The Go-Around Trap
Stall/spin risk on a low-altitude turn in a weight-critical Cessna 172R — the go-around decision that kills
The scenario
Departing Venice Municipal Airport (KVNC), Venice, FL — Runway 13, landing back on Runway 13 after a local sightseeing flight. Elevation 18 ft MSL. It is a hot, humid Florida summer afternoon: OAT 32°C, dew point 24°C, altimeter 29.89. Density altitude is approximately 2,800 ft — well above field elevation. Scattered clouds at 3,500 ft, visibility 10 SM. Light and variable winds, gusting to 8 knots.
Aircraft: Cessna 172R, fuel-injected Lycoming IO-360-L2A (160 hp), fixed-pitch prop, fixed gear, steam panel (vacuum-driven attitude indicator, turn coordinator). You are solo, but the airplane is loaded near maximum gross weight: you, full fuel, and baggage. Weight and balance is within limits, but you are at the aft edge of the envelope and the high density altitude has degraded climb performance noticeably during the departure.
Pilot: you — a Private pilot, current, roughly 180 hours total. You have 25 hours in the C172R. This is your third local flight in the airplane. You did not weigh the baggage before loading; you estimated it. You did not calculate density altitude before departure; you assumed it would be fine on a local flight. You did not brief the go-around procedure.
You are on final approach to Runway 13, 400 ft AGL, descending at 62 KIAS (Vref short-field, full flaps). The runway is made. The approach is stable. Then, 200 ft AGL, you notice the landing zone is occupied by a small maintenance vehicle that was not visible from higher altitude. You have seconds to decide: land short of the vehicle, attempt to slip around it, or go around.
You decide to go around. You advance the throttle to full power, reduce flaps to 10°, and pitch up to climb. The airspeed is 55 KIAS — below Vy (79 KIAS) and dangerously close to Vs (44 KIAS clean). You are 200 ft AGL. The turn from final to downwind is ahead.
- {'label': 'Field', 'value': 'KVNC · Venice'}
- {'label': 'Runways', 'value': '4/22 · 13/31'}
- {'label': 'Elevation', 'value': '18 ft'}
- {'label': 'Aircraft', 'value': 'C172R'}
- {'label': 'Dominant phase', 'value': 'Landing / Takeoff'}
The decision
Before we enter the decision tree — what do you know about stall/spin risk in a go-around? (Pick all that apply; this records your baseline.)
What the record shows
What the NTSB files show
NTSB WPR21FA258 (2021, FATAL): A Cessna 172R on a personal flight departed overweight at high density altitude. The airplane failed to climb effectively after takeoff. The pilot attempted to return to the airport, but the airplane stalled at low altitude during the return turn. The probable cause was the pilot's failure to maintain airspeed and exceedance of the airplane's critical angle of attack, compounded by weight exceedance and high density altitude that degraded climb performance.
NTSB CEN14FA453 (2014, FATAL): A Cessna 172R on a personal sightseeing flight failed to climb after takeoff. The pilot attempted an immediate return to the airport. The airplane stalled during the return turn at low altitude. The probable cause was the pilot's failure to maintain control during the return turn, with contributing factors including inadequate preflight planning that resulted in the airplane exceeding maximum gross weight.
NTSB WPR11FA242 (2011, FATAL): A Cessna 172R stalled during a downwind turn while executing a go-around from a landing attempt. The airplane entered an unrecoverable spin. The probable cause was the pilot's failure to maintain adequate airspeed during the downwind turn, resulting in an aerodynamic stall and in-flight loss of control. Contributing factors included inadequate preflight planning and exceedance of the approved weight and balance envelope.
The common thread across all three accidents: weight exceedance, high density altitude, and a low-altitude turn at insufficient airspeed. In each case, the pilot either pitched up too aggressively or failed to lower the nose when the stall warning appeared. At 200–300 ft AGL, there is no altitude for recovery. The stall becomes impact.
These accidents occurred at other airports and in other regions — NOT at Venice Municipal Airport. However, KVNC's own dominant accident pattern (LOSS_OF_CONTROL_INFLIGHT 24.4%, FORCED_LANDING 12.2%, SPATIAL_DISORIENTATION 12.2%, HARD_LANDING 12.2%, LOSS_OF_CONTROL_GROUND 12.2%) shows that loss-of-control accidents are the field's leading risk. The high density altitude environment in summer, combined with the fixed-gear, fixed-pitch C172R's modest climb performance, makes KVNC a field where weight and airspeed discipline are non-negotiable.
The scenario is localized to KVNC to make the density altitude and the low-altitude turn environment real for you as a student here. The off-field environment around KVNC is mixed — open fields, some development, and water to the south and west. A stall at 200 ft AGL on the Runway 13 downwind (heading roughly 315°) would result in impact in or near the airport area, not a survivable forced landing.
Key lesson — In a heavy C172R at high density altitude, a go-around from a low-altitude approach is a high-risk maneuver. The airplane's climb performance is already degraded. Pitching up aggressively to climb faster will only slow the airplane down and risk a stall. The correct procedure is to accelerate to Vy (79 KIAS) in level or shallow climb BEFORE turning, then turn gently (shallow bank, less than 15°) while maintaining Vy. At 200 ft AGL, there is no altitude for stall recovery. Airspeed is your margin. Do not trade it for a steeper climb angle.
Debrief — teaching points
Weight and balance must be calculated before every flight — not estimated.
All three fatal accidents involved weight exceedance that was not caught in preflight planning. The C172R has a maximum gross weight of 2,450 lbs. At high density altitude, even a small weight exceedance degrades climb performance noticeably. You must weigh the baggage, calculate the CG, and confirm the airplane is within limits before you depart. Estimating is not acceptable. The POH has a weight and balance worksheet — use it.
Density altitude must be calculated and understood before departure.
Density altitude is the 'effective' altitude the airplane 'feels' based on temperature and pressure. At KVNC on a hot summer day (OAT 32°C), the density altitude can be 2,500–3,000 ft or higher — well above field elevation. This means the airplane climbs as if it were departing from a 2,500 ft field, not an 18 ft field. Climb performance is significantly degraded. You must calculate density altitude using the POH or a density altitude calculator and understand how it affects your airplane's performance. If density altitude exceeds your personal limits or the airplane's capability, do not depart.
A go-around from a low-altitude approach is a high-risk maneuver — brief it before you depart.
The go-around procedure should be briefed before every landing approach. The procedure for the C172R is: (1) Advance throttle to full power. (2) Reduce flaps to 10° (or retract fully if necessary). (3) Maintain pitch attitude for level flight or shallow climb — do NOT pitch up aggressively. (4) Accelerate to Vy (79 KIAS) in level or shallow climb. (5) Once Vy is established, turn gently (shallow bank, less than 15°) to downwind. The key is airspeed first, then turn. Do not turn at low airspeed.
In a go-around, maintain Vy (79 KIAS) — do not pitch up to climb faster.
Vy (best rate of climb) is the speed that gives the maximum altitude gain per unit time. Pitching up above Vy does not increase climb rate — it decreases it. The airplane slows down, the stall speed rises (especially in a turn), and the margin between airspeed and stall speed shrinks. At 200 ft AGL in a go-around, that margin is your life. Maintain Vy, turn gently, and climb to safe altitude before aggressive maneuvering.
Stall speed increases with bank angle — at 20° bank, stall speed rises roughly 10%.
In level flight, the C172R stalls at 44 KIAS (Vs, clean). In a 15° bank, stall speed rises to approximately 46 KIAS. In a 20° bank, to approximately 48 KIAS. In a 25° bank, to approximately 50 KIAS. This is why a shallow bank (less than 15°) is critical in a go-around. A steep bank at low airspeed is a stall trap. If you are turning at 55 KIAS in a 20° bank, your stall speed is 48 KIAS — only 7 KIAS margin. The buffeting will come suddenly.
Stall recovery requires lowering the nose — not pulling back.
When the stall warning appears (buffeting, mushy controls), the immediate action is to lower the nose to regain airspeed. Pulling back on the yoke will only deepen the stall. At 200 ft AGL, lowering the nose costs altitude, but it is the only way to regain airspeed and control. If you do not lower the nose, the stall will deepen and may transition into a spin. A spin at 200 ft AGL is unrecoverable.
Built from the real accident record
Scenario built from NTSB WPR21FA258 (2021 C172R stall at low altitude, overweight, high DA), CEN14FA453 (2014 C172R loss of control on return turn, overweight), and WPR11FA242 (2011 C172R stall/spin on go-around downwind, overweight). All three accidents involved weight exceedance and failure to maintain airspeed in low-altitude turns. Anonymized and localized to KVNC.
NTSB reports: WPR21FA258 · CEN14FA453 · WPR11FA242
ACS tasks: PA.I.F — Weather Information · PA.I.G — Cross-Country Flight Planning · PA.II.D — Takeoff and Climb · PA.III.D — Go-Around / Rejected Landing · PA.I.H — Human Factors · PA.VIII.D — Slow Flight, Stalls, and Spins
Relevant FARs: §91.3 · §91.9 · §91.23
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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