engine instrument systems Flashcards

1
Q

what does a tachometer on a reciprocating engine indicate

A

engine RPM, crankshaft speed

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2
Q

where would a carburetor temperature bulb be located

A

in the ram air intake duct

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3
Q

what is the fuel pressure range on a float type carburetor

A

3 to 5 psi

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4
Q

name the basic components of a fuel indicator system

A

transmitter and indicator

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5
Q

why is fuel flow monitored

A

to determine fuel consumption and engine performance

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6
Q

what unit of measurement is generally used to indicate fuel flow

A

pounds or gallons per hour

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7
Q

what does the manifold gauge indicate and how is it calibrated

A

it measures the absolute pressure in the engine manifold and is calibrated in inches of mercury

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8
Q

what directly controls manifold pressure

A

throttle opening and engine (RPM)

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9
Q

where should the thermocouple be installed on a reciprocating engine using a single probe cylinder head temperature system

A

on the hottest cylinder

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10
Q

during engine operation where should the propeller control be set when checking the manifold pressure

A

low pitch, high RPM

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11
Q

what are the possible indications of an oil pressure transmitter or indicator malfunction

A

A severe or sudden drop in oil pressure while the oil temperature remains normal and the oil supply remains full

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12
Q

is the aircraft electrical system required to power a cylinder head temperature gauge

A

no, a thermocouple is used as the electrical source

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13
Q

in reference to a carbureted reciprocating engine, where is a fuel flow indicating system generally connected in an engine fuel system

A

between the engine fuel pump and carburetor

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14
Q

on an engine equipped with a fixed pitch propeller, what controls both manifold pressure and engine RPM

A

the throttle control

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15
Q

what are turbine engine tachometer gauges designed to indicate

A

percentage of compressor RPM

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16
Q

what does turbine engine exhaust gas temperature ( EGT ) indicate?

A

it is the average temperature of turbine discharge gases

17
Q

how is turbine engine EGT obtained

A

usually by several thermocouples spaced at intervals around the exhaust duct perimeter near the turbine exit

18
Q

what pressures are measured to obtain engine pressure ratio

A

total inlet pressure and total turbine exhaust pressure

19
Q

what is the torque being developed by a turboprop engine an indication of

A

shaft horsepower

20
Q

what is the electrical source for a cylinder head temperature system

A

a thermocouple

21
Q

what is the possible cause when oil pressure drops off severely, oil supply remains full, and oil temperature is normal

A

oil pressure transmitter or indicator malfunction

22
Q

how can turbine engine EGT system be checked without running the engine

A

by checking the resistance of thermocouples and circuits