2A552 Test 2 Aircraft

Flares are considered "explosives-loaded" because they contain pyrotechnic materials that can be ignited to produce a bright light and smoke. These materials have the potential to cause an explosion if mishandled or ignited inappropriately. Therefore, the presence of flares on an aircraft would classify it as "explosives-loaded."

Before moving an explosives-loaded aircraft into a hangar, it is necessary to remove all ammunition and explosives. This precaution is essential to ensure the safety of personnel and the hangar itself. By removing these hazardous materials, the risk of accidental ignition or explosion is significantly reduced. It is important to follow proper procedures and protocols to prevent any potential accidents or damage.

After the last flight of a flying period, a basic post-flight inspection should be performed. This type of inspection is conducted to ensure that the aircraft is in a safe and airworthy condition after the flight. It involves a thorough examination of the aircraft's exterior, including the fuselage, wings, control surfaces, and landing gear. The inspection also includes checking for any signs of damage, leaks, or abnormalities that may have occurred during the flight. This inspection is crucial to identify any potential issues and address them before the next flight.

The Air Force core values are integrity, service before self, and excellence. These values represent the guiding principles and moral compass for members of the Air Force. Integrity refers to being honest, ethical, and doing the right thing even when no one is watching. Service before self emphasizes the importance of putting the needs of others and the mission before personal interests. Excellence means striving for the highest standards of performance and constantly seeking improvement in all aspects of one's duties. These core values help shape the culture and behavior of Air Force personnel.

When people are taught the right way to do something, they are also being taught the safe way. This implies that the correct method of doing something is not only efficient and effective, but also ensures the safety of individuals involved. Teaching the safe way emphasizes the importance of following proper procedures and guidelines to minimize risks and potential harm. It promotes a culture of safety and encourages individuals to prioritize their well-being while performing tasks or activities.

If the red fire extinguisher thermal discharge indicator is missing, it indicates that one or both fire bottles have discharged. The thermal discharge indicator is a visual indication that shows whether the fire extinguisher has been discharged due to high temperature. If the indicator is missing, it suggests that the fire bottles have been discharged and need to be replaced.

AFTO Form 95, Significant Historical Data, serves as a permanent history of significant actions for an aircraft. This form is used to document important events, modifications, repairs, and other significant information related to the aircraft. It provides a comprehensive record that can be used for maintenance, safety, and historical purposes. The form helps to track the aircraft's maintenance history and can be referenced in the future to ensure proper maintenance and safety procedures are followed.

If the main transmission on an H-60 helicopter loses all of its oil, it can still operate at cruise for a maximum of 30 minutes. This is because the main transmission relies on oil for lubrication and cooling, and without it, the transmission will eventually overheat and fail. The 30-minute timeframe allows for a limited amount of time to safely land the helicopter before the transmission becomes damaged beyond repair.

When removing the input module from an H-60 power train, if it is difficult to pull it free from the main module, using bolts can help break it loose.

The correct answer is "of supply" because critical items are typically related to supplies or resources that are essential for an organization or operation. Therefore, it makes sense that the local chief of supply would be responsible for designating these critical items.

The correct answer is XD or XF. The explanation for this answer is that the expendability, recoverability, reparability codes (ERRC) XD and XF are both considered repair asset codes. This means that assets with these codes can be repaired if they become damaged or non-functional. The XD code indicates that an item is repairable, while the XF code indicates that an item is reparable. Therefore, assets with either of these codes can be repaired and are classified as repair assets.

The internal bypass flow in the T700 fuel boost pump provides approximately twice the maximum fuel-flow. This means that the pump is capable of delivering fuel at a rate that is twice the maximum flow required by the engine. This allows for a higher fuel flow capacity and ensures that the engine receives an adequate fuel supply even under high demand conditions.

The commander ensures that property is receiving proper care and is being properly safeguarded by making frequent visits to base activities. This allows the commander to personally assess the condition and handling of the property, identify any issues or concerns, and take appropriate actions to address them. Inspecting the property on issue or turn-in may only provide a snapshot view of the property at a specific point in time and may not capture its overall care and safeguarding. Obtaining written reports from supervisors may provide some information, but it may not be as comprehensive or accurate as firsthand observations during frequent visits.

When an individual has acquired physical possession of government property, they assume custodial responsibility. This means that they are responsible for the safekeeping, maintenance, and proper use of the government property under their control. They are expected to ensure that the property is not lost, damaged, or misused, and to report any issues or discrepancies promptly. Custodial responsibility emphasizes the importance of accountability and proper stewardship of government resources.

When setting the torque wrench for torquing a self-locking nut for a tail drive shaft clamp, you need to take into account the nut friction torque and add it to the required torque value. This is because the nut friction torque creates resistance that needs to be overcome in order to achieve the desired level of tightness. By adding the nut friction torque to the required torque value, you ensure that the correct amount of torque is applied to the nut.

A self-locking nut is designed to prevent loosening due to vibrations or other external forces. It achieves this by having a special thread pattern that creates friction and resistance when tightened. In order for the nut to have maximum locking effect, at least two threads must be showing through the nut. This ensures that there is enough engagement between the nut and the bolt to provide sufficient friction and locking force, minimizing the chances of the nut coming loose.

If you discover an error in the technical order (TO) that involves flight safety and could result in serious injury, it is important to submit a TO deficiency report immediately. This is because flight safety is a critical concern and any potential risks should be addressed promptly to prevent accidents or injuries. Waiting for 30 days, the next TO revision, or one to five days before the next flight could lead to unnecessary delays and potential harm. Therefore, immediate action is necessary in such cases.

The correct answer is cyclic control. The cyclic control is a control stick that is located between the pilot's legs and is used to control the pitch and roll of the helicopter. By moving the cyclic control forward or backward, the pilot can control the longitudinal movement of the helicopter, causing it to move forward or backward. Therefore, the longitudinal movement of the H-60 helicopter is accomplished by movement of the cyclic control.

The correct answer is "Spray unit cart" because it refers to a cart that is specifically designed for spraying or cleaning engines. This cart is equipped with a spray unit that can be used to wash engines or remove dirt and debris. The other options, such as "Hobart" and "Soap/water cart," do not accurately describe a cart used for engine washing. "Corrosion control cart" is also not a suitable alternative name for an engine wash cart as it implies a different purpose or function.

When the motor is running on the hydraulic test stand, the valve that should be pressed to relieve any trapped air in the system from the fill and bleed operation is the "Bleed" valve. This valve is specifically designed to release any air pockets that may have been trapped during the filling process, ensuring that the hydraulic system operates smoothly and efficiently. By pressing the "Bleed" valve, any air bubbles or pockets will be expelled, allowing for optimal performance of the system.

To check the H-60 central display unit (CDU) dimming feature, a flashlight would be used. This is because a flashlight can be used to simulate various lighting conditions and check if the CDU dimming feature is functioning properly. It allows the user to assess the visibility and readability of the display unit under different lighting levels.

Emotional irritability is not a sign of fuel vapor inhalation. Fuel vapor inhalation can cause symptoms such as dizziness, headaches, and muscular incoordination. However, emotional irritability is not typically associated with fuel vapor inhalation.

The correct answer is fuel. In the H-60 fuel quantity indicating system, the item used as the dielectric is the fuel itself. A dielectric is a material that is placed between two conductive plates to store electrical energy. In this system, the fuel acts as the dielectric, allowing the measurement of the fuel quantity based on the electrical capacitance between the plates. The alternating current (AC) or direct current (DC) current options are incorrect as they do not accurately describe the item used as the dielectric in this specific system.

Air Force bases and activities typically establish and maintain Limited technical order (TO) files. Limited TO files contain essential TOs that are required for the proper operation and maintenance of equipment, but they do not include every single TO available. Limited TO files are curated to ensure that only the most critical and frequently used TOs are readily accessible, making it easier for personnel to find the information they need quickly and efficiently.

When you place an H-60's WINDSHIELD ANTI-ICE COPILOT switch to the ON position, you should feel heat on the copilot's windshield in approximately five minutes.

When approaching the plane of rotation of the main rotor blades, it is important to exercise caution during engine runup and shut down because the rotor blades tend to droop at decreased speeds. This means that as the speed of the rotor blades decreases, they may sag or hang down lower than usual. This can pose a safety risk if not taken into account, as it could lead to contact with the ground or other objects. Therefore, it is important to be aware of this tendency and take appropriate precautions when approaching the rotor blades.

The most likely cause of a birdcaged rescue hoist cable on an H-60 is the hook bearing not rotating freely. This means that the bearing that allows the hook to rotate and move freely is likely stuck or not functioning properly. This can cause the cable to become twisted and tangled, resulting in a birdcaged cable.

Using leather gloves and maintaining tension on the cable is the correct answer because leather gloves provide better protection against potential injuries and cable fouling compared to rubber gloves. Maintaining tension on the cable helps to prevent it from becoming tangled or snagged during the raising or lowering process, ensuring a smooth and safe operation.

The minimum safe distance between aircraft when refueling is 50 feet. This distance is necessary to ensure the safety of both the aircraft and the personnel involved in the refueling process. Being too close can increase the risk of accidents, such as fuel spills or ignition. Therefore, it is important to maintain a sufficient distance to minimize any potential hazards and ensure a safe refueling operation.

A fire occurring in electrical equipment is a class C fire. Class C fires involve energized electrical equipment, such as appliances, wiring, circuit breakers, and outlets. These fires are caused by electrical faults or malfunctions and can be extremely dangerous. It is important to use appropriate fire extinguishers or methods specifically designed for class C fires to safely extinguish them.

A schematic is a visual representation of a system or circuit that uses symbols to represent the various components and their connections. It provides a simplified and easy-to-understand overview of the system, allowing technicians to identify and understand how different parts of the system are connected and interact with each other. Therefore, a schematic is a valuable troubleshooting aid as it promotes understanding of the system and helps technicians diagnose and fix any issues that may arise.

The correct answer is B because a fire occurring in paints, cooking oil, grease, and petroleum products falls under Class B fires. Class B fires involve flammable liquids and gases.

The proper positioning of fire extinguishers is determined by distance criteria. This means that fire extinguishers should be placed at a distance that allows for easy access and quick response in case of a fire emergency. The goal is to ensure that fire extinguishers are conveniently located and within a reasonable distance from potential fire hazards. By considering distance criteria, fire extinguishers can be strategically placed throughout a building to maximize their effectiveness in suppressing fires.

The correct answer is 8,000 pounds. This means that the capacity of the cargo hook on the H-60 helicopter is 8,000 pounds. This indicates that the cargo hook is capable of lifting and carrying a maximum weight of 8,000 pounds.

The correct answer is "second stage of the tail rotor (TR) servo." The utility module on the H-60 helicopter is responsible for connecting hydraulic pressure to the various components of the aircraft. In this case, it specifically connects the hydraulic pressure to the second stage of the tail rotor (TR) servo. This is important because the TR servo is responsible for controlling the pitch of the tail rotor blades, which helps to stabilize the helicopter during flight. By connecting hydraulic pressure to the second stage of the TR servo, the utility module ensures that the tail rotor functions properly and contributes to the overall control and maneuverability of the helicopter.

When servicing the upper stage of the shock strut, releasing the parking brake is necessary to avoid placing undue stress on the brake assembly. This is because the parking brake holds the tire in place and applying force to the upper stage of the shock strut while the parking brake is engaged can cause unnecessary strain on the brake assembly. By releasing the parking brake, the tire is free to move and the stress on the brake assembly is minimized.

Before servicing an H-60 landing gear strut with nitrogen, you must ensure there are no hydraulic fluid leaks. This is because if there are leaks in the hydraulic fluid system, it can cause contamination and potential damage to the landing gear strut. Therefore, it is important to address any hydraulic fluid leaks before proceeding with the nitrogen servicing to ensure the proper functioning and safety of the landing gear strut.

The master cylinder allows for thermal expansion when the brakes on an H-60 are off. The master cylinder is responsible for converting the force applied to the brake pedal into hydraulic pressure, which then activates the wheel brake assembly. When the brakes are not in use, the master cylinder allows for any thermal expansion or contraction of the brake fluid, ensuring that the brakes remain in proper working condition.

The correct answer is fork assembly. The attachment point for the tail wheel assembly on the H-60 tail landing gear is the fork assembly. The fork assembly is responsible for connecting the tail wheel to the rest of the landing gear system, allowing it to rotate and move as necessary during landing and taxiing. The axle assembly, yoke assembly, and shock strut are not specifically mentioned as the attachment point for the tail wheel assembly in the given question.

In the given configuration, the proprotor blades are folded toward the fuselage, the nacelles are rotated to the horizontal position, and the wing is rotated 90 degrees. This configuration is known as "FULL STOW."

The correct answer is Green. The engine monitoring system's (EMS) electrical harness is color-coded in green for identification purposes.

The correct answer is that each flag is half black and half white. This indicates that the lock pins are disengaged. The half black and half white design is commonly used to visually represent the status of a lock or latch. In this case, the half black portion indicates that the lock pins are not engaged, while the half white portion indicates that they are disengaged. This design allows for easy identification and ensures that the lock pins are clearly visible to the operator.

The search/landing lights must be extended by 10 degrees before they can be turned on.

A wire harness that consists of both conventional (individually shielded and/or unshielded) wires and integrated wiring system (IWS) wires is called a hybrid wire harness. This type of harness combines different types of wires to accommodate various electrical systems and components. The term "hybrid" refers to the mixture of conventional and integrated wiring system wires in the harness.

The ground lockpin is manually installed as a backup safety mechanism to prevent accidental landing gear retraction and to facilitate post-flight servicing and maintenance for the internal drag strut actuator locks. This lockpin securely holds the landing gear in place, ensuring that it does not retract unintentionally. It can be easily installed and removed by ground crew during maintenance procedures, providing an additional layer of safety and convenience.

The correct answer is "Hike." In the context of the question, "Hike" refers to the system on the NLG (Nose Landing Gear) that provides the means to raise the nose of the aircraft during ground maintenance and towing. This system allows for the adjustment of the aircraft's nose position, which is necessary for various maintenance tasks and ground operations.

The PFCS (Primary Flight Control System) combines mechanical, electronic, and hydraulic functions to transmit pilot or copilot inputs to components that control the aircraft. This means that the system utilizes mechanical linkages, electronic sensors, and hydraulic actuators to convert the pilot's input into commands that control the aircraft's movement and stability.

The correct answer is Air Force technical order (AFTO) Form 781, AFORMS (Air Force Operations Resource Management System) Aircrew/Mission Flight Data Document. This form is the source document for logging flight activity for individuals.

The Maintenance Group Commander (MXG/CC) appoints the crashed, damaged, or disabled aircraft recovery (CDDAR) Team Chief. This individual is responsible for overseeing the recovery operations of aircraft that have been involved in accidents or are in a disabled state. The MXG/CC, being in charge of the maintenance group, has the authority to select and assign the most suitable person for this crucial role.

AFTO Form 350, Reparable Item Processing Tag, is used for internal control of a repair cycle asset item. This form is specifically designed for tracking and documenting the repair process of an item. It includes important information such as the item's identification, condition, and repair actions taken. By using this form, the organization can ensure proper accountability and management of repair cycle assets.

The scroll vanes of the T700 engine are anti-iced by hot scavenge oil. This means that the oil that is used to scavenge and remove excess heat from the engine is also used to prevent ice formation on the scroll vanes. The hot oil is directed to the vanes, which helps to keep them free from ice and ensures proper engine performance. This method of anti-icing is more efficient and effective compared to using bleed-air or electrical heating elements.

The correct answer is "As a separate item from the training." This means that the item should not be considered or included as part of the training. It should be treated separately and not be seen as an integral component of the training process.

The C-8 type tensiometer is capable of measuring cable tension from 10 to 200 pounds with an accuracy of 95 percent. This means that the tensiometer can accurately measure cable tension within this range with a high level of precision. The accuracy of 95 percent indicates that the measurements taken by the tensiometer will be very close to the true value of the cable tension.

The Aircrew and Maintenance Debrief Section uses the Maintenance Information System (MIS) to identify and track Repeat/Recur discrepancy trends. They also document the discrepancies on Air Force Technical Order (AFTO) Form/IMT 781A after an aircraft flight is completed. This section is responsible for gathering information from both the aircrew and maintenance personnel to ensure that any recurring issues are properly addressed and documented.

When the battery voltage on the digital protractor drops below 7 volts, the LCD displays "LOW BAT". This indicates that the battery is running low and needs to be replaced or recharged.

The correct answer is yellow air service indicator flag. On the -86 generator control panel, a clogged air filter is indicated by a yellow air service indicator flag. This flag serves as a visual indication to the operator that the air filter needs to be cleaned or replaced. The yellow color is used to distinguish this indicator from other indicators on the control panel.

The cellophane wrap on the separation membranes of the Self Generating Nitrogen Servicing Cart (SGNSC) is necessary for both proper function and nitrogen production. It serves a purpose in the functioning of the cart and is also involved in the production of nitrogen.

Before performing an H-60 electrical continuity check, it is important to remove all power from the circuit being checked. Failure to do so could result in damage to the multimeter.

The maximum height of the B-7 stand is 16 feet.

TO 1H-1(H)G-6 is the correct answer because it is the technical order that establishes functional-check-flight requirements for the HH-60G helicopter. The other options, TO 1H-1(H)G-01, TO 1H-1(H)G-17, and TO 1H-1(H)G-2-1, do not pertain to the functional-check-flight requirements for this specific helicopter model.

When using compressed air for cleaning, it is important to use a diffuser nozzle to distribute the air evenly and reduce the risk of injury. Additionally, it is crucial to ensure that the pressure does not exceed 30 pounds per square inch (psi). This is because higher pressures can cause harm to the surfaces being cleaned or potentially injure the person operating the equipment. Therefore, maintaining a pressure of 30 psi or below is recommended to ensure safe and effective cleaning.

Ground resonance is a helicopter flight characteristic that usually develops during takeoff or landing when the helicopter is 87 to 95 percent airborne. It occurs when the rotor blades become unbalanced and cause the helicopter to vibrate violently. This can be caused by uneven weight distribution or a mechanical issue with the rotor system. Ground resonance can be dangerous and may lead to severe damage or even the loss of control of the helicopter.

When the H-60 refuel probe is extended, the fuel from the retract side of the probe flows to the No. 2 main fuel tank.

The correct answer is 170 gallons. This is because the question states that the H-60 internal auxiliary fuel tank is single point refueled, which means that it can hold a larger amount of fuel compared to other refueling methods. Therefore, the tank can hold 170 gallons of useable fuel.

Removing rust is not part of corrosion prevention because rust is already a form of corrosion. Once rust has formed, it means that the metal has already undergone a chemical reaction with oxygen and moisture, resulting in the formation of iron oxide. Therefore, removing rust is considered a form of corrosion repair or treatment, rather than prevention. To prevent corrosion, measures such as cleaning, painting, and inspecting for early detection are necessary to protect the metal from exposure to moisture and other corrosive elements.

Cheesecloth is not suitable for cleaning exterior plastic surfaces because it is a loosely woven fabric that is typically used for straining liquids or wrapping cheese. Its texture and structure make it less effective for cleaning as it may leave behind lint or fibers on the plastic surface. Flannel cloth, soft cotton cloth, and diaper type cloth are all better options for cleaning exterior plastic surfaces as they are generally more absorbent and less likely to leave residue.

The correct answer is 60% water and 40% methanol or isopropyl alcohol. This is because when washing the engines in cold temperatures, it is important to use a water solution with a higher percentage of alcohol to prevent freezing. Methanol or isopropyl alcohol has a lower freezing point than water, so a higher concentration of alcohol will ensure that the solution remains in a liquid state and effectively cleans the engines.

The explosive cartridge (squib) on the H-60 cargo hook is used to release the load during an emergency. This means that in a critical situation, such as a malfunction or emergency landing, the explosive cartridge is activated to quickly and safely release the load from the aircraft. This allows for the load to be detached and prevents any further complications or dangers during the emergency situation.

The cabin floor limit load is measured in pounds per square foot. The correct answer is 300, indicating that the maximum weight that the cabin floor can support is 300 pounds per square foot.

The nacelle is the mount assembly that provides a means for attaching the proprotor gearboxes, transmission adapters, and conversion spindles to the nacelle structure. The other options, integrated structural accessory and multiple accessories, do not specifically refer to the mount assembly for attaching these components.

The correct answer is cabin. After installation, the H-60 vibration absorber requires a tuning weight adjustment using the 8500 Balancer/Analyzer and functional check flight in the cabin. This suggests that the vibration absorber is located in the cabin of the H-60 aircraft.

The upper door is the only one that is given emergency opening provisions. This suggests that in case of an emergency, such as a fire or evacuation, the upper door can be opened quickly and easily to ensure the safety of the occupants inside the cabin. The other doors may have normal opening/closing mechanisms but do not have specific provisions for emergency situations.

The APU starter is a high-speed motor because it needs to provide a quick and powerful start to the auxiliary power unit. The APU is responsible for providing power to various systems on an aircraft when the main engines are not running, so it requires a motor that can rapidly spin up to get the APU running efficiently.

The breather component of the midwing gearbox (MWGB) oil system is responsible for venting the gearbox to the atmosphere. This allows for the equalization of internal and external case pressure.

The integral overrunning clutch is the component that engages and disengages the auxiliary power unit (APU). This clutch allows the APU to run independently from the main engine and provides power for various aircraft systems when the main engines are not running. It allows the APU to start and stop without affecting the main engine, ensuring smooth operation and flexibility in power generation.

The additional component in the left proprotor gear box (PRGB) that provides for the counter-rotation of the proprotors is the idler gear. The idler gear is responsible for transmitting the rotational force from the main rotor to the left proprotor, allowing it to rotate in the opposite direction. This counter-rotation is necessary for maintaining balance and stability during flight. The flex coupling, curvic coupling, and spindle adapter are not directly involved in providing counter-rotation in the PRGB.

A curvic adapter allows for a more solid connection between a driveshaft and its couplings. The curvic design consists of interlocking teeth on both the driveshaft and the coupling, ensuring a secure and precise fit. This type of adapter is commonly used in high-torque applications where a strong and reliable connection is essential.

The correct answer is proprotor blade. The given statement suggests that the planetary assembly is mounted to something, and out of the options provided, the proprotor blade is the only one that can be mounted to the planetary assembly. The other options, such as cam set plate, blade fold support, and pitch lock mechanism, do not logically fit with the given statement. Therefore, the proprotor blade is the most suitable option.

Pendulum damper assemblies are designed to reduce rotor-induced vibrations and provide anti-ice protection for the proprotor blade assemblies. These assemblies consist of pendulum weights that help dampen the vibrations caused by the rotation of the rotor blades. Additionally, they are equipped with anti-icing systems that prevent ice buildup on the blades, ensuring safe and efficient operation of the proprotor.

The correct answer is "visible from the top and the bottom." This means that the LED light assemblies on the proprotor blades can be seen from both the top and the bottom. This is important for safety purposes, as it allows the lights to be visible to other aircraft or personnel from any direction. It ensures that the proprotor blades are easily noticeable in low light or night conditions, enhancing the overall visibility of the aircraft.

The GRDP (Ground Refuel Distribution Panel) is the component that controls and monitors ground fuel system servicing. It is responsible for distributing fuel to various aircraft and monitoring the fuel levels. The other options mentioned, PFSA and Aerial refuel/defuel panel, are not specifically designed for controlling and monitoring ground fuel system servicing.

The dome lights in the cabin are identical and interchangeable. Each dome light contains two incandescent lamps, one with an opaque lens and one with a green night vision imaging system (NVIS) lens. The dome lights are typically used for general illumination in the cabin area.

The correct answer is DAY NORM. In the flight compartment lighting system, the DAY NORM mode of operation has the maximum brightness levels set for affected cockpit lights. This mode is used during daylight operations to provide adequate lighting for the cockpit without causing discomfort or glare for the pilot. It ensures optimal visibility and allows the pilot to easily read instruments and displays.

The correct answer is "ON." This suggests that the GRDP (presumably referring to some kind of device or system) operates in an active or functioning mode. It is not turned off or in a standby state, but rather in an operational state. The other options, "OFF," "REFUEL," and "NORMAL," do not provide any indication of the mode of operation and are therefore incorrect.

FMU 1 (left FMU) is the correct answer because it is the component that provides control and monitoring of the fuel CG management system operation for the left side of the aircraft. Additionally, it also monitors the low level sensor in the left feed tank. This means that FMU 1 is responsible for managing the fuel system on the left side of the aircraft and ensuring that fuel levels are monitored and maintained properly.

The correct answer is fuel quantity probe. In auxiliary fuel cells indication systems, the fuel quantity probe is the only component that is present. The fuel quantity probe is responsible for measuring the amount of fuel in the auxiliary fuel cells and providing an indication of the fuel level. The other options, such as overfill sensors, low level sensor, and jettison shutoff valve, are not specific components of the auxiliary fuel cells indication systems.

When the flap control panel lever is set at F (Full), the flaps are set to 72.5 degrees.

The correct answer is Fluid compensation valve. The fluid compensation valve is used to shuttle the additional hydraulic fluid gained by hydraulic system 1 during APU clutch and ground check out operations back into hydraulic system 3. This valve ensures that the hydraulic fluid is properly distributed and balanced between the different hydraulic systems. The compensator, charging valve, and system return check valve are not specifically designed for this purpose.

The correct answer is Five. This means that the Air Force uses five authorized inspection concepts.

AFTO Form 781J is the correct answer because it is specifically designed to record aircraft time, engine data, and includes operating times. This form is used to document important information such as operating time, cycle, and oil added during a flight, making it an essential tool for maintenance and tracking purposes.

The correct answer is "The –9 TO of the aircraft you are using for transport." This answer suggests that you should consult the -9 Technical Order (TO) of the specific aircraft you are using for transport. This TO would provide guidance on how to properly load and offload a helicopter onto the transport aircraft.

The correct answer is two lubrication pumps operating in parallel. This means that there are two pumps working simultaneously to provide lubrication to the main transmission of the H-60. Operating in parallel ensures redundancy and reliability, as if one pump fails, the other can still provide lubrication. This setup also allows for increased efficiency and smoother operation of the transmission system.