Aircraft General Knowledge — AeroplanesLektion 17 von 55
17/55Fuel system

Components

Lesezeit ca. 1 min·
en
Sprache wechseln (DE)

Components of a typical fuel system

ComponentFunction
TanksStore fuel. Most singles have one per wing; some types add a header tank for fuel feed under negative g or as a minimum reserve
Fuel selectorPositions typically LEFT, RIGHT, BOTH, OFF. BOTH is common on high-wings (gravity feed from both tanks simultaneously); low-wings often have only L/R
Gascolator / strainerLowest point in the system. Collects water and sediment. Drain before every flight
Engine-driven fuel pumpMain pump on the engine accessory case — mechanical
Electric auxiliary / boost pumpUsed for start, take-off, landing and as backup if the mechanical pump fails
PrimerInjects fuel directly into the intake manifold for cold starts
Fuel quantity gaugesFloat-based; per CS-23.1337 must read "zero" when tank empty. Unreliable — always confirm by dipstick / visual check

Gravity feed vs. pump-fed

SystemUseExample
Gravity feedTank above engine → no main-line pump requiredCessna 152/172 (high wing)
Pump-fedTank below engine → engine-driven pump + electric boost pump requiredPA-28 (low wing), DA40, Aquila

Practice — pre-flight check

  1. Visual fuel quantity (dipstick or visual marker)
  2. Drain gascolator — check for water, sediment, wrong colour
  3. Fuel caps — vent clear, properly secured
  4. Fuel selector position confirmed before start and after in-flight tank changes
Fertig gelesen?
Melde dich an, um deinen Fortschritt zu speichern.