Bounce and Recover — The C182's Energy Problem
A misjudged flare in a high-performance Cessna turns a normal landing into a hard bounce. Recovery decisions at 50 feet determine the outcome.
The scenario
Departing Tampa North Aero Park Airport (X39), Tampa, FL — Runway 14, a 3,541 ft asphalt strip. Elevation 68 ft MSL. You are a commercial pilot with a high-performance endorsement, roughly 800 hours total, 120 hours in the Cessna 182 Skylane. This is your third flight in the 182 this month — you are current but not deeply experienced in the type.
It is a warm Florida afternoon in late summer: OAT 32°C, dew point 24°C, altimeter 29.89. Density altitude is approximately 2,100 ft — the airplane will perform as if it is at 2,100 ft elevation, not 68 ft. Winds are light and variable, 3–5 knots. Visibility 10 SM. A perfect VFR day, but the heat and humidity are working against climb performance and landing distance.
You are on a personal flight, solo, 1,200 lb fuel (full tanks), within CG and weight limits. The 182 is heavier and faster than the 172 you trained in — it carries more energy into the landing, and a misjudged flare or a bounced landing is more consequential. The constant-speed prop and cowl flaps add workload; you have been managing them well.
You are on a 3 nm final approach to Runway 14, descending through 800 ft AGL, airspeed 70 KIAS (best glide / approach speed), flaps 20°. The runway is made. You are stable, on speed, on glide path. The approach feels good. You begin the flare at 50 ft AGL.
Aircraft: Cessna 182 Skylane, Continental O-470 carbureted, constant-speed prop, fixed gear, steam panel, fuel selector BOTH. The airplane was last serviced 2 weeks ago; the elevator trim system was inspected and rigged during that service. You performed a thorough preflight this morning and found nothing amiss.
Pilot: you — a commercial pilot, high-performance endorsement, 800 hours total, 120 hours in type. You are current and proficient. You have landed at X39 once before, 6 months ago, in a 172. The 182 is faster and heavier; the landing characteristics are different. You are aware of this but have not fully internalized the energy difference.
- {'label': 'Field', 'value': 'X39 · Tampa North Aero Park'}
- {'label': 'Runways', 'value': '14/32'}
- {'label': 'Elevation', 'value': '68 ft'}
- {'label': 'Aircraft', 'value': 'C182'}
- {'label': 'Dominant phase', 'value': 'Takeoff / Landing'}
The decision
Before we get into the decision tree — what do you know about the Cessna 182's landing characteristics compared to the 172? (Pick all that apply; this records your baseline.)
What the record shows
What the NTSB files show
NTSB ERA21LA113 (2021): A Cessna 182 on a personal flight experienced a hard landing and runway excursion when the pilot failed to properly recover from a bounced landing. The pilot attempted to recover the landing after the first bounce by reducing power and trying to land again. The second landing was harder than the first. The nose wheel strut failed, the nose wheel separated, and the airplane nose-overed on the runway. The probable cause was the pilot's improper recovery from the bounced landing. The accident resulted in substantial damage to the airframe and injury to the pilot.
NTSB WPR20CA269 (2020): A Cessna 182 landed hard more than halfway down the runway, bounced, and the pilot delayed the go-around decision until insufficient runway remained. The airplane departed the runway and collided with trees. The probable cause was the pilot's decision to continue an unstable approach and delayed go-around. The pilot had multiple opportunities to go around but did not make the decision until it was too late.
NTSB ERA26LA009 (2025): A Cessna 182H made a hard landing on the nose gear after the pilot, while holding the jump door closed, attempted to add elevator trim for the landing flare. The elevator trim system had been improperly rigged by maintenance personnel during a recent service. The pilot did not detect the defect during the preflight inspection. The hard landing resulted in nose wheel damage. The probable cause was maintenance personnel's improper rigging of the elevator trim system and the pilot's failure to perform an adequate post-maintenance preflight inspection that would have detected the defect.
The common thread across these accidents: the Cessna 182 is heavier and faster than the 172. It carries more energy into the landing. A misjudged flare or a bounced landing is more consequential. The 182 is nose-heavy in the landing configuration — if the flare is too shallow or the airplane bounces, the nose will drop and the airplane will porpoise. A hard landing on the nose gear can damage or separate the nose wheel strut, resulting in a nose-over.
The real accidents cited above occurred at other airports and in other aircraft — NOT at Tampa North Aero Park (X39). The scenario is localized to X39 to make the runway environment real and consequential for you as a student here. The off-field environment at X39 is poor — medium development, low-density development, and wooded wetland off both runway ends. A runway excursion at X39 would result in collision with trees or structures, not open water or a clear field.
The consistent lesson: in the Cessna 182, the go-around decision must be made early — by 50 ft AGL, not after the bounce. A bounced landing at 15 ft AGL is not recoverable safely. The first bounce is the decision point: go around or accept a hard landing. Attempting to recover a bounced landing often results in a second, harder bounce and nose wheel damage. The NTSB ERA21LA113 pilot attempted recovery twice; the second attempt resulted in nose wheel separation and a nose-over. The NTSB WPR20CA269 pilot delayed the go-around until insufficient runway remained and collided with trees. The correct decision is made early.
Key lesson — The Cessna 182 is heavier and faster than the 172 — it carries more energy into the landing and is nose-heavy in the landing configuration. A misjudged flare or a bounced landing is more consequential. The go-around decision must be made early — by 50 ft AGL, not after the bounce. A bounced landing is not recoverable safely; attempting recovery often results in a harder second bounce and nose wheel damage. At X39, the off-field environment is poor — trees and structures surround the runway. A runway excursion would result in collision. The correct decision is to go around early.
Debrief — teaching points
The Cessna 182 carries more energy into the landing than the 172.
The 182 is heavier (2,950 lb gross vs. 2,450 lb for the 172) and faster (Vne 176 KIAS vs. 160 KIAS). It carries more kinetic energy into the landing. A misjudged flare or a bounced landing is more consequential. The 182 is also nose-heavy in the landing configuration — if the flare is too shallow or the airplane bounces, the nose will drop and the airplane will porpoise. Pilots transitioning from the 172 to the 182 must respect this energy difference. The landing technique is similar, but the margin for error is smaller.
The flare begins at 50 ft AGL — this is the decision point for a go-around.
If the approach is unstable at 50 ft AGL (too fast, too steep, not on glide path), the go-around decision should be made immediately. Do not attempt to salvage an unstable approach with a last-minute flare. At 50 ft AGL, you have enough altitude and airspeed to go around safely. Below 50 ft AGL, the go-around becomes marginal. Below 25 ft AGL, a go-around is risky. The first bounce is the decision point: if the airplane bounces, go around immediately. Do not attempt to recover the landing.
A bounced landing at 15 ft AGL is not recoverable safely.
When the main gear bounces off the runway, the airplane is in a pitch-up attitude at very low altitude and low airspeed. Attempting to recover by reducing power and lowering the nose often results in a second, harder bounce. The nose wheel takes a heavier impact on the second bounce. The nose wheel strut can fail or separate, resulting in a nose-over. The NTSB ERA21LA113 pilot attempted recovery twice; the second attempt resulted in nose wheel separation and a nose-over. The correct response to a bounce is an immediate go-around, not a recovery attempt.
Elevator trim is critical in the 182 — improper rigging or a trim malfunction makes a normal flare impossible.
The 182's elevator trim system is essential for managing the nose-heavy pitch attitude in the landing configuration. If the trim is rigged incorrectly or malfunctions, the pilot cannot flare normally. The NTSB ERA26LA009 accident resulted from improper rigging of the elevator trim system by maintenance personnel. The pilot did not detect the defect during the preflight inspection. After a recent maintenance service, perform a post-maintenance preflight that includes a full range-of-motion check of the elevator trim system — ensure the trim wheel moves freely and the elevator responds normally.
Density altitude at X39 is approximately 2,100 ft on a warm, humid day.
At 2,100 ft density altitude, the 182's landing distance is significantly longer than at sea level. The runway at X39 is 3,541 ft — adequate for a normal landing, but marginal if the approach is not stabilized or if the landing is long. A hard landing or a bounced landing that consumes runway can result in a runway excursion. The off-field environment at X39 is poor — trees and structures surround the runway. A runway excursion would result in collision. Plan for a longer landing distance and ensure the approach is stable and on glide path.
The go-around is not a failure — it is airmanship.
A go-around is the correct decision when the approach is unstable, the landing is bounced, or the runway is marginal. The NTSB WPR20CA269 pilot had multiple opportunities to go around but delayed the decision until insufficient runway remained. The airplane departed the runway and collided with trees. The pilot who goes around early — at 50 ft AGL or after the first bounce — makes the correct decision. A go-around costs time and fuel, but it prevents an accident.
Built from the real accident record
Scenario built from NTSB ERA21LA113 (2021 C182 hard landing / nose-wheel separation after bounced landing recovery failure), WPR20CA269 (2020 C182 unstable approach, hard landing, delayed go-around, trees), and ERA26LA009 (2025 C182H elevator trim rigging defect / hard landing on nose gear). Anonymized and localized to X39 Tampa North Aero Park.
NTSB reports: ERA21LA113 · WPR20CA269 · ERA26LA009
ACS tasks: PA.V.A — Approach and Landing · PA.V.B — Forward Slip · PA.V.C — Go-Around · PA.I.H — Human Factors · PA.II.A — Preflight Assessment
Relevant FARs: §91.3 · §91.13 · §91.103
Step through the full decision tree, make the calls, and see where each choice leads — then debrief it with your CFI.
Open the interactive scenario →All sample scenarios · More Cessna 182 Skylane scenarios · More scenarios at X39