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11 -5
Quiz 5
| Question | Answer |
|---|---|
| How many instrument classifications are there? — 2 – 3 – 4 | 3 |
| Every indicator requires a – power source – ground – sensor | sensor |
| Instruments used to control an aircraft's attitude are known as – flight instruments – engine instruments – navigation instruments | flight instruments |
| Analog flight instruments are operated by – air pressure and electricity – electricity and gyros – air pressure and gyros | air pressure and gyros |
| Pressure measuring instruments – are remote sensing – are direct reading – can be either of these | can be either of these |
| A bourdon tube is used to measure __ – pressure – angle of attack – air velocity | pressure |
| A diaphragm that is evacuated and then sealed is called a __ – bellows – aneroid – android | aneroid |
| Connecting multiple diaphragm chambers together creates a – bellows – aneroid – android | bellows |
| Diaphragms, aneroids and bellows that are remote sensing are part of a – – reducer – receiver – transducer | transducer |
| What would be used to measure pressure for digital flight instruments? – liquid state sensors – solid state sensors – calibrated bourdon tubes | solid state sensors |
| Absolute pressure is when a force is compared to – a total vacuum – the force exerted – a higher pressure | a total vacuum |
| Gauge pressure is the difference between the pressure being measured and – – no pressure – standard pressure – atmospheric pressure | atmospheric pressure |
| When 2 pressures are compared in a gauge, it is known as – atmospheric pressure – differential pressure – scale pressure | differential pressure |
| The standard pressure and temperature are – 29.92"Hg and 80°F – 30.00"Hg and 59°F – 29.92"Hg and 59°F | 29.92"Hg and 59°F |
| The ______________ gauge is the most important to the health of the engine, and is measured in _________. – Oil Temp, PSI – Oil Pressure, °F – Oil Pressure, PSI | Oil Pressure, PSI |
| Analog manifold pressure gauges make use of – aneroids – solid state sensors – bourdon tubes | aneroids |
| Turbine engine gauges that relate to the thrust being developed are – exhaust gas temp gauges – turbine inlet pressure gauges – engine pressure ratio gauges | engine pressure ratio gauges |
| The airspeed, altimeter and VSI instruments rely on the ______ system. – vacuum – pitot-static – electrical | pitot-static |
| Pitot tubes are mounted – in smooth air, parallel to the line of flight – in turbulent air, perpendicular to the line of flight – in smooth air, perpendicular to the line of flight | in smooth air, parallel to the line of flight |
| The static system is always mounted in the pitot tube – True – False | False |