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SAMPLE SBTClimb / Cruise

Engine Roughness Over Clearwater

Carburetor ice, partial power loss, and a non-towered field surrounded by development — a forced-landing decision in real time

Cessna 172N · Clearwater Air Park (KCLW) · Private · Climb / Cruise

The scenario

Departing Clearwater Air Park (KCLW), Clearwater, FL — Runway 34, climbing out on a 335° heading. Elevation 71 ft MSL; the runway is essentially at sea level. You are on a local VFR flight, solo, full fuel, within limits.

It is a hazy Florida afternoon in late spring: OAT 29°C, dew point 23°C, altimeter 29.92. Scattered clouds at 2,500 ft, light rain shower two miles to the northeast. Visibility 8 SM. Classic Gulf Coast conditions — warm, moist, and exactly the environment the FAA icing probability chart marks as 'serious icing at glide power, moderate icing at cruise power.' KCLW is non-towered (CTAF 122.8); you are in Class G airspace below 3,000 ft MSL. Above 3,000 ft MSL, you are in the overlying Tampa Class B airspace (3,000 MSL → 10,000 MSL).

You are 500 ft AGL, climbing through 75 KIAS (near Vy of 73 KIAS), heading 335°, when the engine begins to run rough. Power is noticeably down — the tachometer is dropping. The off-field environment ahead (Runway 34 climb-out) is low-density development, medium development, and open developed areas (parks, large lots) — not ideal for a forced landing, but better than dense urban. KCLW's own runway is behind you and to the left.

Aircraft: Cessna 172N, solo, full fuel, within limits. Carbureted Lycoming O-320, fixed-pitch prop, steam panel, fuel selector on BOTH. Nothing was written up; the airplane was airworthy at departure. You did not apply carburetor heat during the run-up because the engine ran smoothly. You did not apply it after takeoff because you were heads-down on the climb.

Pilot: you — a Private pilot, current, roughly 200 hours total. You are familiar with KCLW but have not trained extensively in forced-landing site selection. You know the field is surrounded by development, but you have not studied the off-field options in detail.

The decision

Before we get into the decision tree — what do you already know about carburetor ice in the C172N and forced-landing site selection? (Pick all that apply; this records your baseline.)

What the record shows

What the NTSB files show

NTSB CEN24LA362 (2024): A Cessna 172N encountered light rain and carburetor ice at 1,800 ft AGL. The engine ran rough and lost power. The probable cause was carburetor ice formation in conditions conducive to serious icing, with insufficient time and altitude for carburetor heat to clear the accumulated ice. The pilot had not applied carburetor heat proactively in conditions that clearly warranted it.

NTSB CEN14LA276 (2014): A Cessna 172N on a cross-country flight experienced engine roughness and power loss at cruise altitude in conditions conducive to carb icing. The pilot made a forced landing on an island; the aircraft nosed over in soft sand. The pilot survived. The probable cause could not be determined due to premature aircraft release — but the conditions and symptoms are consistent with carburetor ice.

NTSB ANC26LA001 (2025): A Cessna 172 on an instructional flight experienced progressive engine power loss during training maneuvers despite carburetor heat application. The pilot made a forced landing on a road; the aircraft struck a rock during landing roll and nosed over. Atmospheric conditions indicated serious icing conditions in pressure-type carburetors — even with carb heat applied, the ice accumulation was too heavy and too rapid.

NTSB CEN14LA374 (2014): A Cessna 172N on a personal local flight experienced partial engine power loss during cruise and made a forced landing to a cornfield. The accident resulted from partial loss of engine power due to failure of the dual magneto system caused by loose mounting screws, with improper maintenance during the annual inspection as a contributing factor. Not all engine roughness is carburetor ice — magneto failure, fuel contamination, and mechanical problems are also in the differential diagnosis.

NTSB WPR14LA099B (2014): A Piper PA-24 on a personal cross-country flight experienced partial engine power loss during initial climb due to water-contaminated fuel. The accident resulted from the pilot's failure to sump the fuel tanks during preflight, allowing water contamination to cause engine failure. Fuel sumping is a non-negotiable preflight step — water in the fuel tank is invisible until it reaches the engine.

The real accidents cited above occurred at other airports and in other aircraft — NOT at Clearwater Air Park (KCLW). KCLW has its own accident history (dominant pattern: forced landing 22.2%, loss of control 18.5%, gear-up landing 18.5%, hard landing 11.1%, fuel starvation 11.1%), but these specific events happened elsewhere. The scenario is localized to KCLW to make the off-field environment real and consequential for you as a student here.

The consistent thread across all these events: carburetor ice in the C172N is insidious. It builds gradually, the first symptom is roughness and a dropping tachometer (not a dramatic power cut), and by the time it is obvious, it may be too late for a comfortable recovery. The fix — full carburetor heat, immediately, at the first sign of roughness in conducive conditions — is simple. The failure is always a delay.

Key lesson — In warm, moist Gulf Coast air, the C172N's carbureted O-320 can accumulate serious carburetor ice even at cruise power and above-freezing temperatures. Apply full carburetor heat at the first sign of engine roughness or unexplained RPM loss. At low altitude over development, the decision window is measured in seconds — not minutes. Off Runway 34 at KCLW, the off-field environment is low-density and medium development with some open areas — a forced landing there is possible but hazardous. Know your forced-landing sites before you need them.

Debrief — teaching points

Carburetor ice forms in conditions you would not expect.

The FAA icing probability chart shows 'serious icing at glide power' at temperatures between roughly 20°C and 30°C when relative humidity is high — exactly the Gulf Coast afternoon conditions at KCLW. You do not need visible ice, freezing temperatures, or IMC. Warm, moist air at reduced power is the classic carb-ice environment. The C172N's Lycoming O-320 is carbureted; it has no alternate air system. Carburetor heat is the only tool.

The first symptom is subtle — a dropping tachometer and engine roughness.

In a fixed-pitch airplane like the C172N, carburetor ice first shows as engine roughness and an unexplained RPM decrease. There is no dramatic power cut. Pilots who are not actively monitoring the tachometer miss the early warning. By the time the roughness is obvious, significant ice has accumulated. Scan the tachometer as part of your regular instrument scan, especially in conducive conditions.

Apply full carburetor heat — not partial — and expect an initial RPM drop.

When you apply carb heat to an iced carburetor, the RPM will drop further before it rises. This is expected and normal: the heat is melting ice and the resulting water is briefly disrupting combustion. Do not remove carb heat when the RPM drops — that is the heat working. Hold it full on. The RPM will recover as the ice clears, typically within 15–30 seconds depending on ice accumulation. Partial carb heat can worsen the situation by partially melting ice into water ingestion without fully clearing the restriction.

At KCLW, the off-field environment is development — know your forced-landing sites.

Off Runway 34's climb-out (heading 335°), the off-field environment is low-density and medium development with some open areas (parks, large parking lots). Off Runway 16's climb-out (heading 155°), the environment is similar. There is no open water, no clear field — only development. A forced landing at KCLW is a landing in or near development, which is hazardous. Know before you fly: where are the parks? Where are the parking lots? Where is the least hazardous site? Study the field on a satellite image before you depart.

Proactive carb heat use in conducive conditions is not optional.

The C172N POH and the FAA Pilot's Handbook of Aeronautical Knowledge both recommend applying carburetor heat when conditions are conducive to icing — before the symptom appears. In a Gulf Coast summer departure, with OAT near 28–29°C and dew point near 22–23°C, that means applying carb heat during the run-up check (and confirming the expected RPM drop, then recovery) and considering its use during climb in visible moisture or high humidity. Waiting for the roughness to appear at 500 ft AGL over development is waiting too long.

Built from the real accident record

Scenario built from NTSB CEN24LA362 (2024 C172N carburetor ice / power loss), CEN14LA276 (2014 C172N engine roughness / forced landing), ERA09LA517 (2009 C172N total power loss), ANC26LA001 (2025 C172N progressive power loss despite carb heat), WPR15LA086 (2015 C172N partial power loss / mountainous terrain), CEN14LA374 (2014 C172N magneto failure), WPR14LA099B (2014 fuel contamination / forced landing), and WPR12LA306 (2012 C172N exhaust valve failure). Anonymized and localized to KCLW.

NTSB reports: CEN24LA362 · CEN14LA276 · ERA09LA517 · ANC26LA001 · WPR15LA086 · CEN14LA374 · WPR14LA099B · WPR12LA306

ACS tasks: PA.I.F — Weather Information · PA.I.G — Cross-Country Flight Planning · PA.IX.C — Emergency Approach and Landing · PA.I.H — Human Factors · PA.II.B — Engine Starting / Systems Preflight

Relevant FARs: §91.3 · §91.13 · §91.185

Run this scenario yourself

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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