BELL 505 Mechanic's Guide
  • Welcome!
  • 🚁System Descriptions
    • Introduction
    • Airframe Systems
      • Dimensions and Areas
      • Fuselage
        • Forward Fuselage
        • Mid Fuselage
        • Aft Fuselage
        • Roof
        • Tailboom
      • Stabilizers
      • Landing Gear
      • Equipment/Furnishings
      • Fire Protection (Fire Extinguishing)
      • Doors
      • Windows
      • Environmental Control
        • Distribution
        • Avionics Fans
        • Heating
      • Ice and rain protection (Air intakes)
    • Integrated Avionics Systems
      • Systems Integration and Display
      • Indicating/Recording Systems
        • Instruments and Control Panels
        • General Computers
        • Central Warning System
        • Central Display System
      • Communications
      • Navigation
        • Dependent Position Determining
    • Main Rotor
      • Main Rotor Hub and Blade Assembly
      • Rotating Controls
      • Main Rotor Indicating
    • Main Rotor Drive
      • Engine/Gearbox Couplings
      • Mast Assembly
      • Transmission Assembly
      • Transmission Oil
      • Mounts and Attachments
      • Main Rotor Drive Indicating
    • Tail Rotor
      • Tail Rotor Hub and Blade Assembly
      • Rotating Controls
    • Tail Rotor Drive
      • Shafts
      • Gearbox
      • Tail Rotor Drive Indicating
    • Flight Control Systems
      • Rotor Flight Controls
        • Dual Controls Kit
        • Collective Control System
        • Cyclic Control System
        • Anti-torque Control System
        • Servo-Control System
      • Hydraulic Power
    • Fuel
      • Storage
      • Distribution
      • Fuel Indicating
    • Power Plant Systems
      • Power Plant
      • Air
      • Exhaust
      • Oil
      • Engine Control
      • Ignition
    • Electrical Systems
      • Electrical Power
        • DC Generation
        • External Power
        • DC Electrical Load Distribution
        • Multipurpose Equipment
      • Lights
  • 🪛Line Maintenance
    • Overview of Line Maintenance
    • Servicing
      • Replenishing and Depleting
        • Filling the hydraulic system with fluid
        • Draining fluid from the hydraulic system
      • Lubrication
        • Lubricating the main rotor grips
        • Lubricating the trunnion bearings
        • Lubricating the pillow block assemblies
        • Lubricating the duplex bearing
        • Lubricating the needle bearings
        • Lubricating the pitch change mechanism
        • Lubricating the crew seat positioning mechanism
      • Clean and Surface Protection
        • Rotor blade - Erosion tape replacement
        • Flushing the hydraulic system
      • Inspection
        • 50 flight hours/1 year inspection
        • 100 flight hours inspection
        • 100 flight hours/6 months inspection
        • 100 flight hours/1 year inspection
        • 100 flight hours/18 months inspection
        • 150 flight hours inspection
        • 200 flight hours inspection
        • 300 flight hours inspection
    • Test and Checks
      • Power Assurance Check (PAC)
      • Checking the fluid level of the hydraulic system
      • Flame Out Protection System (FOPS) test
      • Testing the operation of the hydraulic system
      • Testing operation of audio integration system
      • Testing operation of speech communication
      • Testing operation of central warning systems
    • Fault Isolation
      • Crew Alerting System (CAS) Messages
        • WARNING Messages
          • BATTERY HOT
        • CAUTION Messages
        • ADVISORY Messages
        • STATUS Messages
      • System Failures
    • Removal/Installation
      • Electrical Power
        • Installing the ground power unit (GPU)
        • Removing the ground power unit (GPU)
      • Equipment/Furnishings
        • Removing the crew seats
        • Installing the crew seats
      • Hydraulic Power
        • Installing the hydraulic power unit
        • Removing the hydraulic power unit
        • Replacing the HRFM filter element
        • Restoring/replacing the hydraulic pressure filter element
        • Removing the hydraulic pump
        • Removing the pump adapter assembly
        • Installing the pump adapter assembly
        • Installing the hydraulic pump
      • Main Rotor
        • Removing the NR sensor
        • Installing the NR sensor
    • Standard Repairs
      • Main Driveshaft
      • Air Intake
  • 🔧Base Maintenance
    • Overview of Base Maintenance
    • Servicing
      • Adjust, align and calibrate
      • Inspection
    • Function Test
    • Fault Isolation
    • Removal/Installation
    • Major Repairs
  • 🧰Component Interim Maintenance
    • Overview of Component Interim Maintenance
    • Time Limits
    • Component Interim Inspections
  • ⚙️Component Restoration (Overhaul)
    • General Information
    • Main Rotor Hub Assembly
      • Dimensions and Areas
      • Maintenance Planning Information
      • Tools and Workaids
      • Disassembly
      • Cleaning and Paint Removal
      • Inspections
        • Conditional Inspection
        • Non-Destructive Inspections
      • Repair
      • Finishing
      • Assembly
    • Swashplate and Support Assembly
    • Mast Assembly
    • Transmission Assembly
    • Freewheel Assembly
    • Tail Rotor Hub Assembly
    • Tail Rotor Gearbox
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On this page
  • Collective jackshaft assembly
  • Collective stick and grip assembly
  • Cyclic stick and grip assembly
  • Left pedal assembly
  • Right pedal assembly
  1. System Descriptions
  2. Flight Control Systems
  3. Rotor Flight Controls

Dual Controls Kit

PreviousRotor Flight ControlsNextCollective Control System

Last updated 1 year ago

The dual controls kit provides the controls for the copilot. It consists of the components that follow:

  • , Includes the copilot throttle switch

  • , Includes the copilot ICS trigger switch

Collective jackshaft assembly

The collective jackshaft assembly consists of an aluminum tube and a collective stick support made of machined aluminum billet. They are assembled together with two bolts perpendicular to each other. The tube is also mounted on the pilot collective jackshaft with two bolts perpendicular to each other. It transmits the force from the copilot collective stick to the pilot collective jackshaft. The bolts are attached with washers and castellated nuts safetied with split pins. The surfaces of the tube mating with the collective stick support and the pilot collective jackshaft are machined to close tolerances to keep its deflection to a minimum when force is applied to the copilot collective stick and grip assembly.

Collective stick and grip assembly

The collective stick and grip assembly lets the operator control the collective pitch of the main rotor blades. The collective stick is made of aluminum tubing with a riveted aluminum collar. Two slots are cut in the bottom of the stick to engage a bolt in the collective stick support. A quick release pin is inserted in matching holes in the collar and the collective stick support to lock the collective stick in position. The grip assembly is made of plastic and has the copilot throttle switch. A harness for connecting the copilot throttle switch to the helicopter exits near the base of the stick. A plastic support is also installed near the base for the connector.

Cyclic stick and grip assembly

The cyclic stick and grip assembly lets the operator control the cyclic pitch of the main rotor blades. The cyclic stick is made of aluminum with a riveted stick end made from a machined aluminum billet. The stick end is inserted into the copilot cyclic base fitting assembly and is locked in place with a hand tightening screw. The grip assembly is made of plastic and has the copilot Intercomm System (ICS) trigger switch. A harness for connecting the ICS trigger switch to the helicopter exits the cyclic stick above the stick end. A doubler riveted above the stick end reinforces the cyclic stick at the harness exit hole.

Left pedal assembly

The left pedal assembly lets the operator control the pitch of the tail rotor blades, and the thrust the tail rotor produces. It consists of an upright tube with the adjustable pedal support, and of the left pedal with its quick release pin. It is made from aluminum with the quick release pin made from corrosion resisting steel. Two slots are cut in the bottom to engage a bolt in the directional pedal jackshaft assembly, and a riveted collar near to the bottom end of the upright tube lets lock the assembly in place.

Right pedal assembly

The right pedal assembly lets the operator control the pitch of the tail rotor blades, and the thrust the tail rotor produces. It consists of an upright tube with the adjustable pedal support, and of the right pedal with its quick release pin. It is made from aluminum with the quick release pin made from corrosion resisting steel. Two slots are cut in the bottom to engage a bolt in the directional pedal jackshaft assembly, and a riveted collar near to the bottom end of the upright tube lets lock the assembly in place.

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Collective jackshaft assembly
Collective stick and grip assembly
Cyclic stick and grip assembly
Left pedal assembly
Right pedal assembly