2a353: Fighter Aircraft Maintenance Journeyman

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  • 1/153 Questions

    The light for a borescope is transmitted by the......

    • Lens
    • Probe
    • View finder
    • Fiber optic cables
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About This Quiz

In the air force the aircrafts need to be in top shape in case they are called to action, this is ensured by aircraft maintenance personnel. Are you on the road to becoming a fighter aircraft maintenance journeyman and are looking for revision material? Look no further as the quiz is designed for that purpose. Give it a try.

Aircraft Maintenance Quizzes & Trivia

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  • 2. 

    The symbol entered on the forms if an aircrft exceeds the PDM cycle by 90 days and an extension is not granted is a.....

    • Red x

    • Red dash

    • Red diagonal

    • Black signature

    Correct Answer
    A. Red x
    Explanation
    If an aircraft exceeds the PDM cycle by 90 days and an extension is not granted, the symbol entered on the forms is a red x. This symbol is used to indicate that the aircraft has exceeded the allowed time for maintenance and requires immediate attention. It serves as a visual indicator for maintenance personnel to identify the aircraft that needs to be addressed promptly.

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  • 3. 

    On the F-15 aircraft, an aircrew can ensure they don't dump too much fuel by........

    • Calculating their maximum landing weight before the mission

    • Using the fuel low level warning system

    • Using the bingo fuel indication system

    • Closely monitoring the gages.

    Correct Answer
    A. Using the bingo fuel indication system
    Explanation
    The bingo fuel indication system is used on the F-15 aircraft to ensure that the aircrew does not dump too much fuel. This system provides a warning when the fuel level reaches a predetermined minimum level, known as the "bingo fuel." By monitoring this indication, the aircrew can make sure they have enough fuel to safely complete their mission and land without wasting excessive fuel. This helps to optimize fuel usage and prevent unnecessary fuel dumping.

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  • 4. 

    On the F-16, the voids and clearances between the center conductor and the outer tube of the fire dectection set sensing elements are filled with........

    • A temperature-sensitive salt mixture

    • Asbestos

    • Sealant

    • Halon

    Correct Answer
    A. A temperature-sensitive salt mixture
    Explanation
    The voids and clearances between the center conductor and the outer tube of the fire detection set sensing elements on the F-16 are filled with a temperature-sensitive salt mixture. This mixture is used to detect any changes in temperature, which can indicate the presence of a fire. As the temperature increases, the salt mixture undergoes a chemical reaction that triggers an alarm, alerting the pilot to the potential fire. This ensures that any fires can be quickly detected and addressed, increasing the safety of the aircraft.

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  • 5. 

    The F-16's flight control accumulators are......

    • Port-type

    • Piston-type

    • Bladder-type

    • Cartridge-type

    Correct Answer
    A. Piston-type
    Explanation
    The F-16's flight control accumulators are piston-type. Piston-type accumulators use a piston to separate the gas and fluid chambers. When fluid is pumped into the accumulator, it compresses the gas, storing energy. This energy can be released to power the aircraft's flight controls when needed. Piston-type accumulators are commonly used in aircraft systems due to their reliability and ability to handle high pressures.

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  • 6. 

    All metal parts of the F-16 's hydrazine fuel tank are constructed of...

    • Kevlar

    • Aluminum

    • Chromium

    • Stainless steel.

    Correct Answer
    A. Stainless steel.
    Explanation
    The metal parts of the F-16's hydrazine fuel tank are constructed of stainless steel because it is a highly corrosion-resistant material that can withstand the harsh conditions and corrosive properties of hydrazine fuel. Stainless steel is also known for its durability and strength, making it suitable for use in an aircraft fuel tank.

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  • 7. 

    What does the F-16's arresting hook caustion light indicate?

    • Arresting hook is up and locked

    • Arresting hook is not up and locked

    • Brake failure, deploy hook immediately

    • Arresting hook pneumatic reservoir low

    Correct Answer
    A. Arresting hook is not up and locked
    Explanation
    The F-16's arresting hook caustion light indicates that the arresting hook is not up and locked. This means that the hook is either in the process of being deployed or it has failed to lock into position. It is important for the hook to be up and locked before any landing or engagement with arresting gear to ensure the safety and stability of the aircraft.

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  • 8. 

    The number of positions on the function switch of the AN/PSM-37 multimeter is....

    • 2

    • 3

    • 5

    • 7

    Correct Answer
    A. 7
    Explanation
    The AN/PSM-37 multimeter has a function switch with 7 different positions. This means that the multimeter can be used for a variety of functions, such as measuring voltage, current, resistance, and other electrical parameters. Having 7 positions on the function switch allows for more versatility and flexibility in using the multimeter for different measurement tasks.

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  • 9. 

    How many air/oil coolers are there on the -229 engine?

    • 3

    • 4

    • 9

    • NONE

    Correct Answer
    A. NONE
  • 10. 

    The F-16's OXY LOW warning light illuminates.......

    • When the reserve liquid oxygen(LOX) supply is being used.

    • At a LOX quantity level of less than 0.9 liters

    • At a LOX quantity level of less that 0.5 liters

    • When LOX pressure drops below 55 psig

    Correct Answer
    A. At a LOX quantity level of less that 0.5 liters
    Explanation
    The F-16's OXY LOW warning light illuminates at a LOX quantity level of less than 0.5 liters. This means that when the amount of reserve liquid oxygen (LOX) in the aircraft drops below 0.5 liters, the warning light will turn on. This is an important safety feature as it alerts the pilot to the low oxygen level, indicating the need to take appropriate actions to replenish the LOX supply and ensure the availability of breathable air for the pilot.

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  • 11. 

    Prebraking of the F-16's main wheels is provided to......

    • Shorten aircraft stopping distances

    • Self-test the brakes prior to landing

    • Ready the brakes for high-temperature conditions

    • Eliminate gyroscopic moments applied to the main landing gear during retraction

    Correct Answer
    A. Eliminate gyroscopic moments applied to the main landing gear during retraction
    Explanation
    Prebraking of the F-16's main wheels is provided to eliminate gyroscopic moments applied to the main landing gear during retraction. This means that by applying the brakes before the wheels retract, any gyroscopic forces that could affect the landing gear are eliminated. This helps to ensure smoother and more stable retraction of the landing gear, reducing the risk of damage or instability during the process.

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  • 12. 

    The nose illumination lights on the A-10 are used for......

    • In-flight refueling

    • Tower identification

    • In-flight visual checks

    • Crew chief identification

    Correct Answer
    A. In-flight refueling
    Explanation
    The nose illumination lights on the A-10 are used for in-flight refueling. These lights are designed to provide visibility during the refueling process, allowing the pilot to accurately align the aircraft with the refueling boom. The lights help ensure safe and efficient refueling by providing a visual reference for the pilot.

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  • 13. 

    Outer mold line inspection will be accomplished on the F-22 when maintenance notices......

    • Fuel leaks

    • Hydraulic spills

    • Low observable damage

    • Worn nose landing gear tire

    Correct Answer
    A. Low observable damage
    Explanation
    Outer mold line inspection on the F-22 will be conducted when maintenance notices low observable damage. This implies that the inspection is specifically designed to identify any damage or imperfections in the outer surface of the aircraft that may affect its stealth capabilities. This inspection is crucial to ensure that the F-22 remains undetectable by radar and maintains its low observable characteristics, which are essential for its operational effectiveness.

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  • 14. 

    On the F-15 aircraft, what is the useable pressure range for the LOX system?

    • 35-70 psi

    • 55-90 psi

    • 75-100 psi

    • 95-120 psi

    Correct Answer
    A. 55-90 psi
    Explanation
    The usable pressure range for the LOX (liquid oxygen) system on the F-15 aircraft is between 55-90 psi. This range indicates the acceptable pressure levels for the system to function properly and deliver the required amount of liquid oxygen. Pressure below or above this range may lead to inefficient operation or potential damage to the system.

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  • 15. 

    On the F-15, what airframe mounted accessory drive switch is commonly called the 50% switch?

    • Two-speed switch assembly

    • Oil pump and start cut-out

    • Power turbine overspeed

    • Right decoupler position

    Correct Answer
    A. Oil pump and start cut-out
    Explanation
    The correct answer is "oil pump and start cut-out." On the F-15, the airframe mounted accessory drive switch commonly referred to as the 50% switch is the oil pump and start cut-out. This switch is responsible for controlling the operation of the oil pump and cutting off the start sequence once it reaches 50% RPM. It is an essential component in ensuring the proper functioning of the aircraft's systems.

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  • 16. 

    On the F-15 aircraft, how long does utility system non-reservoir level-sensing maintain pressure if the aircraft develops a leak in the utility hydraulic system?

    • Until the circuit A and B shutoff valves open.

    • Until the circuit A and B shutoff valves close

    • As long as there is hydraulic fluid left in the utility reservoir

    • As long as there is hydraulic fluid left in the power control backup system

    Correct Answer
    A. As long as there is hydraulic fluid left in the utility reservoir
    Explanation
    The correct answer states that the utility system non-reservoir level-sensing maintains pressure as long as there is hydraulic fluid left in the utility reservoir. This means that even if there is a leak in the utility hydraulic system, the pressure will be maintained as long as there is fluid available in the reservoir.

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  • 17. 

    The function of the F-100 Electronic Engine Control (EEC) is to....

    • Provide histroy data storage

    • Trim the convergent exhaust nozzle

    • Send signals to the cockpit indicators

    • Supervise the trim of the UFC and CIVV

    Correct Answer
    A. Supervise the trim of the UFC and CIVV
    Explanation
    The F-100 Electronic Engine Control (EEC) is responsible for supervising the trim of the UFC (Upper Face Contour) and CIVV (Convergent Inlet Vane Vortex). It does not provide history data storage, trim the convergent exhaust nozzle, or send signals to the cockpit indicators. Its main function is to oversee the adjustment of the UFC and CIVV, ensuring optimal performance and efficiency.

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  • 18. 

    On the F-15, the JFS start handle input is transmitted to the JFS start control manifold by......

    • A torque link

    • A cable assembly

    • A hydraulic signal

    • An electrical signal

    Correct Answer
    A. A cable assembly
    Explanation
    The JFS start handle input on the F-15 is transmitted to the JFS start control manifold by a cable assembly. This means that the movement of the start handle is translated into mechanical motion through the use of a cable. The cable assembly ensures that the input from the pilot is accurately transmitted to the JFS start control manifold, allowing for the proper operation of the JFS (Jet Fuel Starter) system on the aircraft.

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  • 19. 

    The fluid quantity gage on the F-16's hydraulic system A reservoir displays what quantity of measure?

    • Pints

    • Liters

    • Half-pints

    • Percent of full fluid level

    Correct Answer
    A. Percent of full fluid level
    Explanation
    The fluid quantity gauge on the F-16's hydraulic system A reservoir displays the percentage of the full fluid level. This means that the gauge shows how much of the reservoir is filled with fluid, allowing the pilot or technician to monitor the fluid level and ensure it is within the desired range. This measurement is important for maintaining the proper functioning of the hydraulic system and avoiding any potential issues that could arise from low fluid levels.

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  • 20. 

    To measure current flow, you connect an AN/PSM-37 multimeter in....

    • Series in the circuit

    • Parallel in the circuit

    • Series with the component

    • Parallel with the component

    Correct Answer
    A. Series in the circuit
    Explanation
    To measure current flow, you connect an AN/PSM-37 multimeter in series in the circuit. This means that the multimeter is connected in line with the current path, allowing it to measure the current passing through the circuit. Connecting it in parallel with the component or in series with the component would not accurately measure the current flow in the circuit.

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  • 21. 

    A path from the liquid oxygen probes to the quantity indicator on the F-16 is provided by

    • Coaxial cables

    • Oxygen probes

    • The oxygen quantity relay

    • The oxygen low-pressure switch

    Correct Answer
    A. Coaxial cables
    Explanation
    Coaxial cables provide a path from the liquid oxygen probes to the quantity indicator on the F-16. These cables are commonly used in electronic systems to transmit signals with high frequency and low loss. In this case, the coaxial cables are used to transmit the information from the liquid oxygen probes, which measure the quantity of oxygen, to the quantity indicator on the F-16. This allows the pilot or operator to monitor the oxygen levels in the aircraft. The other options mentioned, such as oxygen probes, the oxygen quantity relay, and the oxygen low-pressure switch, may be components or devices related to the oxygen system but they do not directly provide the path for the information to reach the quantity indicator.

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  • 22. 

    Which spark plugs are driven by power box 1 in the RQ-1's engine ignition system?

    • Top spark plugs in all cylinders

    • Bottom spark plugs in all cylinders

    • All spark plugs in the left bank of cylinders

    • Top spark plugs in cylinders 1 and 2, and the bottom spark plugs in cylinders 3 and 4

    Correct Answer
    A. Top spark plugs in cylinders 1 and 2, and the bottom spark plugs in cylinders 3 and 4
    Explanation
    The power box 1 in the RQ-1's engine ignition system drives the top spark plugs in cylinders 1 and 2, and the bottom spark plugs in cylinders 3 and 4.

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  • 23. 

    What type of fuel tanks are used on the RQ-1?

    • Confromal

    • Integral wing tanks

    • External fuselage tanks

    • Rubberized fuel bladders mounted in the fuselage

    Correct Answer
    A. Rubberized fuel bladders mounted in the fuselage
    Explanation
    The correct answer is rubberized fuel bladders mounted in the fuselage. This means that the RQ-1 uses flexible containers made of rubberized material to store fuel, which are then placed inside the fuselage of the aircraft. This type of fuel tank offers advantages such as lightweight construction, easy installation, and the ability to conform to the shape of the fuselage.

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  • 24. 

    The AF IMT 2691 is used to .....

    • Serve as a receipt document

    • Serve as a shipping document

    • Transfer aircraft -21 equipment

    • Account for aircraft -21 equipment

    Correct Answer
    A. Account for aircraft -21 equipment
    Explanation
    The AF IMT 2691 is used to account for aircraft -21 equipment. This means that it is a document that helps keep track of and record the inventory of equipment specifically used for aircraft -21. It serves as a tool to ensure that all equipment is properly documented and accounted for, making it easier to manage and maintain the inventory.

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  • 25. 

    On the F-15 aircraft, the airframe mounted accessory drive component that takes the input from the pawl carrier assembly and transmits the rotational force to the power takeoff drive shaft for engine starting is the......

    • Layshaft

    • Face gear

    • Gear trian

    • Pinion gear

    Correct Answer
    A. Layshaft
    Explanation
    The layshaft on the F-15 aircraft is responsible for taking the input from the pawl carrier assembly and transmitting the rotational force to the power takeoff drive shaft for engine starting. It is a crucial component that helps in transferring power effectively and efficiently.

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  • 26. 

    The aft portion of the U-2 canopy is coated with four coats of paint to......

    • Provide shade and prevent night blindness

    • Provide insulation from low temperatures

    • Combat solar radiation and glare

    • Reduce solar heat signature

    Correct Answer
    A. Combat solar radiation and glare
    Explanation
    The aft portion of the U-2 canopy is coated with four coats of paint to combat solar radiation and glare. This coating helps to protect the pilot's eyes from the intense sunlight and glare that can be present at high altitudes. It also helps to reduce the amount of solar radiation that enters the cockpit, which can help to keep the interior of the aircraft cooler. By combatting solar radiation and glare, the paint coating improves the pilot's visibility and overall safety during flight.

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  • 27. 

    On the F-22, what provides the maintainer an indication that the filter element requires replacement? 

    • Differential compensator

    • Filter element indicator

    • Selector unit indicator

    • Differential pressure indicator

    Correct Answer
    A. Differential pressure indicator
    Explanation
    The correct answer is the differential pressure indicator. This indicator provides the maintainer with an indication that the filter element requires replacement by measuring the pressure difference across the filter. When the pressure difference exceeds a certain threshold, it indicates that the filter is becoming clogged and needs to be replaced to ensure proper functioning of the system.

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  • 28. 

    The F-16's emergency generator supplies power to the ......

    • Battery buses

    • Monitor busus

    • Essential buses

    • Emergency buses

    Correct Answer
    A. Essential buses
    Explanation
    The F-16's emergency generator supplies power to the essential buses. These buses are responsible for providing power to critical systems and components in the aircraft, ensuring their operation in emergency situations. By supplying power to the essential buses, the emergency generator helps maintain the functionality of vital systems, such as navigation, communication, and flight control, during power outages or failures.

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  • 29. 

    What system malfunction causes the F-16's liquid oxygen quantity indicator to rotate counterclockwise?

    • Shorted probe

    • Oxygen pressure leak

    • Moisture in the converter

    • Short-to-ground in the high voltage side of the circuit.

    Correct Answer
    A. Short-to-ground in the high voltage side of the circuit.
    Explanation
    A short-to-ground in the high voltage side of the circuit can cause the F-16's liquid oxygen quantity indicator to rotate counterclockwise. This means that there is an electrical connection between the high voltage side of the circuit and the ground, causing a malfunction in the system. This malfunction leads to the incorrect rotation of the indicator, indicating a lower quantity of liquid oxygen than what is actually present.

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  • 30. 

    When refueling the U-2, the fuel tank filled first is the.......

    • Left outboard wing

    • Left inboard wing

    • Fuselage sump

    • Extermal

    Correct Answer
    A. Fuselage sump
    Explanation
    The correct answer is fuselage sump. When refueling the U-2, the fuel tank that is filled first is the fuselage sump. This is because the fuselage sump is located in the central part of the aircraft and is typically the first tank to be filled in order to maintain the balance and stability of the aircraft during refueling.

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  • 31. 

    The compression ratio of the RQ-1 Rotax 914F engine is.....

    • 4.0:1

    • 6.0:1

    • 8.0:1

    • 9.0:1

    Correct Answer
    A. 9.0:1
    Explanation
    The compression ratio of the RQ-1 Rotax 914F engine is 9.0:1. The compression ratio refers to the ratio of the volume of the cylinder when the piston is at the bottom of its stroke to the volume when the piston is at the top of its stroke. A higher compression ratio indicates that the air-fuel mixture is compressed to a smaller volume, resulting in a more efficient combustion process. In the case of the Rotax 914F engine, a compression ratio of 9.0:1 means that the air-fuel mixture is compressed to 1/9th of its original volume before ignition, leading to improved engine performance and fuel efficiency.

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  • 32. 

    The number of liquid oxygen converters on the U-2 is......

    • 1

    • 2

    • 3

    • 4

    Correct Answer
    A. 2
    Explanation
    The U-2 has 2 liquid oxygen converters.

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  • 33. 

    On the F-22, what components take care of the on-board engine monitoring diagnostic functions? 

    • FADEC and CEDU

    • DTC and CSFDR

    • PMA and IMIS

    • MVI and IFPC

    Correct Answer
    A. FADEC and CEDU
    Explanation
    FADEC (Full Authority Digital Engine Control) and CEDU (Central Engine Diagnostic Unit) are the components that take care of the on-board engine monitoring diagnostic functions on the F-22. FADEC controls and monitors the engine's performance, while CEDU collects and analyzes data from various sensors to diagnose any potential issues. These components work together to ensure the engine's optimal performance and safety.

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  • 34. 

    The F-100 engine exhaust nozzle position transmitter is driven by......

    • The convergent exhaust nozzle control

    • 115-VAC power

    • 26-VAC power

    • An air motor

    Correct Answer
    A. The convergent exhaust nozzle control
    Explanation
    The F-100 engine exhaust nozzle position transmitter is driven by the convergent exhaust nozzle control. This means that the position of the exhaust nozzle is controlled by the convergent exhaust nozzle control, and the transmitter is responsible for transmitting the position information. It is not driven by 115-VAC power, 26-VAC power, or an air motor.

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  • 35. 

    On the F-15, what happens to the aileron servo cylinders if they lose hydraulic pressure?

    • The pressure sensor unlocks

    • Lock to the neutral postion

    • The cavitation valves close

    • Act as flutter dampers

    Correct Answer
    A. Act as flutter dampers
    Explanation
    If the aileron servo cylinders on the F-15 lose hydraulic pressure, they will act as flutter dampers. Flutter is a phenomenon that occurs when there is an uncontrolled oscillation of the aircraft's control surfaces, which can be dangerous. The aileron servo cylinders, in this case, will help dampen the flutter and stabilize the aircraft, preventing further damage or loss of control.

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  • 36. 

    On the F-15, the speed brake selector valve is located behind...

    • Door 88L

    • Panel 77R

    • Panel 66R

    • Panel 59

    Correct Answer
    A. Panel 59
    Explanation
    The correct answer is panel 59. This means that the speed brake selector valve on the F-15 is located behind panel 59.

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  • 37. 

    On the F-15, what position does the speed brake actuator go to by setting the speed brake switch to aft?

    • Retract

    • Extend

    • Down

    • Up

    Correct Answer
    A. Extend
    Explanation
    When the speed brake switch on the F-15 is set to aft, the speed brake actuator moves to the "extend" position. This means that the speed brake is deployed or opened, creating additional drag on the aircraft and helping to reduce its speed. By extending the speed brake, the pilot can effectively slow down the aircraft during flight.

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  • 38. 

    On the U-2, the speed brakes are located on.....

    • Top of each wing

    • The bottom of each wing

    • Top of the center fuselage

    • Each side of the aft fuselage

    Correct Answer
    A. Each side of the aft fuselage
    Explanation
    The correct answer is each side of the aft fuselage. The speed brakes on the U-2 are located on each side of the aft fuselage. Speed brakes are used to increase drag and reduce the speed of an aircraft, and their placement on the U-2 allows for effective control and maneuverability.

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  • 39. 

    If the alternator on the RQ-1 fails, backup power is provided by.........

    • Two lead-acid batteries

    • Two dry-cell nickel-cadmium batteries

    • An air turbine generator powered by ram air

    • Two silver-zinc, rechargeable, alkaline-type batteries

    Correct Answer
    A. Two dry-cell nickel-cadmium batteries
    Explanation
    If the alternator on the RQ-1 fails, backup power is provided by two dry-cell nickel-cadmium batteries. These batteries are capable of storing electrical energy and can be used as a backup power source when the alternator fails. Dry-cell nickel-cadmium batteries are commonly used in aviation and other applications where reliable backup power is required.

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  • 40. 

    On the F-22, the responsibility for all low observable maintenance rests with the.....

    • Crew chief

    • Aero repair

    • System specialist

    • Aircraft structural maintenance

    Correct Answer
    A. Aircraft structural maintenance
    Explanation
    The correct answer is aircraft structural maintenance because they are responsible for maintaining the low observable features of the F-22. This includes maintaining the stealth capabilities of the aircraft by ensuring that its surfaces are properly coated and maintained to minimize radar detection. The crew chief is responsible for overall maintenance of the aircraft, aero repair specialists focus on repairing and maintaining the aircraft's systems, and system specialists deal with specific systems on the aircraft. Therefore, the responsibility for low observable maintenance specifically falls under the aircraft structural maintenance personnel.

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  • 41. 

    On the F-15 aircraft, what component contains the logic circuits for the overheat/fire detection system?

    • BIT panel

    • Flashing relay

    • Control panel

    • Controllers

    Correct Answer
    A. Controllers
    Explanation
    The logic circuits for the overheat/fire detection system on the F-15 aircraft are contained in the controllers. These controllers are responsible for receiving and processing signals from various sensors and components within the aircraft to detect any signs of overheating or fire. They play a crucial role in ensuring the safety and functionality of the overheat/fire detection system.

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  • 42. 

    On the F-15, what is the output rotation of the constant speed drive unit of the integrated drive generator?

    • 4500 RPM

    • 9000 RPM

    • 10000 RPM

    • 12000 RPM

    Correct Answer
    A. 12000 RPM
    Explanation
    The correct answer is 12000 RPM. The constant speed drive unit of the integrated drive generator on the F-15 has an output rotation of 12000 RPM.

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  • 43. 

    Which valve in the F-16's hydraulic system A ensures emergency power unit (EPU) pump flow is not supplied to the ground test stand if connected during EPU operations?

    • Pump pressure check

    • Ground pressure check

    • Reservoir service manifold relief

    • Ground test manifold pressure check

    Correct Answer
    A. Ground test manifold pressure check
    Explanation
    The ground test manifold pressure check ensures that the emergency power unit (EPU) pump flow is not supplied to the ground test stand during EPU operations. This valve is responsible for preventing any potential damage or accidents that could occur if the EPU pump flow is mistakenly supplied to the ground test stand. By checking the manifold pressure, the valve ensures that the flow is directed only to the intended system and not to the ground test stand.

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  • 44. 

    What warns the F-16 pilot of an anti-skid system failure?

    • Caution light

    • Warning horn

    • Heads up display

    • Sinking brake pedals

    Correct Answer
    A. Caution light
    Explanation
    The F-16 pilot is warned of an anti-skid system failure by a caution light. This light serves as an indicator to the pilot that there is an issue with the anti-skid system, which is responsible for preventing the aircraft's wheels from locking up during braking. The caution light alerts the pilot to take necessary actions or precautions to ensure the safe operation of the aircraft.

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  • 45. 

    The internal fuel storage styston on the F-16 consists of........

    • Five fuel tanks

    • Six fuel tanks

    • Seven fuel tanks

    • Nine fule tanks

    Correct Answer
    A. Seven fuel tanks
    Explanation
    The F-16 aircraft has a fuel storage system consisting of seven fuel tanks. This configuration allows for a larger fuel capacity, which is crucial for longer flights and extended missions. The extra fuel tanks provide the aircraft with increased range and endurance, enabling it to fly further distances without the need for refueling. Additionally, having multiple fuel tanks also helps distribute the weight of the fuel more evenly throughout the aircraft, enhancing its stability and maneuverability in flight.

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  • 46. 

    The position the A-10 feel and trim devices provide the stick to represent any trim set into the elevator actuator is.........

    • Aft load

    • Lateral load

    • Positive load

    • Neutral (zero load)

    Correct Answer
    A. Neutral (zero load)
    Explanation
    The A-10's feel and trim devices provide the stick with a representation of the trim set into the elevator actuator. This means that the devices give the pilot a sense of the position of the elevator trim. The correct answer, "neutral (zero load)", indicates that the feel and trim devices do not apply any additional load or force to the stick, but rather provide a neutral or balanced position.

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  • 47. 

     On the F-22, what prevents the maintainer from installing the filter bowl without a filter element inside?

    • Filter bowl lever

    • Ratchet spring lever

    • Spring-loaded lever

    • Safety lever lock ring

    Correct Answer
    A. Spring-loaded lever
    Explanation
    The spring-loaded lever prevents the maintainer from installing the filter bowl without a filter element inside. This lever is designed to ensure that the filter element is properly installed and secured in place before the filter bowl can be attached. Without the filter element, the lever will not engage and the maintainer will not be able to fully secure the filter bowl, preventing any potential damage or malfunction that could occur without the filter element in place.

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  • 48. 

    On the F-15, through which part of the torque tube does longitudinal input from the control stick travel?

    • Inner casing

    • Outter casing

    • Aft control rod

    • Center control rod

    Correct Answer
    A. Outter casing
    Explanation
    The correct answer is "outter casing". On the F-15, longitudinal input from the control stick travels through the outer casing of the torque tube. The torque tube is a component that helps transmit control inputs from the pilot to the aircraft's control surfaces. In this case, the outer casing specifically carries the longitudinal input, which refers to inputs that control the aircraft's pitch or nose-up/nose-down movement.

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  • 49. 

    Which components of the F-16's brake assembly are keyed on their outside diameters to the wheel?

    • End plates

    • Torque tubes

    • Rotating Discs

    • Stationary Discs

    Correct Answer
    A. Rotating Discs
    Explanation
    Rotating discs in the F-16's brake assembly are keyed on their outside diameters to the wheel. This means that the rotating discs have grooves or notches on their outer edges that match with corresponding grooves or notches on the wheel. This keying mechanism ensures that the rotating discs are securely attached to the wheel and can rotate together, allowing the brakes to function effectively.

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Quiz Review Timeline (Updated): Mar 21, 2023 +

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  • Current Version
  • Mar 21, 2023
    Quiz Edited by
    ProProfs Editorial Team
  • Sep 14, 2009
    Quiz Created by
    Rcs2004
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