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27 Cards in this Set
- Front
- Back
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The relationship of current between the legs of a capacitive bridge circuit when the circuit is balanced is equal current |
but opposite phases. |
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What unit of measurement is used for capacitance? |
Farad. |
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What capacitive bridge-type fuel quantity system component acts to null out the error signal generated by the balanced bridge? |
Rebalancing potentiometers. |
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The range of the F-15 fuel flow indicator is from 0 to |
100 pph × 1000 pph. |
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What is the F-15’s exhaust nozzle position indication range? |
0 to 100% open. |
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Which F-15 component automatically changes the nozzle position as a function of engine setting? |
CENC. |
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On the F-15E, what is used as the primary engine display? |
EMD. |
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The F-15E N2 rpm indication system displays percent rpm in the range of 0 to |
110 |
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Which F-15E nozzle position indicating system component drives the engine exhaust nozzle position transmitter through a mechanical interface? |
CENC. |
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Which component determines if a low oil pressure condition exists on the F-15E? |
ADCP. |
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What is the attitude displayed on the F-15 standby AI? |
360° roll, 92° climb and 78° dive. |
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Which switch on the GND PWR control panel applies power to STANDBY ATTD IND circuit breakers on the F-15? |
2 |
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How long after power has been removed will the F-15 standby AI provide a good indication? |
9 minutes. |
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On an F-15A through D, which type of information does the FDA send to the CC? |
TACAN DATA, heading set, glide-slope and localizer deviation. |
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On an F-15A through D, which horizontal situation indicating system component monitors servo operation to detect and indicate a malfunction? |
HSI. |
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On an F-15A through D, what component selects the information source for display on the HSI? |
STEER MODE switch. |
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On an F-15A through D, in which STEER MODE position is the HSI to-from pointer, AI horizontal pointer, and glide slope indicator out of view? |
NAV. |
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The HSI no. 1 pointer is a function of |
the ADF and TACAN. |
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As a function of the F-15A through D HSI no. 1 bearing pointer, the priority system is |
the ADF. |
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The BEACON light illuminates when the |
aircraft passes over the middle/outer ILS marker. |
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On the F-15 acceleration indicating/g-force exceedance system, acceleration in the positive direction is caused by aircraft movement in what direction? |
Upward. |
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What should the F-15 acceleration indicator read (in g-forces) when no external force is applied? |
1g. |
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On the F-15, what type of BIT executes a more in-depth check of the avionics systems and provides additional data to review for isolating malfunctions? |
Initiated. |
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How many fault indicator latches does the F-15 ASP have for numerous LRUs, systems, and locations (including door components)? |
72 |
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What color will the F-15 ASP ball-type latch indicators turn when a failure is detected by a system’s BIT program? |
Orange. |
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Malfunctioning LRUs or systems will report failures to the F-15 BCP and ASP using a BCP signal |
with an open and an ASP signal with a ground. |
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If any BCP avionics light illuminates, what signal does the BCP send to the caution lights logic unit to turn on the AV BIT light on the F-15? |
Open. |
