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
Powered by GitBook
On this page
  • Preliminary requirements
  • Required Conditions
  • Consumables, materials and expendables
  • Safety conditions
  • Procedure
  • Do a detailed inspection of the tail damper assembly as follows:
  • Do a general visual inspection of the hydraulic pressure line (from filter) as follows:
  • Do a general visual inspection of the hydraulic suction tube as follows:
  • Do a detailed inspection of the crew doors as follows:
  • Do a detailed inspection of the clamshell door as follows:
  • Do a detailed inspection of the pivot sleeve assembly as follows:
  • Do a detailed inspection of the support assembly as follows:
  • Requirements after job completion
  • Required Conditions
  1. Line Maintenance
  2. Servicing
  3. Inspection

300 flight hours inspection

Preliminary requirements

Required Conditions

Action/Condition
Procedure/Data

Remove the right transmission fairing (432BR).

Remove the upper-right mid-fuselage access-panel (433BR).

Remove the left transmission fairing (432AL)

Remove the upper-left mid-fuselage access-panel (433AL).

Consumables, materials and expendables

Name
Identification/References
Quantity

Drycleaning solvent

C-304

AR

Cleaning compound

C-318

AR

Lockwire

C-447

AR

Clean cloth

C-516

AR

Safety conditions

MAKE SURE YOU OBEY ALL OF THE SAFETY PRECAUTIONS WHEN YOU USE SOLVENTS. FAILURE TO DO SO MAY RESULT IN INJURY TO PERSONS AND/OR DAMAGE TO COMPONENTS.

DO NOT ALLOW SOLVENT TO MAKE CONTACT WITH PARTS MADE OF ELASTOMERIC MATERIAL OR DAMAGE WILL OCCUR.

Procedure

Do a detailed inspection of the tail damper assembly as follows:

The tail damper isolator springs are constructed from wire rope.

  1. Examine the isolator springs for evidence of broken strands and corrosion and for birdcaging or separation of the wound wires.

  2. Examine the clips for condition and security. Both ends of wires must be visible in the window.

  3. Examine the stiffener for condition and security.

  4. Examine the cotter pins, nuts, washers, and bolts that attach the stiffener and the isolator springs for condition and security.

  5. Examine the weights for condition and security.

  6. Examine the cotter pins, nuts, washers, and bolts that attach the weights to the isolator springs for condition and security.

Do a general visual inspection of the hydraulic pressure line (from filter) as follows:

  1. Visually examine the hydraulic pressure line (from filter) for mechanical damage and corrosion.

  2. Visually examine the fins of the hydraulic pressure line (from filter) for blockage.

  3. If there is a blockage, remove the cause.

  4. If there is damage to the hydraulic pressure line (from filter), replace the tube.

Do a general visual inspection of the hydraulic suction tube as follows:

  1. Visually examine the hydraulic suction tube for mechanical damage and corrosion.

  2. Visually examine the fins of the hydraulic suction tube for blockage.

  3. If there is a blockage, remove the cause.

  4. If there is damage to the hydraulic suction tube, replace the tube.

Do a detailed inspection of the crew doors as follows:

  1. Clean the eyebolts, latch bolts, and handle with Clean cloth moistened with Drycleaning solvent.

  2. Examine the crew doors for cracks, mechanical damage, and corrosion.

  3. Examine the eyebolts for cracks, mechanical damage, and corrosion.

  4. Shake the eyebolts and make sure that they are not worn too much.

  5. Examine the latch bolts of the crew doors for cracks, mechanical damage, corrosion, and ensure the latch bolts retract 0.080 inside the housing at ambient room temperature.

  6. Shake the latch bolts and make sure that they are not worn too much.

  7. Examine the handles of the crew doors for cracks, mechanical damage, corrosion, and correct operation.

  8. Shake the handle and make sure that it is not worn too much.

  9. If there is damage to the crew doors, wear on the eyebolts, wear on the latch bolts, and/or wear on the handles, contact customer support and services for permitted damage.

Do a detailed inspection of the clamshell door as follows:

  1. Clean the latch knobs, and hinges with Clean cloth moistened with Drycleaning solvent.

  2. Examine the clamshell door for cracks, mechanical damage, and corrosion.

  3. Examine the hinges for cracks, mechanical damage, and corrosion.

  4. Examine the latch knobs of the clamshell door for correct adjustment, and correct operation.

  5. Shake the latch knobs and make sure that they are not worn too much.

  6. If there is damage to the clamshell door, hinges, and/or wear on the latch knobs, contact customer support and services for permitted damage.

Do a detailed inspection of the pivot sleeve assembly as follows:

  1. Lift up the boot from the outer cap assembly as follows:

    1. Cut and remove the lockwire from the bottom of the boot.

    2. Remove the boot from the outer cap.

  2. Move the cyclic stick and grip assembly fully forward.

  3. Examine the pivot sleeve assembly for wear, mechanical damage, and corrosion. Look carefully at the ball area.

  4. Examine the two slots on top of the pivot sleeve assembly for wear and deterioration.

  5. Move the cyclic stick and grip assembly fully aft.

  6. Examine the pivot sleeve assembly for wear, mechanical damage, and corrosion. Look carefully at the ball area.

  7. Examine the two slots on top of the pivot sleeve assembly for wear and deterioration.

  8. Move the cyclic stick and grip assembly fully left.

  9. Examine the pivot sleeve assembly for wear, mechanical damage, and corrosion. Look carefully at the ball area.

  10. Examine the two slots on top of the pivot sleeve assembly for wear and deterioration.

  11. Move the cyclic stick and grip assembly fully right.

  12. Examine the pivot sleeve assembly for wear, mechanical damage, and corrosion. Look carefully at the ball area.

  13. Examine the two slots on top of the pivot sleeve assembly for wear and deterioration.

  14. While another person moves the collective stick and grip assembly slowly, examine the sleeve bearings between the pivot sleeve assembly and the support assembly for radial play and smooth operation.

  15. While another person moves the collective stick and grip assembly slowly, examine the bushings for wear.

  16. If there is damage to the pivot sleeve assembly, wear on the bushings, and/or play on the sleeve bearings, refer to component maintenance for permitted damage.

  17. Make sure that the pivot sleeve assembly is correctly installed.

Do not let the solvent touch the boot or damage to the boot can occur.

  1. Install the boot on the outer cap assembly as follows:

    1. Visually examine the outer cap assembly for unwanted material.

    2. If necessary, clean the top of the outer cap assembly with a Clean cloth moist with Drycleaning solvent.

    3. If there is oil or grease on the boot, clean it as follows:

      1. Clean the boot with Cleaning compound.

      2. Flush with water, then dry the boot with a Clean cloth.

    4. Put the bottom of the boot in position around the outer diameter of the outer cap assembly.

    5. Safety the bottom of the boot with Lockwire.

Do a detailed inspection of the support assembly as follows:

  1. Clean the support assembly with a Clean cloth moistened with Drycleaning solvent.

  2. Examine the support assembly for mechanical damage and corrosion.

  3. Shake the idler assembly and make sure that the bushings are not worn too much.

  4. If there is damage to the support assembly and/or wear on the bushings, refer to component maintenance for permitted damage.

  5. Make sure that the support assembly is correctly installed.

Requirements after job completion

Required Conditions

Action/Condition
Procedure/Data

Install the upper-left mid-fuselage access-panel (433AL).

Install the left transmission fairing (432AL)

Install the upper-right mid-fuselage access-panel (433BR).

Install the right transmission fairing (432BR).

Last updated 7 months ago

🪛