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
  • Grease lubrication practices
  • Special lubrication practices
  1. Line Maintenance
  2. Servicing

Lubrication

Instructions for the lubrication a system, equipment, component, or item.

Grease lubrication practices

DO NOT PURGE LUBRICATE THE HANGER BEARINGS OR THEY WILL BE OVER- GREASED. IF THIS OCCURS, THE BEARINGS WILL RUN HOTTER AND FOR A LONGER PERIOD OF TIME AND THESE CONDITIONS CAN CAUSE DAMAGE TO THE BEARING COMPONENTS.

DO NOT USE A HIGH CAPACITY/HIGH VELOCITY GREASE GUN TO GREASE LUBRICATE THE COMPONENTS. THE USE OF THIS EQUIPMENT CAN CAUSE DAMAGE TO THE COMPONENTS.

The following practices do not apply to the hanger bearings.

Obey the following grease lubrication practices:

  1. Before and after a grease lubrication, visually examine the grease fittings to make sure that the spring loaded steel ball is visible. If the steel ball is not visible, does not go back to the closed position, the grease fitting shows excessive leakage, or it is difficult to apply grease during the lubrication, replace the grease fitting (BHT-ALL-SPM, Chapter 8).

  2. If the grease fitting is replaced because the spring loaded steel ball was not visible, put a small steel probe into the back of the grease fitting and make sure that the steel ball is there. If the steel ball is not there, examine to make sure that the steel ball has not moved into the component and caused damage. Discard the grease fittings that have been removed.

  3. Protect the grease lubricants from excessive temperature and humidity, and from contamination. See the posted shelf life, if applicable.

  4. Before you use a supply of grease, whether in its original container or in dispensing equipment, make sure that no oil separation has occurred.

  5. If oil separation occurred without loss (leakage) of oil, thoroughly remix the oil component with the thickening agent to restore the original load bearing capabilities. Use only clean tools for mixing.

  6. Discard any grease supply that has lost some of its oil component after separation, whether in its original container or in grease dispensing equipment. Oil-depleted lubricants can be dangerous to the bearings.

  7. Intermixing brands of grease within the same specification is not permitted. If you need to change the grease brand, purge to remove the old grease until there is only new grease visible, unless specified differently.

DO NOT USE HIGH PRESSURE WATER, STEAM, OR SOLVENT WASH WHEN YOU CLEAN THE ROTATING CONTROL BEARINGS. HIGH PRESSURE WILL FORCE WATER, SOLVENT, AND SOMETIMES FOREIGN PARTICLES INTO THE BEARING CAVITY.

Purge lubrication of a bearing means that new grease is injected in the bearing to remove the old grease.

Special lubrication practices

Obey the following special lubrication requirements:

  • After each day of operation in rain or after washing the main rotor hub, purge lubricate all the exposed control bearings to remove trapped moisture and to make sure that a lube film is applied to the applicable surface.

  • Before each flight, when the helicopter has been exposed to high ambient temperatures, purge lubricate the main rotor grips and the pillow blocks/trunnion to make sure that any grease that was separated will be replaced with fresh grease. This practice will prevent premature brinelling of the main rotor yoke bearing journals.

  • If the helicopter is parked outside in a heavy dew environment, purge lubricate all the exposed control bearings every 7 days. This practice will reduce the risk of moisture being trapped in voids.

  • If the helicopter has been, or will be, parked or stored for more than 45 days without operation or service, purge lubricate all the bearings. Same applies to spare components on the shelf.

  • After each wash, all the bearings exposed to the wash should be lubricated.

Last updated 8 months ago

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