2A354P Vol.2
- 1.
Write your text here
- 2.
On the F-15C, D, and E fuel quantity indicator, the BINGO indicator is adjusted to providethe pilot with warnings when a
- A.
Preset fuel level is reached and to automatically stop fuel dumping.
- B.
Preset fuel level is reached and to automatically start fuel dumping.
- C.
Fuel level is reached and fuel dump is increased.
- D.
Fuel imbalance starts fuel dumping.
Correct Answer
A. Preset fuel level is reached and to automatically stop fuel dumping. -
- 3.
The unit in the F-15 fuel quantity indicating system that rectifies the AC power into positiveand negative DC pulses is the
- A.
Tank unit.
- B.
Indicator
- C.
Thermistor
- D.
Control units.
Correct Answer
A. Tank unit. -
- 4.
6. (202) On the F-15C/D/E aircraft, the fuel quantity system requires calibration after replacement of the
- A.
External tank
- B.
Signal conditioner
- C.
Tank unit number 2
- D.
Low-level control unit
Correct Answer
B. Signal conditioner -
- 5.
What unit of measurement is used for capacitance?
- A.
Volts
- B.
Farad
- C.
Ohms
- D.
Henrie
Correct Answer
B. Farad -
- 6.
The relationship of current between the legs of a capacitive bridge circuit when the circuit isbalanced is equal curren
- A.
With the reference capacitor leading in phase by 90°.
- B.
And identical phase.
- C.
But opposite phases.
- D.
Option 4
Correct Answer
C. But opposite phases. -
- 7.
What capacitive bridge-type fuel quantity system component acts to null out the error signalgenerated by the balanced bridge?
- A.
Bridge amplifier.
- B.
Fixed input capacitor.
- C.
Frequency-sensitive filter.
- D.
Rebalancing potentiometers.
Correct Answer
D. Rebalancing potentiometers. -
- 8.
When performing a full tank check or making full adjustment of the fuel quantity system onan F-15, you must conside
- A.
Altitude
- B.
Humidity
- C.
Fuel density
- D.
Outside temperature
Correct Answer
C. Fuel density -
- 9.
When the F-15 fuel quantity indicator pounds counter is driven to its mechanical stop, this isa probable indication of a/an
- A.
Loose tank unit
- B.
Faulty tank unit
- C.
Open tank aboard relay
- D.
Indicator out of calibration
Correct Answer
B. Faulty tank unit -
- 10.
What type of position is a simple synchro indicating system designed to display?
- A.
Mechanical
- B.
Servomotor
- C.
Pneumatic
- D.
Electrical
Correct Answer
A. Mechanical -
- 11.
How many hydraulic pressure transmitters does the F-15 have?
- A.
5
- B.
2
- C.
3
- D.
4
Correct Answer
C. 3 -
- 12.
The F-15 hydraulic pressure indicators display psi with a range of 0 to
- A.
1000
- B.
2000
- C.
3000
- D.
4000
Correct Answer
D. 4000 -
- 13.
Which F-15 hydraulic pressure system component loses its connection, causing theapplicable circuit or pump light on the BCP to illuminate, when hydraulic pressure drops below1,600–1,400 psi?
- A.
Pump pressure switches.
- B.
Reservoir level sensor.
- C.
Pressure transmitter.
- D.
Pressure indicator.
Correct Answer
A. Pump pressure switches. -
- 14.
The F-15 oil pressure indication range in psi is from 0 to
- A.
100 in increments of 5 psi.
- B.
200 in increments of 5 psi.
- C.
100 in increments of 10 psi.
- D.
200 in increments of 10 psi.
Correct Answer
A. 100 in increments of 5 psi. -
- 15.
What psi must either or both oil pressures remain at for five seconds in order for the F-15OIL PRESS light to illuminate?
- A.
4 ±1
- B.
6 ±1
- C.
8±1
- D.
10 ±1
Correct Answer
C. 8±1 -
- 16.
The F-15 tachometer indicator shows percent rpm in the range of 0 to
- A.
90
- B.
100
- C.
110
- D.
120
Correct Answer
C. 110 -
- 17.
How many FTIT AL/CR sensors are on each F-15 engine?
- A.
3
- B.
5
- C.
7
- D.
9
Correct Answer
C. 7 -
- 18.
What temperature range in C is indicated on the FTIT indicator?
- A.
0° to 1,200°C.
- B.
0° to 1,200°C.
- C.
100° to 1,400°C.
- D.
200° to 1,400°C.
Correct Answer
D. 200° to 1,400°C. -
- 19.
What temperature in C must the FTIT exceed in order for the “WARNING FTITOVERTEMP LT/RT” to be heard in the F-15 pilot’s headset?
- A.
800°± 10°C.
- B.
800°± 20°C.
- C.
1,000°± 10°C.
- D.
1,000°± 20°C.
Correct Answer
C. 1,000°± 10°C. -
- 20.
The F-15 fuel flow indicating systems provide the pilot with a display of the
- A.
Speed of fuel consumed in gallons per hour.
- B.
Rate of fuel being consumed by the aircraft engines.
- C.
Amount of fuel being consumed in gallons per hour.
- D.
Amount of fuel remaining in the main and wing tanks.
Correct Answer
B. Rate of fuel being consumed by the aircraft engines. -
- 21.
The range of the F-15 fuel flow indicator is from 0 to
- A.
100 gph × 1000 gph
- B.
100 pph × 1000 pph.
- C.
200 gph × 1000 gph.
- D.
200 pph × 1000 pph.
Correct Answer
B. 100 pph × 1000 pph. -
- 22.
(208) What is the F-15’s exhaust nozzle position indication range?
- A.
0 to 100% open.
- B.
25 to 100% open.
- C.
0 to 100% closed.
- D.
25 to 100% closed.
Correct Answer
A. 0 to 100% open. -
- 23.
Which F-15 component automatically changes the nozzle position as a function of enginesetting?
- A.
CC
- B.
EDU
- C.
DEEC
- D.
CENC
Correct Answer
D. CENC -
- 24.
On the F-15E, what is used as the primary engine display?
- A.
UFC
- B.
EMD
- C.
MPCD
- D.
ADCP
Correct Answer
B. EMD -
- 25.
The F-15E N2 rpm indication system displays percent rpm in the range of 0 to
- A.
90
- B.
100
- C.
110
- D.
120
Correct Answer
C. 110 -
- 26.
Which F-15E nozzle position indicating system component drives the engine exhaust nozzleposition transmitter through a mechanical interface?
- A.
EDU
- B.
DEEC
- C.
ADCP
- D.
CENC
Correct Answer
D. CENC -
- 27.
If any BCP avionics light illuminates, what signal does the BCP send to the caution lightslogic unit to turn on the AV BIT light on the F-15?
- A.
Open
- B.
Ground
- C.
26 VAC
- D.
115 VAC
Correct Answer
A. Open -
- 28.
Which component determines if a low oil pressure condition exists on the F-15E?
- A.
EDU
- B.
AIU NO.1
- C.
DEEC
- D.
ADCP
Correct Answer
D. ADCP -
- 29.
What is the attitude displayed on the F-15 standby AI?
- A.
180° roll, 92° climb and 78° dive.
- B.
180° roll, 98° climb and 72° dive.
- C.
360° roll, 92° climb and 78° dive.
- D.
360° roll, 98° climb and 72° dive.
Correct Answer
C. 360° roll, 92° climb and 78° dive. -
- 30.
Which switch on the GND PWR control panel applies power to STANDBY ATTD INDcircuit breakers on the F-15?
- A.
1
- B.
2
- C.
3
- D.
4
Correct Answer
B. 2 -
- 31.
How long after power has been removed will the F-15 standby AI provide a good indication?
- A.
3 minutes
- B.
6 mintues
- C.
9 minutes
- D.
12 minutes
Correct Answer
C. 9 minutes -
- 32.
On F-15A through D, which type of information does the FDA send to the CC?
- A.
HSI mode, pitch and bank steering, heading marker.
- B.
TACAN DATA, course set, time meter readout.
- C.
TACAN DATA, heading set, glide-slope and localizer deviation.
- D.
Destination/target bearing, to-from data, HSI mode.
Correct Answer
C. TACAN DATA, heading set, glide-slope and localizer deviation. -
- 33.
On an F-15A through D, which horizontal situation indicating system component monitorsservo operation to detect and indicate a malfunction?
- A.
Mode select switch
- B.
AI
- C.
FDA
- D.
HSI
Correct Answer
D. HSI -
- 34.
On an F-15A through D, what component selects the information source for display on theHSI?
- A.
FDA
- B.
Compass control panel
- C.
STEER MODE switch
- D.
HSI
Correct Answer
C. STEER MODE switch -
- 35.
On an F-15A through D, in which STEER MODE position is the HSI to-from pointer, AIhorizontal pointer, and glide slope indicator out of view?
- A.
ILS/NAV
- B.
TACAN
- C.
ILS/TCN
- D.
NAV
Correct Answer
D. NAV -
- 36.
The HSI no. 1 pointer is a function of
- A.
NAV and TACAN
- B.
The ADF and TACAN
- C.
TACAN
- D.
NAV
Correct Answer
B. The ADF and TACAN -
- 37.
As a function of the F-15A through D HSI no. 1 bearing pointer, the priority system is
- A.
ADF
- B.
ILS
- C.
TACAN
- D.
NAV
Correct Answer
A. ADF -
- 38.
The BEACON light illuminates when the
- A.
Localizer deviation is at its limit.
- B.
Aircraft glide slope is out of limits.
- C.
ILS is invalid.
- D.
Aircraft passes over the middle/outer ILS marker.
Correct Answer
D. Aircraft passes over the middle/outer ILS marker. -
- 39.
On the F-15 acceleration indicating/g-force exceedance system, acceleration in the positivedirection is caused by aircraft movement in what direction?
- A.
Upward
- B.
Forward
- C.
Backward
- D.
Downward
Correct Answer
A. Upward -
- 40.
What should the F-15 acceleration indicator read (in g-forces) when no external force isapplied?
- A.
0g
- B.
1g
- C.
2g
- D.
-1g
Correct Answer
B. 1g -
- 41.
On the F-15, what type of BIT executes a more in-depth check of the avionics systems andprovides additional data to review for isolating malfunctions?
- A.
Periodic
- B.
Initiated
- C.
Automatic
- D.
Continuous
Correct Answer
B. Initiated -
- 42.
What color will the F-15 ASP ball-type latch indicators turn when a failure is detected by asystem’s BIT program?
- A.
Orange
- B.
White
- C.
Black
- D.
Red
Correct Answer
A. Orange -
- 43.
How many fault indicator latches does the F-15 ASP have for numerous LRUs, systems,and locations (including door components)?
- A.
48
- B.
56
- C.
72
- D.
96
Correct Answer
C. 72 -
- 44.
Malfunctioning LRUs or systems will report failures to the F-15 BCP and ASP using a BCPsignal
- A.
And an ASP signal that are both an open.
- B.
And an ASP signal that are both a ground.
- C.
With a ground and an ASP signal with an open.
- D.
With an open and an ASP signal with a ground.
Correct Answer
D. With an open and an ASP signal with a ground. -
- 45.
If the F-15 pilot wanted to hydraulically shut down the lateral system of the PRCA, whichposition would the roll ratio switch be placed to?
- A.
Off
- B.
Automatic
- C.
Shut down
- D.
Emergency
Correct Answer
D. Emergency -
- 46.
Which F-15 component is used to control the flow of hydraulic fluid to the PRCA?
- A.
Roll ratio controller.
- B.
Mode select assembly.
- C.
Lateral feel trim actuator.
- D.
Aileron rudder interconnect.
Correct Answer
B. Mode select assembly. -
- 47.
Which F-15component separates the single PRCA output into two mechanical outputs?
- A.
Mechanical mixer.
- B.
Mode select assembly.
- C.
Lateral feel trim actuator.
- D.
Aileron rudder interconnect.
Correct Answer
A. Mechanical mixer. -
- 48.
Which F-15 components in the longitudinal flight control subsystem are used to createsymmetrical up and down movements for pitch maneuvering?
- A.
Flaps
- B.
Vertical rudders.
- C.
Horizontal ailerons.
- D.
Horizontal stabilators.
Correct Answer
D. Horizontal stabilators. -
- 49.
Which F-15 longitudinal flight control subsystem component is used to help neutralize theeffect of acceleration on the control stick during maneuvers?
- A.
Pitch ratio switch.
- B.
Longitudinal mass balance.
- C.
Pitch and roll channel assembly.
- D.
Longitudinal FTA.
Correct Answer
B. Longitudinal mass balance. -
- 50.
Which F-15 longitudinal flight control subsystem component automatically compensates fortrim changes caused by accelerating from subsonic to supersonic flight?
- A.
Mechanical mixer.
- B.
Pitch trim controller.
- C.
Pitch ratio controller.
- D.
Longitudinal feel trim actuator.
Correct Answer
B. Pitch trim controller. -
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Mar 14, 2022Quiz Edited by
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Nov 30, 2016Quiz Created by
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