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
  • Mid fuselage belly skin
  • Left mid-belly access panel
  • Right mid-belly access panel
  • Mid-left mid-fuselage access panel
  • Baggage compartment floor
  • Control-tunnel access panel
  • Baggage compartment panel
  • Foam packings fuel compartment
  1. System Descriptions
  2. Airframe Systems
  3. Fuselage

Mid Fuselage

PreviousForward FuselageNextAft Fuselage

Last updated 1 year ago

The mid fuselage consists of the structural elements from the bulkhead behind the cabin to the bulkhead behind the baggage compartment, and from the bottom skin to the top of the baggage compartment. It houses the fuel storage, baggage compartment, and flight controls tunnel. It has the components that follow:

The mid fuselage is a composite and aluminum assembly. The flight controls tunnel, located at the front, houses the main rotor control tubes, its two side walls serve as principal load bearing elements, linking the forward end of the truss assembly with the two keel beams. The baggage compartment door is attached to it to make it a weather tight area for cargo and baggage. The fuel storage is located below the baggage compartment and also to the left of the flight controls tunnel. The fuel filler access door is attached to the left to protect the fuel filler port and the tank drain. It has the components that follow.

Mid fuselage belly skin

The Mid Fuselage Belly Skin is a carbon fiber composite panel which is permanently attached under the mid fuselage / fuel / baggage bay portion of the aircraft between the passenger cabin and aft body panels. It supports the fuel bag primarily, as well as provides aerodynamic shape, structural integrity and lightning strike protection for the fuel bag to the mid fuselage structure. It has three removable panels which provide access to the controls tunnel components and various systems routing on either side of the aircraft. This panel has special limitations to damage, paint thickness and the application of decals (each referred to as an organic coating). Structural performance and lightning strike protection may be affected if the limitations are not respected.

Left mid-belly access panel

The left mid-belly access panel is made of aluminum alloy. It protects and gives access to the mid fuselage internal components, and provides the aerodynamic shape and structural integrity of the fuselage. It is located on the bottom on the left side of the mid fuselage and is attached to the structure with screws.

Right mid-belly access panel

The right mid-belly access panel is made of aluminum alloy. It protects and gives access to the mid fuselage internal components, and provides the aerodynamic shape and structural integrity of the fuselage. It is located on the bottom on the right side in the middle of the mid fuselage and is attached to the structure with screws.

Mid-left mid-fuselage access panel

The mid-left mid-fuselage access panel is an assembly of an aluminum alloy skin reinforced with three stiffeners. It protects and gives access to the baggage compartment and the fuel tank, and provides the aerodynamic shape and structural integrity of the fuselage. It is located on the left side in the middle of the mid fuselage and is attached to the structure with screws.

Baggage compartment floor

The baggage compartment floor is a composite panel assembly. It is located on the bottom of the baggage compartment. It is attached to the structure with screws and gives access to the fuel tank. It has nine footman loops mounted on it that permit to secure the cargo and baggage during the flight.

Control-tunnel access panel

The control-tunnel access panel is made of aluminum alloy. It is located on the bottom in the middle forward end of the mid fuselage. It is attached to the structure with screws and gives access to the flight controls tunnel.

Baggage compartment panel

The baggage compartment panel is a composite panel assembly. It is located on the bottom of the baggage compartment at the right front end. It is attached to the structure with screws and gives access to the fuel tank. It has on footman loop mounted on it that permits to secure the cargo and baggage during the flight.

Foam packings fuel compartment

The foam packings fuel compartment are made of separate pieces of foam. They are located around the fuel tank, in the fuel cell compartment. They protect the fuel tank from unwanted movements during flight. They also hold the fuel tank in the best position to maximise the flow of fuel during operation.

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Mid fuselage belly skin
Left mid-belly access panel
Right mid-belly access panel
Mid-left mid-fuselage access panel
Baggage compartment floor
Control-tunnel access panel
Baggage compartment panel
Foam packings fuel compartment