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
  • Forward driveshaft
  • Fan shaft assembly
  • Aft driveshaft
  • Driveshaft segments
  • Disc packs
  1. System Descriptions
  2. Tail Rotor Drive

Shafts

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Last updated 1 year ago

The shaft system transmits shaft power from the freewheel to the tail rotor gearbox and decreases the stress level in the shafts when the tailboom moves during flight. The system also pushes air through the oil cooler for the cooling of the engine and transmission oil.

The shaft system has the components that follow:

Forward driveshaft

The forward driveshaft is located under the engine, in the turbine section, and connects the freewheel to the fan shaft assembly. It is a steel alloy riveted assembly made of a shaft and two flange adapters.

Fan shaft assembly

The fan shaft assembly is located above the tailboom attachment to the aft fuselage. It connects the forward driveshaft to the aft driveshaft and pushes air into the plenum and through the oil cooler for the cooling of the engine and transmission oil. The fan shaft assembly includes the subassemblies that follow:

  • Shaft assembly and two flange adapters

  • Impeller and housing

  • Forward and aft bearing hangers

The shaft assembly is made of steel alloy and has a flange to attach the aluminum impeller. Two steel alloy flange adapters engage the splines on the end adapters of the shaft assembly and connect the forward and aft driveshafts. When the shaft assembly turns, it drives the impeller inside a housing which connects to the plenum. Cool air moves through the inlet of the housing and then flows to the oil cooler. The forward and aft hangers attach the shaft assembly to the truss assembly and have provisions for alignment of the bearing inside with the adjacent driveshaft. The bearings are permanently sealed units that have four 0.080 inch (2 mm) holes on each side of the seal for lubrication.

Aft driveshaft

The aft driveshaft is located above the tailboom and connects the fan shaft assembly to the driveshaft segments. It is an aluminum riveted assembly made of a shaft and two flange adapters.

Driveshaft segments

The driveshaft segments are located along the top of the tailboom. There are five driveshaft segments that connect the aft driveshaft to the tail rotor gearbox. The driveshaft segments are all the same. Thus, they are fully interchangeable units. Each driveshaft segment includes the subassemblies that follow:

  • Shaft assembly and two flange adapters

  • Bearing hanger

The shaft assembly is an aluminum riveted assembly made of a shaft and one flange adapter. The other flange adapter engages the splines on the opposite end of the shaft assembly and connects the adjacent driveshaft segment. The hanger attaches the driveshaft segment to the tailboom and has provisions for alignment of the bearing inside with the adjacent driveshaft segments. The bearing is a permanently sealed unit that has four 0.080 inch (2 mm) holes on each side of the seal for lubrication.

Disc packs

The disc packs, or Thomas couplings, are located along the tail rotor driveshafts. There are nine disc packs that connect the shafts and their segments together, to the freewheel and to the tail rotor gearbox. Together, the disc packs absorb the movement of the tailboom during flight to prevent concentration of stress in the shafts.

Each disc pack is made of 9 to 12 stainless steel discs stacked together. Each disc has two index flats parallel to the grain of the disc. These index flats are visual aids to make sure the discs are correctly installed.

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Forward driveshaft
Fan shaft assembly
Aft driveshaft
Driveshaft segments
Disc packs