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PPL Tester

Oil system: design, function, and gauges

Oil system functions:

Wet-sump vs dry-sump:

Wet-sump Dry-sump
Oil held in Sump built into engine Separate external tank
Supply Oil pump (main component) draws from sump, routes oil to engine (pressure lubrication) Oil pump still supplies engine
Return Oil returns to sump after circulation Scavenge pumps return oil from engine to tank
Extra Some engines: rotating crankshaft also splashes oil onto parts (PHAK ch.7) More oil carried: very large reciprocating engines

Oil type and quantity:

Gauges:

Gauge Reads Notes
Oil pressure Pressure of oil supplied to engine, usually psi Green = normal, red = min/max limits. Actual limits and recommended pressures by phase of flight: Aircraft Flight Manual
Oil temperature Lubricating oil temperature Slower than pressure gauge: cold-start rise takes several minutes or longer (PHAK ch.7)

Abnormal oil temperature:

Oil grade:

Oil used Engine Allowed Ref
Detergent Non-detergent-oil Never -
Non-detergent Detergent-oil Emergency only TP 1102

Cold oil: aircraft engine oil more viscous than most engine oils, very thick when cold (TP 1102).

Trap: high oil-temperature reading is not automatically a bad oil pump; blocked cooler or defective gauge reads the same.

References


Practice