Product Parameters
| Item | Specification |
|---|---|
| Material | Ti-6Al-4V, Ti-6Al-4V ELI |
| Specification | ASTM F468, AMS 4965 |
| Thread | Metric (M3–M24), Imperial (1/4"–1") |
| Application | Aerospace, aircraft, spacecraft, high-performance vehicles |
| Surface | Bright finish, passivated, anodized |
| MOQ | 10 pcs |
description
Titanium aircraft bolts are the fasteners that hold aircraft and spacecraft together - the combination of high strength, light weight, and corrosion resistance makes titanium the standard for aerospace fastener applications. Every kilogram saved in fasteners reduces the aircraft weight that the structure must support, so the lightweight of titanium directly translates to fuel savings or payload capacity. Ti-6Al-4V is the standard aerospace titanium alloy - the alloy provides good strength, good corrosion resistance, and the most comprehensive qualification testing and supply base. Ti-6Al-4V ELI (Extra Low Interstitial) has lower carbon, oxygen, and nitrogen content for better ductility and fracture toughness - specified for fatigue-critical applications where those properties matter. ASTM F468 and AMS 4965 define the requirements for titanium bolts in aerospace applications - the specifications cover composition, mechanical properties, dimensions, and testing requirements. The documentation requirements for aerospace fasteners include material test reports and heat batch traceability. The passivated surface is standard for titanium fasteners - the surface treatment removes the alpha case from machining and restores the chromium oxide layer that provides corrosion resistance. Anodizing is used where a colored finish is specified for identification or appearance.

The Weight Math
A steel bolt of the same strength weighs about 60% more than a titanium bolt. On a wide-body aircraft with tens of thousands of fasteners, the weight difference compounds. That is why aerospace specifies titanium - not because it is exotic, but because at aircraft production volumes, the fuel cost difference between steel and titanium fasteners is measurable over the aircraft's operating life.

FAQ
Q1: MOQ?
A1: 10 pieces for aerospace fastener production.
Q2: Materials?
A2: Ti-6Al-4V (standard). Ti-6Al-4V ELI for fatigue-critical applications.
Q3: Specifications?
A3: ASTM F468, AMS 4965. Full traceability and material test reports.
Q4: Surface treatment?
A4: Passivated standard. Anodized for colored identification.
Q5: Lightweight advantage?
A5: Titanium is about 40% lighter than steel - significant in aircraft weight budgets.
Q6: Custom configurations?
A6: Yes. Custom lengths, thread specifications, material grades.
Quality is non-negotiable in precision manufacturing. Every component undergoes rigorous inspection at each stage of production.
- AS/EN/JISQ 9100 - Aerospace quality management for flight-critical and structural parts
- NADCAP - Accredited special processes including heat treatment, NDT, and surface treatment
- DFARS / ITAR - Compliant supply chain for defense and space applications
- Boeing DMS / Airbus SP - Customer-specific requirements documentation available
- Passivation / Electropolishing - ASTM A967 procedures for corrosion resistance
- Material Traceability - Heat number tracking from raw material to finished part
- MIL-A-8625 - Military-specification anodizing for aluminum components
- Coating Thickness Testing - Coating weight and thickness verification per MIL spec
- Salt Spray Testing - 1000-hour ASTM B117 corrosion resistance verification available
From raw material to finished product, every step is controlled and documented:
- Material Preparation - CNC turning/milling to near-net shape
- Heat Treatment - Through-hardening or case-hardening for strength-critical parts
- Surface Preparation - Degreasing, acid cleaning, and surface activation
- Anodizing - Controlled bath process with thickness monitoring
- Sealing / Baking - Chrome sealing, anodize sealing, or hydrogen embrittlement relief baking
- Inspection - Coating thickness measurement, adhesion testing, and visual check
- Packaging - Protective interleaving, VCI packaging, and anti-tarnish wrapping
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