apply aileron and rudder to level the wing. Do not wait for the wing to drop — correct proactively. And maintain a shallow pitch attitude (nose slightly up, not steeply pitched) so that if a gust drops the wing, you have room to apply back pressure without inducing a secondary stall.

Brief your go-around procedure before the approach — do not improvise at 20 ft AGL.

Before you begin the approach, brief yourself on the go-around procedure: full power, flaps 20° at 50 ft AGL, flaps 0° at 100 ft AGL, climb to pattern altitude. Write it down if you need to. When the bounce happens and you are at 20 ft AGL, you will not have time to think — you will execute the procedure you briefed. Improvisation at low altitude in gusty conditions is a recipe for a stall.

Built from the real accident record

Scenario built from NTSB ERA21LA139 (2021 PA-28-181 stall during go-around), CEN12LA337 (2012 PA-28-181 aborted landing / tree strike), ERA09CA322 (2009 PA-28-181 directional control loss), CHI08CA147 (2008 PA-28-181 stall during go-around), and regional precedents ERA20CA072 (Beech 23 go-around stall in crosswind), ATL07CA048 (Mooney M20J go-around stall), GAA17CA103 (Piper PA-28-140 crosswind go-around upset), MIA08CA179 (Cessna 172SP wind-induced go-around loss of control). Anonymized and localized to KVDF.

NTSB reports: ERA21LA139 · CEN12LA337 · ERA09CA322 · CHI08CA147 · ERA20CA072 · ATL07CA048 · GAA17CA103 · MIA08CA179

ACS tasks: PA.II.D — Approach and Landing · PA.II.E — Go-Around / Rejected Landing · PA.I.F — Weather Information · PA.I.H — Human Factors · PA.IX.C — Emergency Approach and Landing

Relevant FARs: §91.3 · §91.13 · §91.103

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