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
  • Preliminary requirements
  • Consumables, materials and expendables
  • Safety conditions
  • Main Procedures
  • Replace procedures
  • Cleanup of allowable damage
  • Standard Repairs
  1. Component Restoration (Overhaul)
  2. Main Rotor Hub Assembly

Repair

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Last updated 2 years ago

This section gives the procedures and data necessary to repair the main rotor hub assembly as follows:

  • All packings and seals

  • Unserviceable hardware

  • Curled or damaged shims

  • Worn or damaged parts

  • Mechanical and corrosion damage

  • Refinish surfaces as required

Standard Repairs

  • Yoke Grips and bearings

  • Trunnion, pillow blocks, and bearings

  • Strap pin

  • Blade bolts

Preliminary requirements

Consumables, materials and expendables

Safety conditions

Main Procedures

Replace procedures

Refer to the 505-CMM for the items that must be replaced, or items which cannot be repaired.

Self-locking nuts are unserviceable when tare torque is not present.

  1. Replace all packings, seals, washers, unserviceable self-locking nuts, and attaching hardware.

  2. Replace shims that have curled or damaged laminations.

  3. Replace cracked, broken, or distorted parts, or parts that have damaged threads.

  4. Replace parts that exceed allowable wear or damage limits.

  5. Replace blade bolt cap if damaged.

  6. Replace trunnion if cracked or if mechanical and corrosion damage limits are exceeded.

    • Visually inspect bushings, thrust washers, and adjusting screws for damage that would render parts unserviceable.

    • Replace trunnion bearing inner race if spalled, brinelled, or discolored due to overheating. Replace inner race and trunnion if damaged due to race turning on spindle of trunnion.

    • Replace bearings if spalled or discolored due to overheating, roller is broken, or operation is rough.

  7. Replace latch nut or blade bolt nuts if cracked, damaged, or corroded.

  8. Replace pillow block if cracked or if damaged beyond limits.

Refer to the manufacturer instructions for the mixing ratio, pot life, and curing time of the adhesive.

  1. Replace pillow block pads as follows:

    1. Lightly abrade bonding surfaces on the pillow block with a 400 grit Abrasive cloth or paper. Clean with MEK and dry with a clean lint free cloth.

    2. Abrade the light brown side of new pillow bloc pads with a 100 or 150 grit Abrasive cloth or paper. Clean with aliphatic naphtha and let the pads air dry.

    3. Apply a 0.003 to 0.008 inch (0.08 to 0.20 mm) thick layer of Adhesive to the bonding surfaces of the pillow block or pillow block pads, as applicable.

    4. Locate the pillow block pads on the inboard and outboard sides of the pillow block, respectively, and within 0.030 inch (0.76 mm) of the hole center.

    5. Bond the pillow block pads to the pillow block and remove excess adhesive before complete cure.

    6. Refinish the pillow block in accordance with DMC-505-A-62-20-01-00A-257A-B, as required.

  2. Replace grip bearings if any of the following conditions is found:

    • Broken or rough rollers.

    • Spalling, scoring, flaking, brinelling, or discoloration.

    • Pits larger than 0.008 inch (0.20 mm).

    • Cluster of three pits or more within an area of 0.25 inch (6.3 mm) diameter with any one pit larger than 0.004 inch (0.10 mm).

  3. Replace any part with defects for which no damage limits are specified.

Cleanup of allowable damage

This section gives information on the repair of negligible and/or allowable mechanical and corrosion damage to main rotor hub parts and the description of the surface treatment after their repair:

Repair allowable mechanical and corrosion damage to the main rotor hub parts (Limits charts)

  • Trunnion and pillow blocks

  • strap fittings, strap pins, and radius ring

  • strap bolts and latches

  • blade bolts and plug

  • excluder retainers

  • pitch horns

  • static stops

  • mast nut and cone set

Repair steel parts as follows

  1. Polish out acceptable damage using fine India stone.

  2. Apply brush-on cadmium plating solution to all previously plated and repaired steel surfaces (BHT-ALL-SPM, Chapter 3, Standard Practices Manual). Do not cadmium plate threaded areas.

Repair aluminum parts as follows:

  1. Polish out acceptable damage using a 400 to 600 grit silicon carbide abrasive cloth or paper.

  2. Apply chemical chromate conversion material to all repaired and bare aluminum surfaces (BHT-ALL-SPM, Chapter 3, Standard Practices Manual).

Dress out minor damage to blade bolt nuts and latch nuts.

Standard Repairs

This section gives the procedures and data necessary to repair damage and also gives the permitted damage for the following parts:

  • Yoke

  • Grips

  • Trunnion

  • Pillow blocks

  • Strap pin

  • Blade bolts

Yoke

Repair yoke as follows:

  1. After primer has cured, examine the yoke pillow block bores with inside micrometer for minimum I.D. of 2.6242 inches (66.655 mm). Sand as required without penetrating primer to get set dimension.

Polish out minor scratches and damage on noncritical areas with

Longitudinal scratches on spindle, not more than 0.002 inch (0.050 mm) deep, do not need to be completely removed. Surface burrs must be removed with a . Clean up minor damage to threads.

Pillow block bore damage must be removed by sanding in a circular motion with a 400 grit . Final polish surface until scratch free with a fine . Make sure that all nicks, scratches, and tool marks are removed.

Damage to bearing and spacer journals and mating fillet radii must be removed by sanding with a 400 grit and .

Damage to other surfaces must be removed by sanding with a 400 grit and . Make sure that all nicks, scratches, tool marks, and corrosion pitting are removed. Touch up surfaces where plating has been damaged or where repairs were done. Apply where required.

Mask the areas of yoke (12, ) that do not require primer or paint ().

Apply ) to yoke (12, ) as required.

Within 8 hours of primer application, apply two coats of light gull gray ), color code 36440 per FED-STD-595, to yoke (12) center section ().

⚙️
Crocus cloth
Crocus cloth
Abrasive cloth or paper
Abrasive pad
Abrasive cloth or paper
Abrasive pad
Abrasive cloth or paper
Abrasive pad
Cadmium plating solution
Figure 1
Figure 18
Epoxy polyamide primer (
C-204
Figure 1
Polyurethane coating (
C-245
Figure 17
Replace procedures
Cleanup of allowable damage

Epoxy polyamide primer

Polyurethane coating

Aliphatic naphtha

MEK

Adhesive

Adhesive

Abrasive pad

Abrasive cloth or paper

India stone

Crocus cloth

Clean cloth

Cover

Solid film lubricant (Heat Cured)

Use ThixO SYN or ThixO #2 as alternate

Cover

Solid film lubricant (Air Cured)

Cover

Chemical film material for aluminum

Cover

Corrosion preventive compound (Soft Film)

Cover

Cadmium plating solution (Brush-on)

Cover

Epoxy primer

Base P/N: 515X330Activator P/N: 910J717