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Inside the Piper Archer

Find a component, trace how it works, then change a condition and see the result.

PA-28-181 Archer IICarbureted · Lycoming O-360-A4M

01

Carbureted fuel system

FUEL SYSTEM · CARBURETED

Locate a component on the aircraft and select it to learn its role.

Preparing the airplane…

Left tank selected · delivery available

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TAKEAWAY

Fuel system takeaway

Follow the selected tank to the selector, strainer, pump delivery, and carburetor. The pumps move fuel; the carburetor meters it into the incoming air.

QUICK CHECK

Which part mixes metered fuel with incoming air?

About this model & sources

Reference configuration: carbureted Piper PA-28-181 Archer II, Lycoming O-360-A4M, fixed-pitch propeller, and conventional pitot-static instruments. Shapes, positions, motion, and lines are simplified for learning, not a maintenance drawing or an aircraft performance simulator. Pump demonstrations show availability of delivery, not fuel pressure or timed engine shutdown; optional primer and detailed bypass plumbing are omitted. Use the handbook for your specific aircraft for operation.

The pitot-static lab uses a standard-atmosphere, low-speed pressure model. Blockages trap pressure at the instant they are introduced. The vertical-speed display illustrates pressure change during altitude adjustments and settles to zero when altitude stops changing. It is not a calibrated flight simulator.

The electrical experiment starts with a running engine, healthy magnetos and fuel supply, and representative electrical equipment. It illustrates source availability and load selection, not measured amperages, battery endurance, a complete wiring diagram, or a failure checklist. Master power combines the BAT and ALT sides. The starter is illustrated separately and is not engaged during this experiment.