Where does the breakage of control cable wires occur most frequently?

Breakage usually occurs where cables pass over pulleys and through fairleads.

Breakage usually occurs where cables pass through pulleys and over fairleads.

Breakage usually occurs where cables pass over pulleys and over fairleads.

Which statement concerning the 100-hour inspection of an airplane equipped with a push-pull tube-type control system is true?

The threaded rod ends should be checked for the amount of thread engagement by means of the inspection hole provided.

The threaded rod ends should be checked for the amount of thread engagement by means of the inspection patch provided.

The threaded rod ends should not be checked for the amount of thread engagement by means of the inspection hole provided.

During inspection of the flight control system of an airplane equipped with differential-type aileron control, side-to-side movement of the control stick will cause

each aileron to have a greater up travel (from the streamlined position) than down travel.

each aileron to have a greater up travel (from the streamlined position) than up travel.

each aileron to have a greater down travel (from the streamlined position) than down travel.

The braking action of a Cleveland disk brake is accomplished by compressing a rotating brake disk between two opposite brake linings. How is equal pressure on both sides of the rotating disk assured?

By allowing the caliper to float to automatically equalize as pressure is applied to the rotor.

By allowing the caliper to float to automatically equalize as pressure is applied to the propeller.

By allowing the float to caliper to automatically equalize as pressure is applied to the rotor.

The repair for an out-of-tolerance toe-in condition of main landing gear wheels determined not to be the result of bent or twisted components consists of

inserting, removing, or changing the location of washers or spacers at the center pivotal point of the scissor torque links.

shimming the axle in the oleo trunnion.

placing shims or spacers behind the bearing of the out-of-tolerance wheel or wheels.

On all aircraft equipped with retractable landing gear, some means must be provided to

extend the landing gear if the normal operating mechanism fails.

retract and extend the landing gear if the normal operating mechanism fails.

prevent the throttle from being reduced below a safe power setting while the landing gear is retracted.

Which statement is true with respect to an aircraft equipped with hydraulically operated multiple-disk type brake assemblies?

Do not set parking brake when brakes are hot.

Set parking brake when brakes are hot.

Do not set parking brake when brakes are cold.

How can it be determined that all air has been purged from a master cylinder brake system?

By noting whether the brake is firm or spongy.

By operating a hydraulic unit and watching the system pressure gauge for smooth, full-scale deflection.

By noting the amount of fluid return to the master cylinder upon brake release.

What function does the absolute pressure regulator perform in the pneumatic power system?

Regulates the compressor inlet air to provide a stabilized source of air for the compressor.

Regulates the compressor exhaust air to provide a stabilized source of air for the compressor.

Regulates the compressor inlet air to provide a stabilized source of fuel for the compressor.

What is the purpose of using backup rings with O-rings in hydraulic systems above 1,500 PSI?

Prevent high pressure from extruding the seal between the moving and stationary part.

Prevent low pressure from extruding the seal between the moving and stationary part.

Prevent high pressure from extruding the seal between the stationary part.

The purpose of the pressure regulator in a hydraulic system is to

maintain system operating pressure within a predetermined range and to unload the pump.

maintain system operating pressure within a determined range and to unload the pump.

maintain system operating pressure within a predetermined range and to load the pump.

The strength and stiffness of a properly constructed composite build up depends primarily on

The orientation of the plies to the load direction

A 60% matrix to 40% fiber ratio

The ability of the fibers to transfer stress to the matrix

Alloy 2117 rivets are heat treated

By the manufacturer and do not require heat treatment before being driven.

By the manufacturer and but require reheat treatment before being driven.

To a temperature of 910 to 930 degree fahrenheit and quenched in cold water

Repairs or splices involving stringers on the lower surface of stressed skin metal wings are usually

Permitted but are normally more critical in reference to strength in tension than similar repairs to the upper surface.

Permitted only if the damaged does not exced 6" in any direction

A typical barrier type aircraft terminal strip is made of

polyester resin and graphite compound

layered aluminum impregnated with compound

A.R_MAJOR EXAM.3

Authored by Chealsey Abraham

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Professional Development

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MULTIPLE CHOICE QUESTION

30 sec • 1 pt

If a single-rotor helicopter is in forward horizontal f light, the angle of attack of the advancing blade is

more than the retreating blade.

equal to the retreating blade.

less than the retreating blade.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the purpose of the free-wheeling unit in a helicopter drive system?

It disconnects the rotor whenever the engine stops or slows below the equivalent of rotor RPM.

It connects the rotor whenever the engine stops or slows below the equivalent of rotor RPM.

It disconnects the rotor whenever the engine go or slows below the equivalent of rotor RPM.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

If a pilot reports that an airplane flies left wing heavy, this condition may be corrected by

increasing the angle of incidence of the left wing, or decreasing the angle of incidence of the right wing, or both.

increasing the angle of incidence of the right wing, or decreasing the angle of incidence of the right wing, or both.

increasing the angle of incidence of the left wing, or increasing the angle of incidence of the right wing, or both.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The angle of incidence is that acute angle formed by

a line parallel to the wing chord and a line perpendicular to the longitudinal axis of the aircraft.

a line parallel to the wing chord and a line parallel to the longitudinal axis of the aircraft.

a line parallel to the wing chord and a line parallel to the lateral axis of the aircraft.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

If the right wing of a monoplane is improperly rigged to a greater angle of incidence than designated in the manufacturer’s specifications, it will cause the

airplane to be off balance both laterally and directionally.

airplane to be on balance both laterally and directionally.

airplane to be off balance or laterally and directionally.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The vast majority of aircraft control cables are terminated with swaged terminals, that must be

checked with a go-no-go gauge after, to show compliance with the manufacturer’s requirements after the swaging operation.

checked with a go-no-go gauge before and after, to show compliance with the manufacturer’s requirements before the swaging operation.

checked with a go-no-go gauge before and after, to show compliance with the manufacturer’s requirements after the swaging operation.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

When inspecting a control cable turnbuckle for proper installation, determine that

the safety wire ends are wrapped a maximum of four turns around the terminal end shanks.

the safety wire ends are wrapped a minimum of five turns around the terminal end shanks.

the safety wire ends are wrapped a minimum of four turns around the terminal end shanks.

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