ASA Assembly & Rigging Practice Test

These questions are part of the practice quiz. Start practicing

• Where is breakage most likely to occur in control cable wires?
• Why are locknuts or lock washers commonly used in assembly?
• What is a probable effect of having exceptionally tight cables in an airplane with correct control travel?
• What should be checked after rigging adjustments are made?
• What is the effect of increasing dihedral on an airplane's lateral stability?
• If a monoplane's right wing is rigged to a greater angle of incidence than recommended, what will be the consequence?
• Which component is vital for achieving the correct path for control cables?
• What is a common indicator of improper elevator rigging?
• Which of the following ensures that components are held together securely in aviation assembly?
• Which part of a helicopter is most affected by torque during flight?
• Which control surface is associated with differential control?
• If a pilot reports that an airplane flies left wing heavy, this condition may be corrected by?
• What type of control cable is frequently used for flight controls?
• What is the acceptable cable tension range for a 3/16 cable at 80°F?
• In aircraft terminology, what does the dihedral angle refer to?
• How can the dihedral angle of a wing be precisely measured?
• The vertical flight of a helicopter is controlled by?
• What is the primary function of control surface rigging?
• Which nondestructive checking method is commonly employed to verify swaged-type terminal installation on control cables?
• In a helicopter, the collective control is used primarily to adjust what?
• What issue may arise if control surfaces are not properly aligned during rigging?
• Which performance aspect can be affected by improper rigging of the wing?
• What is the definition of the buttock line in aircraft terminology?
• What effect does wash-in the left wing of a monoplane have on lift and drag?
• During flight, if the angle of incidence changes, what consequence might occur?
• After a rudder has been repaired or re-covered, what is the next step?
• What should you avoid when inspecting a control cable for wear?
• What component may be adjusted to calibrate the pitch of the elevator?
• In aircraft assembly, what does precision in measurement ensure?
• Why should safety wire be installed on critical fasteners?
• Why is it typically required to jack an aircraft indoors for weighing?
• What type of angle is associated with the dihedral setup of a wing?
• What is the primary purpose of an assembly in aviation?
• What is critical to ensure when installing control surfaces?
• What does differential control on an aileron system primarily indicate?
• In a hovering helicopter equipped with a tail rotor, directional control is maintained by?
• What is the primary concern with using non-standard fasteners in assembly?
• Which characteristic is vital for materials used in assembly?
• The elevators on a conventional airplane are primarily used to achieve rotation about which axis?
• What is the minimum cable size permissible in aircraft primary control systems?
• How does incorrect component installation affect an aircraft?
• When is the use of a digital torque adapter recommended?
• What does the term "rigging" refer to in the context of aircraft systems?
• Why is it crucial to balance control surfaces?
• What action should be taken once the aircraft is securely jacked?
• What is the purpose of a turnbuckle in rigging?
• How is the chord of a wing defined?
• What function does a universal propeller protractor serve?
• Movement about the lateral axis (pitch) in a helicopter is affected by which control?
• Which instrument is typically used to check the alignment of wings during assembly?
• What happens to the tension of a control cable if the temperature drops significantly after it was tensioned?
• What does the term "string line" mean in rigging?
• In rotorcraft external-loading, the ideal location of the cargo release is where the line of action passes?
• What is the primary purpose of conducting visual inspections during assembly?
• If the control stick is moved rearward and to the left, what happens to the right aileron?
• The auxiliary (tail) rotor of a helicopter permits the pilot to compensate for and/or accomplish which of the following?
• What type of materials may be used for control surface hinges?
• During assembly, what might a technician check for signs of corrosion?
• In a primary control system, which type of cable is commonly used?
• What type of bonding is essential during the assembly of aircraft components?
• What is one method for ensuring proper load distribution in an assembly?
• What parameter is primarily checked during weight and balance measurements?
• What tool is typically used to check proper wing twist in a sheet metal constructed wing?
• What method is generally acceptable for inspecting a stainless steel control cable?
• In what situation would you use a shim in assembly?
• What is the maximum angle at which fairleads should deflect the alignment of a cable?
• What does "plumb" mean in the context of rigging?
• What should be inspected regarding the threaded rod ends during a 100-hour airplane inspection?
• What must aircraft flight control trim systems allow the pilot to determine?
• The acute angle formed by the chord line of a wing and the relative wind is known as the?
• What document can be used to determine the primary flight control surface deflection for an imported aircraft after reassembly?
• In which condition should rigging adjustments be performed?
• What purpose do airframe jacks serve during assembly?
• Which of the following could lead to unexpected assembly failures?
• In rigging practices, what does the term "load testing" refer to?
• What is the main role of an optical alignment tool in assembly?
• If control cables are properly adjusted but control surfaces vibrate, what is the likely cause?
• What happens to the angle of incidence of an airplane at rest when it is in flight?
• What direction does the trim tab move when the cockpit control is moved towards the nosedown position?
• Why is it important to lubricate moving parts in assembly?
• What is the correct procedure for installing a cotter pin?
• What will happen to the left aileron if the control stick of a properly rigged aircraft is moved forward and to the right?
• If swaging tool manufacturer instructions are followed correctly, what should be the outcome regarding the terminal strength?
• What should be examined when inspecting control cable terminations?
• In rigging, what does the term "chord line" refer to?
• What does "static balance" mean in relation to control surfaces?
• If a single-rotor helicopter is in forward horizontal flight, the angle of attack of the advancing blade is?
• What might be a sign that a component is not sufficiently secured during assembly?
• Before performing maintenance on an aircraft, which of the following is a primary precaution?
• Which of the following is critical for ensuring the reliability of an assembly?
• Which control input affects the pitch of a helicopter?
• How often should maintenance logs be reviewed for aircraft rigging and assembly?
• When jacking an aircraft, what is the first action that should be taken?
• Which inspection process is critical for ensuring the safety of control cables in aircraft?
• When inspecting a control cable turnbuckle, what is a key aspect to verify?
• During the assembly process, what should be done with all safety pins?
• How do you determine whether a control surface has sufficient free play?
• What is the method to mitigate the effects of misalignment in assembly?
• Why is it important to check the weight limits of jacks before use?
• What phenomenon describes the shaking that occurs due to turbulent air around the aircraft?
• When used near magnetic compasses, cotter pins must be made from which material?
• When using a universal propeller protractor, how should it be calibrated?
• Why is it important to use appropriate installation techniques during assembly?
• Which statement is correct concerning the torque effect on helicopters?
• Why is documenting rigging changes essential during assembly?
• What is the primary purpose of a tension gauge in rigging?
• When should adjustments to rigging be thoroughly re-checked?
• The primary purpose of wing slats is to?
• Which physical factors are involved in the aspect ratio of airplane wings?
• What source provides specific instructions for conducting a symmetry alignment check on an aircraft?
• What is the function of the ailerons in an aircraft?
• Why is it essential to follow the manufacturer's guidelines during assembly?
• What is the primary purpose of the cyclic pitch control in a helicopter?
• The primary purpose of stall strips is to?
• Which tool is essential for measuring control surface deflection?
• What material is commonly used for aircraft rigging due to its strength-to-weight ratio?
• What does the angle of incidence refer to in aviation?
• What is the purpose of the rigging chart in assembly?
• Wing dihedral contributes most to stability of the airplane about which axis?
• If the vertical fin of a single-engine, propeller-driven airplane is rigged properly, it will generally be parallel to?
• Which tool is essential for properly rigging control surfaces on an aircraft?
• Movement of an airplane along its lateral axis (roll) is also known as movement around?
• Buffeting in an airplane is caused by?
• Which type of flap system is known for increasing both wing area and changing wing camber?
• How do you identify a worn control cable?
• What does "zeroing" refer to in the context of aircraft assembly?
• What is the purpose of the free-wheeling unit in a helicopter drive system?
• What indicates excessive wear on the sides of a control cable pulley groove?
• The primary function of the vertical fin in an aircraft is to provide what?
• What is a critical aspect of the assembly process to prevent potential aircraft malfunctions?
• Why is it important to maintain accurate rigging on an aircraft?
• What is the purpose of using jack stands under an aircraft?
• What is the purpose of a fuel strainer during assembly?
• What is the purpose of spring tabs or servo tabs in aircraft?
• Main rotor blades that do not cone by the same amount during rotation are said to be?
• How does temperature affect the rigging tension in cables?
• Which of the following is NOT a benefit of properly rigged control surfaces?
• In terms of aerodynamic efficiency, during turbulent flow, what occurs?
• What is the advantage of using stainless steel for control surface hinges?
• What component is used to change the direction of a control cable?
• What is the significance of torque specifications in assembly?
• Which kind of testing is performed to verify the correct rigging of control surfaces?
• What is a potential consequence of using improper materials in an assembly?
• As the angle of attack of an airfoil increases, what happens to the center of pressure?
• In which conditions is a self-locking nut most likely to fail?
• Why is it crucial to follow the manufacturer's specifications during assembly?
• A helicopter in forward flight, cruise configuration, changes direction by?
• What is one key benefit of using a tension gauge during assembly?
• The function of ailerons during flight is to primarily control?
• When conducting rigging inspections, which aspect is most critical to ensure safety?
• What is the primary advantage of using quick-release pins in assembly?
• When conducting rigging and alignment checks outdoors, the aircraft should be positioned?
• What component is crucial for securing the aircraft during rigging operations?
• If a fiber or nylon insert-type, self-locking nut can be easily threaded on with fingers, what should be done?
• Which safety practice is essential during assembly and rigging?
• The balance condition of a control surface is often determined by observing what aspect of the surface?
• Improper rigging of the elevator trim tab system will affect the balance of the airplane about its?
• Which part of an aircraft is primarily focused on during the assembly process?
• What should be done if a technician finds a discrepancy in the assembly alignment?
• The negative result of poor longitudinal stability in an airplane is?
• Where is fuselage station No. 137 positioned?
• What is the preferred action if a control cable pulley shows signs of excessive wear?
• Stability about the axis that runs parallel to the line of flight refers to which type of stability?
• The purpose in checking main rotor blade tracking is to determine the?
• What impact does the center of gravity have on an aircraft?
• How can you verify aileron rigging accuracy?
• In cold weather, what happens to the tension of a cable-operated control system that was initially tensioned in a heated hangar?
• What is the primary purpose of a tension regulator in a flight control cable system for an all-metal aircraft?
• What is an acceptable safety device for a castle nut when used on secondary structures?
• What types of tests can be performed to ensure proper assembly?
• An airplane that tends to gradually increase a pitching moment set into motion exhibits?
• Movement about the longitudinal axis (roll) in a helicopter is affected by which control?
• Which system is primarily affected by poor rigging practices?
• What is the typical function of a go-no-go gauge in aircraft maintenance?
• When the lift of an airfoil increases, what happens to the drag?
• Which safety measure should be implemented prior to jacking an aircraft?
• What does the term "control surface travel" refer to?
• What is the recommended method for securing loose components during assembly?
• An airplane which has good longitudinal stability should have a minimum tendency to?
• What is a common tool used for tightening nuts and bolts during assembly?
• How does lubrication impact the lifespan of aircraft components?
• The correct dihedral angle of wings can be determined by using?
• Why is the center of lift usually located aft of an airplane's center of gravity?
• What is crucial when terminating aircraft control cables with swaged terminals?
• What is a potential consequence of a poorly assembled control system?
• Why is it important to conduct a symmetry alignment check?
• What is the function of the trim tab on the ailerons?
• Why is it important to maintain a desired flight attitude with trim tabs?
• What Safety precaution is crucial during the assembly of aircraft components?
• What is one purpose of the freewheeling unit required between the engine and the helicopter transmission?