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Exam (elaborations)

Assembly & Rigging C Questions and Answers 100% Solved

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Assembly & Rigging C Questions and Answers 100% Solved

Institution
Assembly And Rigging
Course
Assembly and Rigging









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Institution
Assembly and Rigging
Course
Assembly and Rigging

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Uploaded on
March 21, 2025
Number of pages
5
Written in
2024/2025
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Assembly & Rigging C Questions and Answers
100% Solved
In order to maintain a constant RPM, engine power must be changed every time the pitch of
the rotor blades changes. Two mechanisms used to accomplish these power changes are the
__________ and the __________. ✔️✔️Correlator, Governor


On most helicopters, throttle consists of a twist-grip mounted at the end of the __________
control. ✔️✔️Collective


The helicopter control that changes the pitch of the rotor blades at a certain point in their
rotation is called the __________ pitch control. ✔️✔️Cyclic


The fuselage of some helicopters is kept relatively level in flight at high airspeed by using a(n)
__________ controlled by the cyclic pitch control to increase by the down load on the tail as
the cyclic control is moved forward. ✔️✔️Synchronized Elevator


Boosted controls on a helicopter cannot feed vibration back through the controls if an
__________ control system is used. ✔️✔️Irreversible


The pitch of the tail rotor is controlled by __________ operated by the pilot. ✔️✔️Pedals


A tail rotor located within a circular duct is called a __________. ✔️✔️Fenestron


A helicopter is inherently __________. ✔️✔️Unstable


Three systems used to increase the stability of a helicopter are : ✔️✔️1. Stabilizer Bar
2. Offset Flapping Hinges

, 3. Stability Augmentation


Low frequency vibration is felt as a(n) __________. ✔️✔️Beat


Vibrations caused the main rotor system are usually of the __________ frequency type.
✔️✔️Low


An out-of-track rotor would normally cause a __________ vibration. ✔️✔️Vertical


An out-of-balance rotor would normally cause a __________ vibration. ✔️✔️Lateral


Helicopter blades must be balanced both: ✔️✔️1. Statically
2. Dynamically


Helicopter blades are balanced in what two directions? ✔️✔️1. Chordwise
2. Spanwise


Three methods of checking main rotor blade track are: ✔️✔️1. Marking stick or flag
2. Strobe light
3. Infrared light


Adjusting the length of the pitch change rods is normally done to correct an out-of-track
condition found __________. ✔️✔️On the ground


Bending the rotor blade trim tabs is normally done to correct an out-of-track condition found
__________. ✔️✔️In flight

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