Bounced Landing, Nose-Heavy Flare
A Cessna 182's energy and pitch authority demand precision on short final — misjudge the flare and the nose drops hard
The scenario
Departing Peter O Knight Airport (KTPF), Tampa, FL — Runway 22, a 3,583 ft asphalt strip at 8 ft MSL. Elevation is essentially sea level; density altitude is moderate (roughly 1,200 ft DA). You are a Commercial pilot with 850 hours total, 120 hours in the Cessna 182 Skylane, and you hold a high-performance endorsement. This is your second flight in the 182 from this field.
It is a clear VFR afternoon: OAT 26°C, altimeter 29.98, wind 180° at 8 kt gusting to 12 kt. Runway 22 is oriented 217° true; the wind is nearly aligned, a slight left crosswind (about 4 kt). Visibility 10 SM. Smooth air. A textbook landing day — except for one thing: the airplane was returned from maintenance yesterday. The elevator trim was rigged during a control-cable inspection. You performed a preflight and a short functional test, but you did not fly the airplane before this flight.
You are on short final to Runway 22, 400 ft AGL, 70 KIAS (Vref, power-off approach speed for short-field landing). The runway is made. Flaps are full (40°). Prop is set to high RPM (full forward). Cowl flaps are open for cooling. You are configured for a short-field landing — the 182 is nose-heavy in this configuration, and the flare requires deliberate elevator back-pressure to arrest the descent and touch down on the main gear first.
You begin the flare at 20 ft AGL. You apply back-pressure on the yoke to raise the nose and slow the descent. The elevator feels normal — responsive. But as you continue the flare, the nose does not come up as much as you expect. You are sinking faster than you anticipated. The main gear touches down at 50 ft down the runway, but the descent rate is high — you feel the impact. The nose gear follows hard. The airplane bounces.
Aircraft: Cessna 182 Skylane, solo, within limits. Continental O-470 carbureted, constant-speed prop, cowl flaps, fixed gear, steam panel. The elevator trim was rigged yesterday; you did not detect any issue in the preflight or the functional test.
Pilot: you — a Commercial pilot, 850 hours total, 120 hours in type, high-performance endorsement current. You are familiar with the 182's nose-heavy pitch characteristics and the need for deliberate elevator back-pressure on landing. You did not apply full back-pressure on the flare because you did not anticipate the elevator authority to be compromised.
- {'label': 'Field', 'value': 'KTPF · Peter O Knight'}
- {'label': 'Runways', 'value': '4/22 · 18/36'}
- {'label': 'Elevation', 'value': '8 ft'}
- {'label': 'Aircraft', 'value': 'C182'}
- {'label': 'Dominant phase', 'value': 'Landing / Approach'}
The decision
Before we get into the decision tree — what do you know about the Cessna 182's landing characteristics and hard-landing recovery? (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 did not apply sufficient back-pressure during the flare, resulting in a hard landing. The airplane bounced, and the pilot did not recover from the bounce — the nose wheel separated and the airplane nose-overed. The probable cause was the pilot's improper recovery from the bounced landing. The accident was fatal.
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 the delayed go-around decision. The pilot and passenger were seriously injured.
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. Maintenance personnel had improperly rigged the elevator trim system during a control-cable inspection. The pilot and maintenance personnel failed to perform adequate post-maintenance and preflight inspections that would have detected the defect. The probable cause was maintenance personnel's improper rigging of the elevator trim system, with contributing factors being the failure to perform post-maintenance and preflight inspections.
The real accidents cited above occurred at other airports and in other aircraft — NOT at Peter O Knight Airport. KTPF has its own accident history (see field dominant patterns: FORCED_LANDING 19.4%, LOSS_OF_CONTROL_INFLIGHT 16.7%, LOSS_OF_CONTROL_GROUND 11.1%, DITCHING 11.1%, STALL_SPIN 8.3%), but these specific events happened elsewhere. The scenario is localized to KTPF to make the off-field environment real and consequential for you as a student here.
The consistent thread across all these events: the Cessna 182 is nose-heavy on landing, and the flare requires deliberate, sustained back-pressure to raise the nose and touch down on the main gear first. A hard landing or a bounce requires immediate, full back-pressure to recover — hesitation or inadequate back-pressure results in a second hard landing, nose wheel separation, and potential nose-over. Additionally, post-maintenance inspections are critical: improper elevator trim rigging can compromise the elevator authority available during the flare, making the hard landing more likely.
Off Runway 22's departure end (heading 217°), the off-field environment is open water — Tampa Bay. An engine failure or a marginal climb-out with full flaps in this configuration could result in a ditching. The decision to retract flaps to 10° immediately during a go-around is not optional — it is the difference between a successful climb-out and a water landing.
Key lesson — The Cessna 182's nose-heavy pitch characteristics demand deliberate, sustained back-pressure during the flare. A hard landing or bounce requires immediate full back-pressure to recover — hesitation results in a second hard landing and potential nose wheel separation. Additionally, post-maintenance inspections and test flights are essential: improper elevator trim rigging can compromise the elevator authority available during the flare. Off Runway 22 at KTPF, the off-field environment is open water — a marginal climb-out with full flaps is a ditching waiting to happen.
Debrief — teaching points
The Cessna 182 is nose-heavy on landing — the flare requires deliberate, sustained back-pressure.
The C182's heavier, faster airframe and nose-heavy pitch characteristics mean that the flare requires deliberate, sustained back-pressure on the yoke to raise the nose and touch down on the main gear first. A shallow flare or inadequate back-pressure results in a hard landing on the nose gear. The elevator authority is available — you must use it. Do not be timid on the flare. Apply full back-pressure and hold it through touchdown.
A bounce requires immediate, full back-pressure — not power, not a go-around, but back-pressure.
If the airplane bounces on landing, the correct recovery is to apply full back-pressure on the yoke and hold it. This arrests the descent and allows the airplane to settle onto the runway more gently. Do NOT add power — that will only increase the bounce. Do NOT attempt a go-around mid-bounce — that is unstable and dangerous. Full back-pressure is the correct response. If the bounce is severe or the recovery is not working, then consider a go-around, but the first response is always full back-pressure.
A go-around decision must be made EARLY — delaying it past mid-runway leaves insufficient runway for a safe climb-out.
If the approach is unstable or the landing is clearly going wrong, the go-around decision must be made early — ideally before you reach mid-runway. Delaying the decision until you are halfway down the runway leaves insufficient runway for a safe climb-out, especially with full flaps and a nose-heavy airplane. The C182 needs runway to climb out. Make the decision early and commit to it.
In a go-around, retract flaps to 10° immediately — full flaps are not a climb configuration.
Full flaps (40°) are a landing configuration, not a climb configuration. In a go-around, retract flaps to 10° (Vfe 140 KIAS) immediately to maximize climb rate. The C182 with full flaps has marginal climb performance, especially at low altitude. Retract flaps immediately and the climb rate improves dramatically. This is not optional — it is the difference between a successful climb-out and a water landing.
Post-maintenance inspections and test flights are essential — a preflight alone may not detect rigging errors.
After any maintenance involving control cables or trim rigging, a functional test on the ground and a test flight before normal operations are essential. A preflight walk-around may not detect improper trim rigging or cable tension issues. A functional test on the ground (moving the trim through its full range and checking the feel) and a test flight (confirming the elevator authority and trim feel in flight) will reveal problems that a preflight alone will miss. Do not skip this step.
Elevator trim affects the force required to hold a pitch attitude, but does not change the maximum pitch authority available.
Improper elevator trim rigging can make the elevator feel sluggish or require excessive force to move, but full back-pressure on the yoke will still raise the nose. However, if the trim is severely out of specification, the elevator may be jammed or the cable may be over-tensioned, which can compromise the elevator authority. This is why post-maintenance inspections are critical. If the elevator feel is abnormal, do not fly the airplane — get it inspected.
Built from the real accident record
Scenario built from NTSB ERA21LA113 (2021 C182 hard landing / nose-wheel separation after bounced landing), WPR20CA269 (2020 C182 hard landing / delayed go-around decision), and ERA26LA009 (2025 C182H hard landing from improper elevator trim rigging). Localized to Peter O Knight Airport (KTPF), Tampa, FL.
NTSB reports: ERA21LA113 · WPR20CA269 · ERA26LA009
ACS tasks: PA.VII.A — Normal Approach and Landing · PA.VII.B — Forward Slip · PA.VII.C — Go-Around / Rejected Landing · PA.IX.C — Emergency Approach and Landing · PA.I.H — Human Factors
Relevant FARs: §91.3 · §91.13 · §61.31
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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