Want To Go Into The Aviation Industry? This Quiz Is A Must!

Closing the oxygen manual shutoff valve is the correct answer because it is important to prevent the oxygen from fueling the fire. By closing the valve, the supply of oxygen to the fire is cut off, reducing the risk of the fire spreading or intensifying. This action helps to control the situation and minimize the potential danger.

During a ground evacuation, if a hot brake is suspected or main wheel well fire exists, it is important to chock the nose gear only. Chocking the nose gear will help prevent the aircraft from rolling forward and potentially causing further damage or danger. Chocking the opposite or main gear may not effectively prevent the aircraft from moving forward.

The correct answer is "Yellow, Yellow" because the question states that the chopping locations are marked in a certain color on both the inside and outside of the fuselage. Therefore, the correct answer is the option that mentions the same color twice, which is "Yellow, Yellow".

Engine-driven generators are mounted to the GMAD (Generator and Motor Accessory Drive) system. The GMAD system is responsible for driving various accessories on the aircraft, including the generators. These generators are typically located on the engine itself and are driven by the engine's power to generate electrical power for the aircraft's systems.

The eight Emergency Exit Lights activate when all of the conditions mentioned in the options are met. This means that the lights will activate when the Emergency Exit light test switch is armed, when the airplane experiences a decelerating force of 2G's or more, or when the essential DC bus power fails. Therefore, any of these events can trigger the activation of the Emergency Exit Lights.

The statement is false because auxiliary fuel tanks are typically located in the fuselage or under the wings, not on top of the wing. Therefore, it would not be possible to dip them from the top of the wing to check fuel levels.

Aircraft safety checks are completed every 30 minutes to ensure the safety and functionality of the aircraft. Regular checks are essential to identify any potential issues or malfunctions that may arise during the flight. This frequent interval allows for prompt detection and resolution of any problems, minimizing the risk of accidents or incidents. By conducting safety checks every 30 minutes, the crew can maintain a high level of vigilance and ensure the aircraft's overall safety throughout the flight.

During reverse taxiing, it is important for the BA to continuously conduct conning phraseology to advise the pilot of progress. This is necessary to ensure the safety of the aircraft and to prevent any potential collisions or accidents. By providing continuous verbal signaling, the BA can effectively communicate with the pilot and keep them informed about the progress of the reverse taxiing maneuver. This helps the pilot make informed decisions and take appropriate actions during the maneuver.

The white eyeball light encircled by a green ring is the indication that the power is connected to the plane. This combination of lights is commonly used in aircraft to indicate that external power is successfully connected. The white eyeball light represents the power being supplied, while the green ring around it signifies that the power is connected and functioning properly.

The aircraft battery should be replaced after dropping below 22 volts. This is because the voltage drop below this threshold indicates that the battery is no longer able to provide sufficient power to the aircraft's electrical systems. Replacing the battery at this point ensures that the aircraft has a reliable power source for safe operation.

The correct answer is "No, it is forbidden by the M3710.1E and TO 1C-130J-1." This means that cellular phones are not authorized for use on the C130J aircraft during flight. The M3710.1E and TO 1C-130J-1 are likely regulations or guidelines that prohibit the use of cellular phones on the aircraft.

According to CIM 3710.1 (series), a flight crew member should not fly for more than 50 hours in any consecutive 7 days and should not fly for more than 125 hours during any consecutive 30-day period. Therefore, both statement A and statement B are accurate according to the CIM 3710.1 (series) regulations.

To tie down the main landing gear, 14 10k chains are required.

The brake systems accumulators are located in the nose wheel well.

The correct answer is 4 because the C130J aircraft typically has four fire extinguishers installed. These extinguishers are strategically placed throughout the aircraft to ensure that any potential fires can be quickly and effectively extinguished. Having four fire extinguishers allows for sufficient coverage and increases the chances of successfully combating any fire emergencies that may arise during flight.

The correct answer is 4 because the question asks about the number of oxygen regulators installed in the cargo compartment on the C130J. Therefore, there are four oxygen regulators installed in the cargo compartment.

The maximum weight limit for items to be placed on or moved across the ramp unsupported is 2,000 lbs.

According to the given statement, all aircraft must carry one Personal Flotation Device (PFD) for each person on board. It also states that aircrew survival vests can only be worn by trained personnel. Therefore, the correct answer is 1, indicating that each person on board should have one PFD.

The correct answer is 250-650ft. This range indicates that the flares in a MK-79 SIGNAL FLARE KIT can travel to a height between 250 and 650 feet. This suggests that the flares have a significant vertical reach, potentially allowing them to be seen from a distance or in situations where visibility is limited.

In the event of a ground evacuation for LOX or Battery Emergency, the BA should follow the crew brief and chock the mains after exiting. This means that the BA should first listen to the instructions given by the crew and follow them accordingly. After safely exiting the aircraft, the BA should then proceed to chock the mains, which refers to securing the main landing gear of the aircraft to prevent it from moving. This is an important safety measure to ensure that the aircraft remains stable during the evacuation process.

When required to OVER-WING fuel the C130J, the fuel hose should be routed over the leading edge. This means that the hose should be positioned in front of the wing, rather than behind it (trailing edge) or at the tip of the wing. Routing the hose over the leading edge ensures that fuel can be efficiently and safely transferred to the aircraft's tanks.

The correct answer is Utility, Booster, and Auxiliary. These are the three types of aircraft hydraulic systems. The utility system provides hydraulic power for various non-critical functions, such as landing gear extension and retraction. The booster system assists in operating the primary flight controls, such as the ailerons and elevators. The auxiliary system is responsible for powering secondary systems, such as cargo doors and brakes. These three systems work together to ensure the proper functioning of various aircraft components and systems.

The correct answer is 2,000 lbs each. This means that the aircraft pry bars, also known as Johnson Bars, are rated to withstand a maximum weight of 2,000 lbs each. This rating ensures that the pry bars are strong enough to handle heavy loads and provide the necessary leverage for tasks such as lifting or moving aircraft parts.

The APU door will not open fully during Emergency APU start.

The two hand axes are installed on the aircraft at the Aft FS 245 bulkhead LH side and aft of LH Paratroop door.

The statement is true because it states that all the overhead escape hatches have external release handles. This means that these escape hatches can be opened from the outside using the release handles provided.

The walk-around bottle recharging stations are located in both the FS 245 right side and the FS 617 right side of the cargo compartment.

During an emergency, it is crucial to provide the highest concentration of oxygen to the patient. By setting the O2 regulator diluter lever in the 100% Oxygen position, it ensures that the patient receives pure oxygen without any dilution. This is important because oxygen is essential for respiration and can help stabilize the patient's condition during an emergency. Therefore, the statement "True" indicates that setting the O2 regulator diluter lever in the 100% Oxygen position is the correct action during an emergency.

The correct answer is LH Nose FWD of battery access door and inside SPR access door. This means that the external ICS receptacles for ground crew voice communications are located in the left-hand nose area, forward of the battery access door, and inside the SPR (Special Purpose Receiver) access door.

An area trimmed in yellow on the C130J indicates egress points. Egress points are designated locations on an aircraft where crew members can exit in case of an emergency or evacuation. The yellow trim helps to highlight these points, making them easily identifiable in critical situations. This ensures that crew members can quickly and safely exit the aircraft when needed.

If during a power up check you find an ECB (Electronic Circuit Breaker) strapped open, the correct action to take is to check the EAL (Equipment Authorization List) for the reason why the ECB is strapped open. This is important because the ECB could be intentionally strapped open for a valid reason, such as during maintenance or troubleshooting. By checking the EAL, you can determine whether it is safe to unstrap the ECB or if further action is required.

The max horsepower for the AE 2100D3 is 4,700 (HP).

During a pre-flight check, the accumulator for the utility hydraulic system should ideally read 1,500 psi. However, a small variation of +/- 100 psi is considered acceptable and within the acceptable range. This means that the accumulator pressure can be as low as 1,400 psi or as high as 1,600 psi and still be considered within the acceptable range for the pre-flight check.

The utility system on the C130J operates on the flaps, main landing gear, nose landing gear, nose wheel steering, a portion of the flight controls, and normal brakes. This means that the utility system is responsible for controlling and operating these components of the aircraft during flight and landing.

The correct answer is orange smoke. This type of signal flare produces orange smoke when ignited.

The correct answer is 45,880 lbs. This is the total internal fuel capacity that the C130J aircraft can carry.

The plane produces and stores DC power using 2 batteries and 4 transformer rectifiers. The batteries provide the initial power supply, while the transformer rectifiers convert the AC power generated by the plane's engines into DC power. This combination of batteries and transformer rectifiers allows for a reliable and consistent source of DC power on the plane.

The AE 2100D3 engines use Mobile Jet II oil.

ACAWS stands for Advisory, Caution, and Warning System. This system is designed to provide information and alerts to users about potential hazards, risks, or issues that they need to be aware of. The system includes advisory messages, cautionary messages, and warning messages, each indicating different levels of severity. By using ACAWS, individuals can stay informed and take appropriate actions to prevent accidents or mitigate risks.

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Engine oil is used to actuate the propellers. Engine oil is a type of fluid that is specifically designed to lubricate and cool the internal components of an engine. It is also used to transfer power from the engine to other mechanical systems, such as the propellers. Engine oil has the necessary properties to withstand the high temperatures and pressures generated by the engine, making it suitable for use in actuating the propellers.

The emergency flap brake valve is located in the Utility System.

The stub shaft(s) for manually lowering the main landing gear are located under the Utility and Booster system reservoir at FS 469.

The emergency hydraulic nose landing gear extension valve handle is located aft of the LH forward Load Master ICS control box at eye level.

The fire extinguishers on the aircraft are located in multiple areas. They can be found on the flight deck at location 241, in the cargo compartment at location 245, on the left side of FS 617, and one is located aft of the LH Paratroop door.

The correct answer is 11. This suggests that there are 11 egress points on the C130J aircraft. Egress points are locations that allow for the exit or evacuation of personnel from the aircraft.

Aviation personnel are restricted from aerial flight for 12 hours after the last alcohol use and must have no residual effects. This time period allows for the body to metabolize and eliminate the alcohol from their system, ensuring that they are no longer under the influence and can safely operate an aircraft. It is crucial for aviation personnel to adhere to these restrictions in order to maintain the safety of themselves, their passengers, and others in the airspace.

The correct answer is "Door then the ramp." This means that when operating the ramp and door, the door should be opened first, followed by the ramp. This sequence is typically followed for safety reasons, as opening the door first allows for any potential hazards or obstacles to be identified and cleared before the ramp is deployed.

The wing life raft release handles on the C130J are located on each wing, below the forward escape hatch and above the toilet.

The CGU-1B (Cargo Straps) are used to secure lightweight cargo. They are not designed for heavy cargo or fragile cargo. The option "To tie down AET3 Neil Wilson to the landing gear" is not a valid use for cargo straps.

The circuit breaker for MC#2 is located in the Aft 245 RH MAIN/AV DC panel.

The correct answer is Florescent GREEN. The SEA DYE marker used in USCG Aircrew vests is fluorescent green in color. This color is chosen to enhance visibility and make it easier to locate individuals in emergency situations, especially in water environments.

The correct answer is two raised ridges. This suggests that the night end of the MK-124 MOD 0 SIGNAL FLARE can be identified by the presence of two raised ridges.

The emergency signal mirror is designed to reflect sunlight, making it visible from a distance. The fact that it can be seen up to 40 miles away on a sunny day indicates its effectiveness in attracting attention and signaling for help in emergency situations.

The Normal and Emergency Brake accumulators are located in the Nose Wheel Well.

The normal engine start sequence is 3,4,2,1. This means that step 3 is performed first, followed by step 4, then step 2, and finally step 1.

When the External PWR/APU switch is moved through the OFF position, the Integrated Control System (ICS) will be lost for a period of 10 seconds. This means that during this time, the aircraft's control system will not be functioning properly and certain functions may be temporarily unavailable. It is important for pilots and crew members to be aware of this temporary loss of control and take appropriate measures to ensure the safety of the aircraft and its occupants.

After NP (Ng Propeller) is on speed, it can take up to 2 minutes for the propeller to rotate when starting a new engine. This delay is due to the time required for the engine to build up enough power and for the propeller to reach its operational speed.

Core bolts on the aircraft floor can be recognized by their alignment with two screws on the floor. This means that the bolts are positioned in a straight line with two screws. This alignment helps to ensure that the bolt is securely fastened and provides stability to the aircraft floor. The other options mentioned, such as having a square washer, being painted green, or having a flat side, do not specifically indicate the recognition of a core bolt on the aircraft floor.

Dowty is the correct answer because they are the company responsible for making the propeller for the C-130J.

When manually lowering the flaps, they should be moved slowly in 10% increments because the flap brakes are no longer operational. Moving the flaps slowly allows the pilot to monitor for any asymmetrical condition, such as one flap moving faster or slower than the others. By moving the flaps in small increments, any potential issues can be detected and addressed before they become a safety concern.

Pinning the paratroop doors in the closed position can lead to various issues. Firstly, it could cause damage to the door, which may affect its functionality. Secondly, in case of an emergency egress, the door could stick, making it difficult for the paratroopers to exit quickly and safely. Lastly, the door pin is not designed to be used for keeping the doors closed, so doing so could result in unforeseen problems. Therefore, all of the mentioned reasons explain why the paratroop doors should never be pinned in the closed position.

The main landing gear extension wrench is located in the forward (FWD) area of the utility system, behind a litter stanchion.

The tie-down rings on the cargo floor are rated for a maximum weight capacity of 10,000 lbs. This means that they are designed and tested to safely secure and hold items weighing up to 10,000 lbs during transportation. It is important to adhere to this weight limit to ensure the safety and stability of the cargo and the vehicle.

A BA should start their preflight with enough time to ensure that all preflight items are complete before the Aircraft Commander arrives. This ensures that all necessary checks and preparations are done before the aircraft is ready for takeoff. Starting the preflight earlier allows for any potential issues or discrepancies to be addressed and resolved in a timely manner, ensuring a smooth and efficient operation.

The primary duty of a fire guard when standing is to ensure the safe egress of the crew. This means that their main responsibility is to make sure that all crew members are able to safely exit the area in the event of a fire. This includes being aware of escape routes, assisting crew members if needed, and ensuring that everyone is accounted for during an evacuation.

The O2 mask(s) should be checked during the preflight. This is because the preflight check is conducted before every flight and ensures that all necessary equipment, including the O2 masks, are in proper working condition. Checking the O2 masks during the preflight allows any issues or malfunctions to be identified and addressed before the flight takes off, ensuring the safety and well-being of the crew and passengers.

The correct answer is "Through their full travel". This means that the life raft release handles must be pulled all the way until they have completed their full range of motion in order for the life raft to be fully ejected and inflated.

Before applying power, it is important to ensure that the cargo door manual control valve handle and ramp manual control knob are set to 6N/NEUT position, and that the auxiliary hydraulic switches are OFF. This ensures that the cargo door and ramp are in the correct position and that the auxiliary hydraulic system is not activated, preventing any potential accidents or damage during power application.

If the core bolts/washers are found loose or missing from the restraint rail sections, it will restrict the aircraft from flying. The core bolts/washers are important components that secure and hold the restraint rail sections in place. Without them, the restraint rail sections may become unstable or detached, posing a safety risk and preventing the aircraft from being able to fly.

The correct answer is "Lower side of the life raft compartments". This is because the question is asking about the absence of a life raft, and the lower side of the life raft compartments is where the life raft would typically be stored. By inspecting the windows on the lower side of the life raft compartments, one should be able to determine if the life raft is present or not.

In the event of a gear up landing, it is important to open exits that are easily accessible and provide a safe means of evacuation. Overhead escape hatches, side exits, and paratroop doors are the most suitable options for this situation. These exits are strategically located and designed to allow for a quick and efficient evacuation of the aircraft. Opening these exits will ensure that passengers and crew members can safely exit the aircraft in case of an emergency.

Section 3 of the CGTO 1C-130J-1 Flight Manual covers Emergency Procedures. This section provides guidance and instructions on how to handle various emergency situations that may arise during flight operations. It includes procedures for engine failures, fires, electrical malfunctions, and other critical emergencies. Pilots and crew members can refer to this section for step-by-step instructions on how to respond and mitigate these emergencies, ensuring the safety of the aircraft and its occupants.

The safety strap for airdrops is secured to Flight Station (FS) 617.

The maximum restraint weight for the CGU-1B (Cargo Strap) is 5,000 lbs. This means that the strap is designed and tested to safely secure cargo weighing up to 5,000 lbs, ensuring that it remains in place during transportation.

The correct answer is Ramp and Door, Ground tie-valve, Emergency brakes and Emergency NLG extension.

The auxiliary hydraulic system is responsible for providing pressure to various components in an aircraft. In this case, it provides pressure to the ramp and door, allowing them to open and close smoothly. It also supplies pressure to the ground tie-valve, which is used to secure the aircraft on the ground. Additionally, the auxiliary hydraulic system provides pressure to the emergency brakes, allowing for quick and effective stopping in emergency situations. Lastly, it provides pressure for the emergency NLG (Nose Landing Gear) extension, which is used if the normal landing gear fails to deploy.

During cold refueling operations, the minimum required fire extinguisher is one 150 lb Dry Chemical. This is because cold refueling operations involve handling flammable liquids such as jet fuel, which can pose a fire hazard. A 150 lb Dry Chemical fire extinguisher is capable of extinguishing larger fires and provides a higher level of fire protection compared to a 20 lb Dry Chemical extinguisher or a water can.

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The correct answer is Main tanks and Externals. This means that both the main tanks and the external tanks can be fueled "over the wing". "Over the wing" fueling refers to the process of refueling an aircraft by connecting the fuel hose to the wing fuel ports. In this case, both the main tanks, which are located in the wings, and the external tanks, which are attached to the wings, can be fueled in this manner.

The hydraulic systems on a plane are categorized into three types: utility, booster, and auxiliary. The utility system is responsible for operating various components such as landing gear, flaps, and brakes. The booster system assists in controlling the flight controls, providing additional power to the pilot. The auxiliary system supports functions like cargo doors and thrust reversers. These three systems work together to ensure the proper functioning of different aircraft components and systems.

Entering and exiting the nose wheel well from the left side is necessary to prevent burns from venting LOX. LOX stands for liquid oxygen, which is highly flammable and can cause severe burns if it comes into contact with skin. By using the left side, which is away from the venting LOX, the risk of accidental exposure and burns is minimized.

During Main Landing Gear tiedown, if 25,000-pound tiedown chains are not available, three connectors (tiedown devices) and seven 10,000-pound chain segments are required to tie down each pair of opposite struts. This is necessary to ensure the proper securement and stability of the landing gear.

The correct answer is 83282 or 87257. These numbers refer to the type of fluid used by the hydraulic systems on the plane.

Smoking, open flames, and spark producing items need to be kept at a distance of 50ft from refueling operations. This is important to ensure safety and prevent any potential accidents or fires that could occur due to the ignition of flammable substances. By maintaining this distance, the risk of sparks or flames coming into contact with fuel is minimized, reducing the likelihood of a hazardous situation.

After discharging the first bottle of agent as required, if the condition of the APU fire persists, it is recommended to wait for a minimum of 15 seconds before discharging the remaining bottle. This allows for a brief interval to assess the effectiveness of the first discharge and determine if further action is necessary.

The correct answer is "There is no pin through the shaft." This means that the input shaft for the main landing gear does not have a pin running through it. This could be identified by visually inspecting the shaft and observing that there is no pin present.

The given signal described in the question is used to indicate the action of disconnecting the Auxiliary Power Unit (APU) during ground handling of the aircraft. The pilot pulls the extended index finger of the right hand from the palm of the left hand to communicate this instruction to the ground crew member. This signal is important for ensuring proper coordination and communication between the pilot and the ground crew during aircraft operations.

The LOX system shutoff valve is located on the right side of the Aft 245 bulkhead.

The control panel for the aft cargo lighting is located over the ramp and doors controls.

The stub shaft(s) for manually lowering the flaps are located directly under the Utility hydraulic system.

The correct hand signal from the Director to the Pilot to "STOP" at position is when the Director raises both hands to eye level, with palms facing the pilot in a gesture similar to a policeman's stop signal. This signal clearly communicates to the pilot that they need to stop the aircraft at their current position.