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Axles

Sr. No. Application Area Fastener Types Primary Functions Materials Commonly Used Key Performance & Regulatory Factors
1 Fuselage Assembly Bolts, Screws, Rivets
  • Secure fuselage skins and frames
  • Maintain structural integrity under stress
 Aircraft-grade aluminum, titanium, or high-strength steel
  • Must endure cabin pressurization cycles
  • Subject to FAA/EASA regulations
2 Wing Structures Hi-Lok Bolts, Advanced Rivets
  • Attach wing skins to ribs, spars, and stringers
  • Resist loosening under vibration
 Titanium alloys, high-strength steel
  • High corrosion resistance
  • Lightweight for fuel efficiency
3 Engine Assemblies Aerospace Bolts, Locking Nuts, Studs
  • Secure turbine and compressor components
  • Withstand high heat and pressure
 Nickel superalloys, titanium, stainless steel
  • High tensile and shear strength
  • Regular inspection due to stress
4 Landing Gear Shear Bolts, Locking Pins, Bushings
  • Absorb heavy impact loads
  • Secure wheel, brake, and steering systems
 Heat-treated steel, titanium
  • Designed for high-load cycles
  • Frequent maintenance checks
5 Control Surfaces Clevis Pins, Special Bolts, Nuts
  • Connect ailerons, rudders, elevators
  • Transfer pilot commands accurately
 Aluminum alloys, specialty steels
  • Must resist vibration-induced loosening
  • Requires strict balancing for stability
6 Interior Cabin Screws, Captive Fasteners, Quick-Release Fasteners
  • Secure passenger seats, overhead bins, and paneling
  • Allow rapid installation/removal for reconfigurations
 Lightweight alloys, polymers, composites
  • Must meet flammability and safety standards (e.g., FAR 25.853)
  • Designed for ergonomic installation/maintenance
  • Must pass static and dynamic load tests
7 Avionics & Electronic Systems Small Screws, Lock Nuts, Inserts
  • Secure circuit boards, navigation units, and flight instruments
  • Mitigate loosening from constant vibration
 Stainless steel, aluminum
  • Often feature EMI/RFI shielding
  • Need secure locking to avoid electrical faults
  • Regulated by RTCA/DO-160 environmental testing requirements
8 Fuel Systems & Tanks Sealing Rivets, Self-Sealing Screws, O-Ring Bolts
  • Prevent fuel leakage under pressure
  • Maintain structural and chemical integrity of fuel compartments
 Corrosion-resistant alloys, specialized sealants
  • Must be fuel-resistant
  • Critical to preventing contamination and fuel loss
  • Regular safety checks to ensure seal integrity
9 Helicopter Rotor Assemblies High-Strength Bolts, Pins
  • Secure rotor blades to hub assemblies
  • Transfer torque and lift forces
 High-tensile steels, titanium
  • Subject to continuous rotational stress
  • Balanced torque application essential for rotor equilibrium
  • Fail-safe designs to prevent catastrophic failures
10 Cabin Flooring & Cargo Floor Bolts, Quick-Release Pins, Tie-Down Rings
  • Secure floor panels and cargo rails
  • Offer quick reconfiguration for cargo loading
 Aluminum or steel with protective coatings
  • Must handle dynamic loads during takeoff, landing, and turbulence
  • Quick-release designs expedite loading/unloading
  • Must conform to cargo restraint standards (e.g., NAS 3610)

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