Fuel Selector Confusion on Climb
A Piper Cherokee 180's fuel selector has no BOTH position — mismanagement at low altitude is unforgiving
The scenario
Departing Brooksville–Tampa Bay Regional Airport (KBKV), Brooksville, FL — Runway 09, climbing out on a heading of 090° true. Elevation 76 ft MSL. Clear skies, light winds, 22°C OAT. A routine morning flight to Jacksonville, FL, 120 nm northeast.
Aircraft: Piper Cherokee 180 (PA-28-180), solo, full fuel (48 gallons usable, 24 gallons per tank). The airplane is within limits. You completed a normal preflight and engine run-up. Both fuel tanks are full. The fuel selector is currently on LEFT, as it was during the run-up.
Pilot: you — a Private pilot, current, roughly 180 hours total. You have about 40 hours in Piper Cherokees. You are familiar with the fuel selector (LEFT / RIGHT / OFF positions), but you have not flown this particular airplane in three weeks. Your last flight in a Cherokee was in a school airplane with a different panel layout.
The tower clears you for takeoff on Runway 09. You line up, advance the throttle to full power, and rotate at 60 KIAS. The engine is running smoothly. You lift off at 55 KIAS and begin the climb. At 300 ft AGL, heading 090°, climbing through 70 KIAS, you reach for the fuel selector to switch from LEFT to RIGHT tank — standard procedure on climb to balance fuel burn.
As your hand moves the selector, you notice the panel layout is slightly different from what you remember. The selector lever is in a different position than you expected. You hesitate for a moment, then move it. The engine runs smoothly for another 10 seconds. Then it begins to sputter.
- {'label': 'Field', 'value': 'KBKV · Brooksville–Tampa Bay'}
- {'label': 'Runways', 'value': '3/21 · 9/27'}
- {'label': 'Elevation', 'value': '76 ft'}
- {'label': 'Aircraft', 'value': 'PA-28-180'}
- {'label': 'Dominant phase', 'value': 'Landing / Cruise'}
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 improper fuel tank management. The pilot failed to switch fuel tank position during the flight, running one tank dry while the other had fuel. The airplane impacted terrain. The probable cause was the pilot's in-flight mismanagement of the available fuel supply by failure to switch fuel tank position.
NTSB MIA02FA144 (2002, fatal): A Piper PA-28-180 lost engine power on downwind leg shortly after takeoff. The accident resulted from misrouting of fuel lines to the fuel selector, which resulted in fuel starvation. The pilot attempted a forced landing but struck trees and terrain. The probable cause was the misrouting of the fuel lines to the fuel selector, which resulted in the use of a fuel tank with inadequate fuel supply.
NTSB WPR24LA178 (2024): A Piper PA-28 lost engine power due to fuel starvation when the pilot placed the fuel selector in an intermediate position. The airplane made a forced landing. The probable cause was the pilot's incorrect movement of the fuel selector valve to an off or restricted position.
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 during descent. The accident resulted from the student pilot's improper fuel tank selection and inadequate instructor oversight.
NTSB ERA24LA116 (2024): A Piper PA-28-180 experienced fuel starvation during the second approach to landing after the student pilot failed to switch fuel tanks despite instructor reminders. The accident resulted from the student pilot's lack of fuel management and the flight instructor's inadequate monitoring, leading to fuel starvation and forced landing on a highway.
The real accidents cited above occurred at other airports and in other aircraft — NOT at Brooksville–Tampa Bay Regional Airport. KBKV has its own accident history (hard landings and runway excursions are dominant), but these specific fuel-starvation events happened elsewhere. The scenario is localized to KBKV to make the off-field environment real and consequential for you as a student here.
The consistent thread across all these events: the Piper Cherokee 180's fuel selector (LEFT / RIGHT / OFF) has no BOTH position. The pilot must actively switch tanks. Positioning the selector between LEFT and RIGHT restricts fuel flow and causes starvation even with fuel in the tanks. Intermediate positions are not safe — they are fuel-starvation traps. The fix — checking the selector position immediately at the first sign of engine roughness — is simple. The failure is always a delay or a misunderstanding of the selector's three discrete positions.
Key lesson — The Piper Cherokee 180's fuel selector has LEFT / RIGHT / OFF positions — there is NO BOTH. The pilot must actively switch tanks during flight. Positioning the selector between LEFT and RIGHT restricts fuel flow and causes starvation even with fuel in the tanks. At low altitude on climb-out, the decision window is measured in seconds — not minutes. Check the fuel selector position immediately at the first sign of engine roughness. Off Runway 09 at KBKV, the off-field environment is open terrain (pasture and medium development) — a forced landing there is survivable. But a fuel-selector error caught and corrected at 300 ft AGL is the best outcome.
Debrief — teaching points
The Piper Cherokee 180 has LEFT / RIGHT / OFF — no BOTH position.
Unlike the Cessna 172, which has a BOTH position, the PA-28-180's fuel selector has only three discrete positions: LEFT, RIGHT, and OFF. There is no BOTH. The pilot must actively switch tanks during flight to balance fuel burn. Running one tank dry while the other is full is a real trap — and it happens to experienced pilots who forget they are not flying a Cessna. Preflight briefing and a checklist reminder at cruise altitude are essential.
Intermediate positions (between LEFT and RIGHT) restrict fuel flow and cause starvation.
The fuel selector must be moved fully to LEFT or fully to RIGHT. Positioning it between the two — even slightly — restricts fuel flow through the selector valve and can cause fuel starvation even when both tanks have fuel. This is not a minor issue; it is a starvation trap. NTSB WPR24LA178 and CEN24LA189 both involved intermediate-position fuel selector errors. Always move the selector fully to one position or the other — never leave it in between.
At the first sign of engine roughness on climb-out, check the fuel selector immediately.
Engine roughness at low altitude can be carburetor ice, fuel contamination, or a fuel-selector error. The PA-28-180 is carbureted, so carb heat is one response. But the first action on climb-out should be to glance at the fuel selector and confirm it is fully to LEFT or fully to RIGHT. A fuel-selector error caught at 300 ft AGL is a learning moment. A fuel-selector error not caught until 400 ft AGL is an emergency.
Fuel management in the PA-28-180 is a continuous task, not a one-time preflight item.
The NTSB CEN24LA191 pilot failed to switch fuel tanks while distracted crossing a mountain range. The ERA24LA116 student pilot failed to switch tanks despite instructor reminders. Fuel management is not something you do once at takeoff; it is a continuous task throughout the flight. Set a timer or a mental reminder to switch tanks every 30 minutes at cruise. Brief your passenger or instructor on the fuel-management plan before flight.
Off Runway 09 at KBKV, the off-field environment is open terrain — good for a forced landing.
The off-field environment off Runway 09's departure end (heading 090°) is mostly open developed areas (parks/large lots), pasture, and medium development. This is good terrain for a forced landing — not water, not dense forest, not mountains. If the engine fails on the Runway 09 departure and you cannot return to the airport, establish 65 KIAS best glide, fuel selector OFF, mixture lean, master off before touchdown, and flaps for slowest possible touchdown speed. A controlled forced landing in open terrain is survivable.
Precautionary landings after fuel-selector errors are not optional.
If you experience a fuel-selector error at low altitude — even one that resolves — a precautionary landing and a systems check are the correct next step. The NTSB NYC03LA096 case involved a loose fuel line connection that was not detected in the preflight. A precautionary landing and a maintenance inspection are not overreactions; they are the correct response to any in-flight fuel-system anomaly.
Built from the real accident record
Scenario built from NTSB NYC03LA096 (2003 PA-28-180 loose fuel line / forced landing), DFW05FA028 (2004 PA-28-180 fuel tank mismanagement, fatal), MIA02FA144 (2002 PA-28-180 fuel line misrouting, fatal), WPR24LA178 (2024 PA-28 fuel selector intermediate position), CEN24LA191 (2024 PA-28-180 failure to switch tanks), CEN24LA189 (2024 PA-28-180 student fuel selector error), ERA24LA116 (2024 PA-28-180 student fuel starvation on approach), and CEN24LA108 (2024 PA-28 fuel selector OFF position). Anonymized and localized to KBKV.
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.C — Takeoff and Climb · PA.IX.C — Emergency Approach and Landing · PA.I.H — Human Factors
Relevant FARs: §91.3 · §91.13 · §91.185
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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