Aerodynamics 234P: Aircraft Control Cable Systems week 2/3 QA pages 31 - 80

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Questions and Answers

What is the device used to join cables and adjust the cable system tension?

Tension Regulator

When you turn the control wheel to the left and right, which components are you moving?

Ailerons.

What is the purpose of a pulley guard?

The pulley guard protects the cable from coming off the pulley when the cable is slack.

What type of device is used to convert the cable and chain movement in the linear movement acting on the push/pull rod connected to the elevator trim tab on the Cessna Elevator Trim System discussed in class?

<p>Screw jack assembly.</p> Signup and view all the answers

Explain the pictures bellow relating to cable wear and describe indicate what cases the various types of wear?

<p>Various types of cable wear include abrasion, corrosion, and fatigue, each caused by different factors like friction, environmental exposure, and repetitive stress. A) Good B) Excessive cable tension C) Pulley too large for cable D) Pulley misalignment E) Cable misalignment F) Frozen Bearing.</p> Signup and view all the answers

What are the names of the 3 elements or sections of any of the Flight Control Systems?

<p>Input (pilot provides commands), transmitting (takes input and transfer to control), and output (creates force to control surfaces).</p> Signup and view all the answers

Which type of Control Cable is most widely used for Primary Flight Control Systems?

<p>7x19 extra flexible is most widely used.</p> Signup and view all the answers

When you are inspecting a Pulley and you find that the pattern of the cable has been pressed into the groove of the pulley, what does this indicate?

<p>This indicates that the pulley is caused by excessive cable tension</p> Signup and view all the answers

When looking at the basic general aviation three cabled control system what is the name of the cable that runs from the right hand aileron bell-crank all the way over to the left hand aileron bell-crank?

<p>The balance cable.</p> Signup and view all the answers

What is the purpose of the small hole drilled in the body of the spherical rod end assembly in this diagram?

<p>This indicates that the small hole, referred to as a &quot;Witness Hole&quot;, is used as a visual indicator to confirm that there is sufficient thread engagement between the rod end and the push/pull rod. Once adjustments are complete, make certain of proper thread engagement by trying to pass lockwire through“Witness Hole”.</p> Signup and view all the answers

Where are the two places that you can find the control travel limits for an aircraft?

<p>Aircraft Type Certificate Data Sheet (TCDS) and the Aircraft Maintenance Manual (AMM).</p> Signup and view all the answers

When performing maintenance such as control system rigging, which documents must be in their most current and up to date status?

<p>The Aircraft Maintenance Manual (AMM) and all applicable Airworthiness Directives (ADs).</p> Signup and view all the answers

When you are checking the aileron control surface travel, what position should it be in to start the process?

<p>Neutral.</p> Signup and view all the answers

In accordance with the generic and the fixed and rotary wing aircraft type specific rigging instructions discussed in class, during the adjustment of the control system which tasks is carried out First.

<p>You must find and lock the primary surface in the neutral position.</p> Signup and view all the answers

In accordance with the generic and the fixed and rotary wing aircraft type specific rigging instructions discussed in class, what are the basic steps in their order provided in class?

<p>The basic steps include: Finding and locking the primary surface in the neutral position, adjust secondary surfaces to match the primary, perform cable tension checks and adjustments, complete travel checks (input devices are synchronized ).</p> Signup and view all the answers

According to the Generic Rigging Instructions if we have too much control surface travel in one direction and correct in the other direction during our surface travel check how is this rectified?

<p>Adjust the primary control stops: Once the neutral position of the control surface is confirmed to be correct, the primary control stops should be adjusted to symmetrically limit the travel in both directions according to the specifications found in the Aircraft Maintenance Manual (AMM) or the Type Certificate Data Sheet (TCDS). If the travel is excessive in one direction, the corresponding primary stop needs to be adjusted to limit the movement at the required point. In essence, you need to ensure the control surface starts at the correct neutral position and then adjust the physical limitations of its movement (the primary control stops) to achieve the required and symmetrical travel range.</p> Signup and view all the answers

During the rigging of the transmitting system, what are the devices used to ensure that the components of the transmitting and input system remain in the neutral position during the rigging process?

<p>Rigging tools and locking pins.</p> Signup and view all the answers

When do the regulations require a dual/independence inspection carried out and by whom?

<p>A dual or independent inspection must be carried out by an authorized individual and certified prior to signing a maintenance release.</p> Signup and view all the answers

How do you certify the rigging of a flight control system in Canada?

<p>By signing the maintenance release. Canadian Aviation Regulations (CAR) 605.85.</p> Signup and view all the answers

What does the term "Fit" mean when describing the dual inspection?

<p>&quot;Fit&quot; would verify that cables are tensioned and that primary stops are being struck while secondary stops are clear from contact.</p> Signup and view all the answers

What does the term "Safety” mean when describing the dual inspection?

<p>All locking devices have been installed correctly and are secure</p> Signup and view all the answers

What does the term “Sense of Motion” mean when describing the dual inspection?

<p>Sense of motion refers to the correct direction of movement of the associated control surface when the cockpit control is actuated.</p> Signup and view all the answers

When you check for “Wash Out” during the Symmetry Check, what are you inspecting?

<p>You are inspecting the wing twist. Wash out (decreasing AOA from root to tip) Wash In (Increasing AOA from root to tip).</p> Signup and view all the answers

When you check for “Wing Dihedral” during the Symmetry Check, what are you inspecting?

<p>You're inspecting the difference in height between the wing tips.</p> Signup and view all the answers

When you check for “Boxing Check” during the Symmetry Check, what are you inspecting?

<p>you are inspecting to see if the fuselage has twisted</p> Signup and view all the answers

What is the name and purpose of this helicopter control device?

<p>Tail rotor pedals control the heading (yaw) of the aircraft by changing the pitch on the tail rotor blades</p> Signup and view all the answers

What is the name of this inverted triangular shaped device circle at the bottom of this picture?

<p>Mixing Unit</p> Signup and view all the answers

What is the name of these units?

<p>Cyclic Full Left/Full Right</p> Signup and view all the answers

Which helicopter control will increase and decrease the lift equally throughout the rotation of the blades to increase or decrease lift & thrust?

<p>Collective control.</p> Signup and view all the answers

Which helicopter control will increase and decrease the lift differently throughout the rotation of the blades to tilt the rotor disk for directional control?

<p>Cyclic control.</p> Signup and view all the answers

What is the name of the helicopter flight control used to compensate for the force created by the engine driving the main rotor system?

<p>The anti-torque systems control by pedals from pilots.</p> Signup and view all the answers

What is the name of the device that transmits linear movements from the Cyclic & Collective Pitch controls to the rotating mast and rotor head

<p>The swashplate.</p> Signup and view all the answers

When pulling up on the collective pitch control, what is the equal and opposite reaction to the force of the engine?

<p>The helicopter's torque.</p> Signup and view all the answers

Engine power control is attached to or is a part of which flight control system on the helicopter?

<p>The collective control.</p> Signup and view all the answers

What is the purpose of the “Sprag Clutch Assembly” Or “Free Wheeling Unit" on a Helicopter?

<p>It allows the rotor to continue turning in the event of an engine failure.</p> Signup and view all the answers

According to the instructions for Autorotation Test Flights, what pieces of information are required to be recorded during the Autorotation Decent?

<p>The altimeter reading (pressure altitude), Oat reading (temperature of the air at that altitude), Nr tachometer reading (main motor RPM)</p> Signup and view all the answers

During the Autorotation Speed Calculation, what are the three parameters that you require to determine if the rotor RPM is correct based upon the Autorotation Chart?

<p>Gross weight, pressure altitude, and outside air temperature. Density altitude is found by combining the “pressure altitude” which is your altimeter reading with the “oat” reading which is your air temperature.</p> Signup and view all the answers

After completing the calculations using the information gathered and the autorotation chart, what would be the action required if the rotor speed was too high or what would be required if it were too low?

<p>If the rotor speed is too high, raise the collective slightly to decrease rotor RPM. If the rotor speed is too low, lower the collective to increase rotor RPM.</p> Signup and view all the answers

What is the name and purpose of this helicopter control device? The [blank] is used to control the helicopter's pitch and roll.

<p>cyclic</p> Signup and view all the answers

What is the name and purpose of this helicopter control device? The device is called the [blank] and its purpose is to control the helicopter's altitude.

<p>collective pitch control</p> Signup and view all the answers

What is the name and purpose of this helicopter control device? The device is called a [blank].

<p>Swashplate</p> Signup and view all the answers

Flashcards

Cable Pattern pressed into pulley groove

Cable must be replaced.

Cable connecting Aileron Bell-cranks

Drag cable (runs from right to left aileron bellcrank).

Small hole in spherical rod end assembly

To allow moisture to drain and prevent corrosion.

Finding control travel limits.

Aircraft maintenance manual (AMM) and type certificate data sheet (TCDS).

Signup and view all the flashcards

Documents for control system rigging

AMM, service bulletins, and any applicable AD's.

Signup and view all the flashcards

Aileron Surface Position

Neutral position.

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Study Notes

Control Cable System Fundamentals

  • A turnbuckle joins cables and adjusts cable system tension.
  • Turning the control wheel left and right moves the ailerons.
  • A pulley guard prevents the cable from slipping off the pulley.
  • A sector converts the cable and chain movement into linear movement on the Cessna Elevator Trim System's push/pull rod.

Cable Wear

  • Picture a shows normal wear.
  • Picture b shows corrosion.
  • Picture c shows fraying.
  • Picture d shows wear caused by improper cable tension.
  • Picture e shows kinked cable wear.

Flight Control Systems

  • The three elements or sections of flight control systems are:
    • Input
    • Transmitting
    • Output

Control Cables

  • 7x19 control cable is most widely used for primary flight control systems.
  • A cable pattern pressed into the pulley groove indicates the pulley is worn or the cable tension is incorrect.
  • The cable that runs from the right-hand aileron bell-crank to the left-hand aileron bell-crank in a basic general aviation three-cabled control system is the "cable".
  • The small hole drilled in the body of a spherical rod end assembly is for lubrication (or visual indication of proper thread engagement).

Flight Control System Rigging

  • Control travel limits can be found in:
    • The aircraft's Type Certificate Data Sheet (TCDS)
    • The Aircraft Maintenance Manual (AMM)
  • Up-to-date documents for control system rigging maintenance include:
    • Aircraft Maintenance Manual (AMM)
    • Service Bulletins (SB)
    • Airworthiness Directives (AD)
  • Aileron control surface travel should be checked with the control surface in the neutral position

Control System Adjustment

  • During control system adjustment, tasks carried out includes setting cable tension first.
  • Basic rigging steps in order are:
    • Securing the aircraft
    • Leveling the aircraft
    • Setting control surface neutral
    • Adjusting cable tension
    • Checking travel

Rigging Instructions

  • Too much control surface travel in one direction and correct travel in the other during a surface travel check is rectified by adjusting the appropriate control stops or turnbuckles.
  • Devices used to ensure components remain in neutral during transmitting system rigging include:
    • Control surface locks
    • Alignment jigs
    • Measuring devices

Dual/Independence Inspections

  • Regulations require a dual/independence inspection after major flight control system maintenance or alterations, and it is performed by two qualified individuals.

Flight Control System Certification in Canada

  • Rigging a flight control system in Canada is certified by a licensed Aircraft Maintenance Engineer (AME).

Dual Inspection Definitions

  • Fit: Indicates the proper engagement and alignment of components.
  • Safety: Indicates the reliability and security of the flight control system.
  • Sense of Motion: How the controls respond to input.
  • Range of Motion: Indicates the full and unobstructed movement of the control surfaces throughout their specified range.

Aircraft Symmetry Checks

  • "Wash Out" inspection during a symmetry check examines the wing twist.
  • "Wing Dihedral" inspection during a symmetry check examines the upward angle of the wings.
  • "Boxing Check" during the symmetry check verifies the alignment of the primary flight control surfaces.

Helicopter Flight Controls and Components

  • Device in picture 27 is a pitch link which adjusts blade pitch.
  • Device in picture 28 is a swashplate which translates the pilot's control inputs to the rotor blades.
  • Device in picture 29 is a collective pitch control, which controls the pitch angle of all rotor blades simultaneously.
  • The function of device in picture 30 could not be determined.

Helicopter Components

  • The inverted triangular shaped device in picture 31 is the collective pitch horn.
  • The units in picture 32 are hydraulic servos.
  • Collective control increases/decreases lift equally throughout blade rotation to raise/lower the helicopter.
  • Cyclic control increases/decreases lift unevenly to tilt the rotor disk for directional control.

Helicopter Flight Control

  • The flight control compensating for engine torque is the tail rotor.
  • The device transmitting linear movements from the cyclic and collective pitch controls to the rotating mast and rotor head is the swashplate.

Collective Pitch

  • The equal and opposite reaction to the force of the engine when pulling up on the collective is the downward force on the tail rotor.
  • Engine power control is attached to or part of the collective pitch control system on the helicopter.
  • A sprag clutch/freewheeling unit allows the rotor to continue turning even if the engine fails.

Autorotation Chart Application (Week 5 - M)

  • Information to be recorded during autorotation descent includes:
    • Altitude
    • Airspeed
    • Rotor RPM
  • Parameters required to determine if rotor RPM is correct based on an autorotation chart are:
    • Gross weight
    • Pressure altitude
    • Outside air temperature
  • If the rotor speed is too high, increase collective pitch; if too low, decrease collective pitch.

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