Assembly & Rigging Flashcards
Movement about the longitudinal axis (roll) in a helicopter is effected by movement of the
Cyclic pitch control
If control cables are adjusted properly and the control surfaces tend to vibrate, the probable cause is
Worn attachment fittings
If the control stick of an aircraft with properly rigged flight controls is moved forward and to the right, the left aileron will move
Down and the elevator will move down.
A tension regulator in the flight control cable system of a large all-metal aircraft is used primarily to
Retain a set tension
Excessive wear on both of the sides of a control cable pulley groove is evidence of
Pulley misalignment
In rotorcraft external-loading, the ideal location of the cargo release is where the line of action passes
Through the center of gravity at all times.
An airplane which has good longitudinal stability should have a minimum tendency to
Pitch
Aircraft flight control trim systems must be designed and installed so that the
Pilot can determine the relative position of the trim tab from the cockpit.
The purpose in checking main rotor blade tracking is to determine the
Relative position of the blades during rotation.
The vertical flight of a helicopter is controlled by
Collective pitch changes
Which statement is correct concerning torque effect on helicopters?
Torque direction is the opposite of rotor blade rotation.
Where is the buttock line or buttline of an aircraft?
A width measurement, left or right of, and parallel to, the vertical center line.
When a fiber or nylon insert-type, self-locking nut can be threaded on a bolt or stud through the insert with only the fingers, it should be
Rejected
If the control stick of an aircraft with properly rigged flight controls is moved rearward and to the left, the right aileron will move
Down and the elevator will move up
if the vertical fin of a single-engine, propeller-driven airplane is rigged properly, it will generally be parallel to
The vertical axis but not the longitudinal axis
Which is an acceptable safety device for a castle nut when installed on secondary structures?
Cotter pin
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 elevators of a conventional airplane are used to provide rotation about the
Lateral axis
Main rotor blades that do not cone by the same amount during rotation are said to be out of
Track
Improper rigging of the elevator trim tab system will affect the balance of the airplane about its
Lateral axis
Other than the manufacturer maintenance manual what other document could be used to determine the primary flight control surface deflection for an imported aircraft that is reassembled after shipment?
Aircraft type certificate data sheet
When used in close proximity to magnetic compasses, cotter pins are made of what material?
Corrosion resisting steel
(Refer to Figure 8.) Identify the cable that is used in primary control systems and in other places where operation over pulleys is frequent
3
Rigging and alignment checks should not be undertaken in the open. However, if this cannot be avoided, the aircraft should be positioned with the
Nose into the wind