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SAMPLE SBTTakeoff / Initial Climb

Fuel Selector Confusion on Climb-Out

A Piper Cherokee 180's fuel selector has no BOTH position — mismanagement on departure can mean engine failure at 500 ft AGL

Piper Cherokee 180 · Tampa Executive Airport (KVDF) · Private · Takeoff / Initial Climb

The scenario

Departing Tampa Executive Airport (KVDF), Tampa, FL — Runway 05, climbing out on a 042° heading. Elevation 22 ft MSL. Clear skies, light winds from 080° at 4 kt, OAT 26°C, altimeter 29.98. Visibility 10 SM. A textbook VFR morning in central Florida.

Aircraft: Piper PA-28-180 Cherokee, solo, full fuel (both tanks), within limits. Lycoming O-360-A, carbureted, fixed-pitch prop, fixed gear, steam panel. The airplane was airworthy at departure; nothing was written up. The fuel selector is in the LEFT position — standard for takeoff.

Pilot: you — a Private pilot, current, roughly 250 hours total. You have flown the Piper Cherokee before, but not frequently. You are familiar with the fuel selector (LEFT / RIGHT / OFF), but you have not yet internalized the discipline of switching tanks on a regular schedule. You did a thorough preflight; both tanks showed full on the sight gauges.

You are 500 ft AGL, climbing at 74 KIAS (Vy, best rate of climb), heading 042°. The engine is running smoothly. Off the Runway 05 departure end ahead of you is wooded wetland, medium development, and pasture — good forced-landing terrain if needed. But you are not thinking about forced landings; you are focused on the climb-out and the departure procedure.

At 600 ft AGL, you notice the engine is running slightly rough. Not dramatically — just a subtle miss, a slight hesitation in the power delivery. You scan the engine instruments: the tachometer is steady at 2,400 RPM, the oil temperature and pressure are normal, the ammeter is in the green. Nothing obvious is wrong. You continue the climb.

The decision

Before we get into the decision tree — what do you already know about the Piper Cherokee 180's fuel system? (Pick all that apply; this records your baseline.)

What the record shows

What the NTSB files show

NTSB DFW05FA028 (2004, fatal): A Piper PA-28-180 on a night cross-country flight lost engine power due to fuel starvation from the pilot's failure to switch fuel tanks. The pilot was distracted by weather and low ceilings; he did not monitor the fuel selector or switch tanks on schedule. The engine quit on downwind leg; the pilot attempted a forced landing but struck terrain. The probable cause was the pilot's in-flight mismanagement of the available fuel supply by failure to switch fuel tank position, with low ceilings and dark night conditions as contributing factors. This accident occurred at a different airport — NOT at KVDF.

NTSB CEN24LA191 (2024): A Piper PA-28-180 on a cross-country personal flight lost engine power due to fuel starvation when the pilot failed to switch fuel tanks while distracted crossing a mountain range. The pilot made a forced landing in a field. The probable cause was the pilot's failure to switch fuel tanks while en route, which resulted in the loss of engine power due to fuel starvation. This accident occurred at a different airport — NOT at KVDF.

NTSB CEN24LA189 (2024): A Piper PA-28-180 on an instructional flight lost all engine power when the student pilot positioned the fuel selector valve between port positions (an intermediate position, neither fully LEFT nor fully RIGHT) during descent. The probable cause was the student pilot's selection of an improper fuel tank selector position, which resulted in fuel starvation and a total loss of engine power. This accident occurred at a different airport — NOT at KVDF.

NTSB WPR24LA178 (2024): A Piper PA-28 on a personal flight lost engine power due to fuel starvation when the pilot placed the fuel selector in an intermediate position and made a forced landing. The probable cause was the pilot's incorrect movement of the fuel selector valve to an off or restricted position, which resulted in fuel starvation and a loss of engine power. This accident occurred at a different airport — NOT at KVDF.

The consistent thread across all these events: the Piper Cherokee 180's fuel selector has LEFT / RIGHT / OFF positions — there is NO BOTH position. The pilot must actively switch tanks every 30 minutes of flight time. Fuel starvation happens when (1) the selected tank runs dry, (2) the selector is placed in an intermediate position (between LEFT and RIGHT), (3) the selector is moved to OFF, or (4) the selected tank is contaminated or has a fuel-line issue. At low altitude on departure, fuel starvation is an emergency. The decision window is measured in seconds.

Off Runway 05 at KVDF, the climb-out environment is wooded wetland, medium development, and pasture — good forced-landing terrain. Off Runway 36, the environment is medium development, wooded wetland, and open water — a ditching scenario. The field's dominant accident pattern is loss of control on the ground (18.4%) and hard landing (18.4%), but forced landing (15.8%) is also significant. Fuel starvation is a forced-landing driver.

The real accidents cited above occurred at other airports — NOT at Tampa Executive Airport. KVDF has its own accident history, but these specific events happened elsewhere. The scenario is localized to KVDF to make the off-field environment real and consequential for you as a student here.

Key lesson — The Piper Cherokee 180's fuel selector has LEFT / RIGHT / OFF — no BOTH position. The pilot must actively switch tanks every 30 minutes of flight time to balance fuel consumption and detect a starvation problem early. Fuel starvation from selector mismanagement (forgetting to switch, placing the selector in an intermediate position, or selecting a contaminated tank) is the signature failure mode of this airplane. At low altitude on departure, an engine failure due to fuel starvation is an emergency. Diagnose quickly: if the engine roughens on climb-out, check the selector position first, then switch tanks. If the engine recovers, return to the airport for a precautionary landing and maintenance inspection. Do not continue the flight on a single tank without understanding why the other tank failed.

Debrief — teaching points

The Piper Cherokee 180 has no BOTH position — you must actively switch tanks.

Unlike the Cessna 172, which has a BOTH position and draws from both tanks simultaneously, the Piper Cherokee 180's fuel selector has only LEFT / RIGHT / OFF. The pilot must actively switch tanks every 30 minutes of flight time to balance fuel consumption. Forgetting to switch tanks is the signature failure mode of this airplane. At takeoff, the selector is placed on LEFT (or RIGHT, depending on which tank you want to use first). As you climb out, you must remember to switch tanks on schedule — typically every 30 minutes. Failure to switch results in the selected tank running dry while the other tank has fuel, causing fuel starvation and engine failure.

Fuel starvation can also result from an intermediate selector position.

If the fuel selector is placed between LEFT and RIGHT (an intermediate position), neither tank feeds the engine properly. The result is fuel starvation even though both tanks have fuel. This can happen if the selector knob is not fully seated in the LEFT or RIGHT position, or if the pilot moves the selector too slowly and leaves it in an intermediate position. Always ensure the selector is fully seated in the LEFT or RIGHT position — not in between. NTSB CEN24LA189 and WPR24LA178 both involved intermediate selector positions.

Engine roughness on climb-out in the Cherokee is more likely fuel-system related than carburetor ice.

While carburetor ice can occur in the Cherokee's carbureted Lycoming O-360, engine roughness on climb-out is more commonly caused by fuel-system issues: a contaminated tank, a fuel-line problem, or a selector misposition. Carb heat is worth trying, but if it doesn't help, immediately check the fuel selector position and consider switching tanks. The left tank is more prone to contamination (water, sediment) because the fuel cap and vent are on the left wing; switching to the right tank often clears the problem.

At low altitude on departure, fuel starvation is an emergency.

At 600 ft AGL on climb-out, you have roughly 30 seconds of decision time before altitude becomes critical. If the engine roughens or loses power, diagnose quickly: check the selector position, apply carb heat if needed, and switch tanks if the selector is correct. If the engine recovers after switching tanks, you have two options: (1) return to the airport for a precautionary landing and maintenance inspection, or (2) continue the flight on the good tank only, accepting the endurance limitation. Option 1 is the safer, more conservative choice. Option 2 is workable only if you are confident in the good tank and your flight plan does not exceed the single-tank endurance.

Establish a fuel-switching discipline before every flight.

Before takeoff, decide which tank you will use first (typically LEFT) and set a timer or note the time. Every 30 minutes, switch to the other tank and note the time. This discipline serves two purposes: (1) it balances fuel consumption between the two tanks, and (2) it detects a fuel-system problem early — if one tank is contaminated or has a fuel-line issue, you will discover it at altitude where you have time to diagnose and return to the airport, not at 600 ft AGL on departure. The NTSB accidents involving fuel starvation almost always involved a pilot who did not switch tanks on schedule or who was distracted and forgot to switch.

Off Runway 05 at KVDF, the forced-landing environment is good — wooded wetland, pasture, and medium development.

If the engine fails on the Runway 05 departure and you cannot return to the airport, the off-field environment ahead is wooded wetland, pasture, and medium development — good forced-landing terrain. Establish 65 KIAS best glide, pick the best landing surface you can see (open pasture or a cleared area), and execute a controlled forced landing. Flaps for slowest possible touchdown speed, doors unlatched, master off before impact. Off Runway 36, the environment is medium development, wooded wetland, and open water — a ditching scenario. Know the off-field environment before you line up on the runway.

Built from the real accident record

Scenario built from NTSB DFW05FA028 (2004 PA-28-180 fuel starvation / night cross-country, fatal), CEN24LA191 (2024 PA-28-180 failure to switch tanks en route), CEN24LA189 (2024 PA-28-180 student selector misposition during descent), ERA24LA116 (2024 PA-28-180 student fuel mismanagement on approach), and WPR24LA178 (2024 PA-28 selector intermediate position starvation). Localized to Tampa Executive Airport (KVDF).

NTSB reports: NYC03LA096 · DFW05FA028 · MIA02FA144 · WPR24LA178 · CEN24LA191 · CEN24LA189 · ERA24LA116 · CEN24LA108

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

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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