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  • Titanium Rod for Aerospace Fasteners Supplier \| Gr5(TC4)/Gr23 ELI, AMS4928/AMS4965, VAR, UT Per AMS2631, MTC 3.1
Titanium Rod for Aerospace Fasteners Supplier \| Gr5(TC4)/Gr23 ELI, AMS4928/AMS4965, VAR, UT Per AMS2631, MTC 3.1

Titanium Rod for Aerospace Fasteners Supplier \| Gr5(TC4)/Gr23 ELI, AMS4928/AMS4965, VAR, UT Per AMS2631, MTC 3.1

Спецификацияtitanium rod for aerospace fasteners, aerospace titanium fastener blank, Gr5 TC4 AMS4928 rod, AMS4965 STA titanium bar, Gr23 ELI F136 fastener stock, Ti-6Al-4V bolt blank Baoji, VAR melted titanium ro

Описание продукции: Aerospace fastener rod from Baoji — Gr5(TC4) per AMS4928/AMS4965 and Gr23 ELI per ASTM F136, VAR double/triple melt, UT per AMS2631, EN 10204 3.1 with measured values. Round/hex blank for bolts, studs

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Titanium Rod for Aerospace Fasteners | Gr5 (TC4) & Gr23 ELI, AMS 4928 / AMS 4965, VAR, MTC 3.1

Meta Description: Aerospace fastener rod from Baoji — Gr5(TC4) per AMS4928/AMS4965 and Gr23 ELI per ASTM F136, VAR double/triple melt, UT per AMS2631, EN 10204 3.1 with measured values. Round/hex blank for bolts, studs, pins. Annealed default; STA PO-stated. Traceability from ingot to fastener.

Overview — An Aerospace Fastener Starts at the Ingot, Not the Lathe

A bolt that goes on an airframe is not "a Ti-6Al-4V rod with threads". It is a documented chain: melt route → forging stock → heat treat condition → UT level → head-formability → MTC numbers. Break one link, the fastener fails audit — even if it machines beautifully.

We supply aerospace fastener blank rod: Gr5/TC4 (AMS 4928 annealed / AMS 4965 STA) and Gr23 ELI (ASTM F136 chain for fracture-critical/implant-adjacent programs). VAR double/triple melt, annealed default, UT per PO, heat-traceable ingot-to-bar. We do not relabel industrial B348 as "aerospace" — the spec on the PO is the contract.

Two Grades, Two Jobs

Grade Spec path Use in fasteners
Gr5 / TC4 (R56400) ASTM B348 + AMS 4928 (annealed) / AMS 4965 (STA) Airframe bolts, structural studs, landing-gear pins, high-load screws
Gr23 ELI (R56401) ASTM F136 / ISO 5832-3 + AMS 4930 chain Fracture-critical, cryogenic, medical-adjacent load paths

Selection rule: static high-load + weight save → Gr5 STA. Fracture-critical / fatigue-dominated / implant-adjacent → Gr23 ELI. Don't buy ELI "just because it sounds better" if the program calls AMS 4928 — pay for the chain you need, not the label.

Annealed vs STA — Write It Into the PO

Condition Spec Strength class When
Annealed (M) AMS 4928 UTS ≥895 MPa, YS ≥828 MPa Machining blanks, moderate-load bolts, default shelf
STA AMS 4965 UTS ~1100–1170 MPa (size-dependent) Max static strength, high-preload airframe fasteners

STA strength steps down with diameter (quench rate drops in big sections) — AMS 4965 sets lower minima for larger bars; that is correct, not a defect. STA is never shelf-default; it needs PO-stated heat treat + re-MTC + weld/PWHT review.

Melt & Traceability Chain (The Part Auditors Check)

  • VAR double (or triple on request) melt — ingot pedigree on MTC
  • Ingot → forge stock → bar → cut blank: one heat number, no break
  • EN 10204 3.1, mill-authorized IR, with measured chemistry + tensile (not minima-only)
  • UT per AMS 2631 / AMS 2154 Class A/AA on request; immersion UT for critical lots
  • Grain size reported; beta-transus / alpha-case check on PO for forged heads
  • 3.2 (SGS/BV/TÜV) witness PO-fronted — not back-signed after shipment
  • AS9100D-documented process available on qualification; confirm scope before PO

Rod Forms for Fastener Production

Form Process fit Note
Round rod (ground/h9) CNC turn + thread roll Most airframe bolt blanks
Hex rod (SW cold-drawn) Bolt head formed by machining/anti-rotate Skip hex-milling op
Forging stock (Ø large) Hot-header / press head Grain flow into head = fatigue win
Centerless ground Screw machine / Swiss Ra 0.4–0.8µm, chamfered ends

Head-Forming Reality (Cold Heading vs Machining)

  • Annealed Gr5 cold-heads with controlled lube + sharp dies; work-hardens fast — heading trial on same heat first
  • STA is not for cold heading — head in annealed state, then heat-treat fastener after forming if STA required
  • Thread rolling > single-point threading for fatigue: compressive surface layer
  • Cleanliness matters: oxide/degreaser residue jams headers; rod delivered VCI-wrapped, no shop oil
  • Diameter consistency ±0.025–0.05mm (h6/h9) keeps head volume repeatable

Stock Scope (Honest)

Grade Ø range Condition Status
Gr5 TC4 Ø6–120mm (common Ø10/16/20/25/32) Annealed (AMS 4928 route) Core heats rotating
Gr5 TC4 STA Per PO AMS 4965 heat treat PO-fronted, not shelf
Gr23 ELI Ø8–80mm project ELI + F136 chain Separate PO, DMR docs
Hex SW6–60mm Cold-drawn h11/h9 Common AF rotating
Length 100–6000mm cut-to-length — Same-week on in-stock heat

Honest line: aerospace-grade heats are qualified, not "click-buy". We confirm AMS clause + melt route + UT level before PI — no ghost "AMS-ready shelf".

Chemistry Ceiling (Reference)

Element max Gr5 (AMS 4928) Gr23 ELI (F136)
O 0.20% 0.13%
Fe 0.40% 0.25%
N 0.05% 0.03%
H 0.015% (AMS tighter on STA) 0.0125%
C 0.08% 0.08%
Al / V 5.5–6.75 / 3.5–4.5% 5.5–6.5 / 3.5–4.5%

Mechanical Floor (Annealed, Measured on MTC)

Grade UTS min YS min Elong
Gr5 (AMS 4928) 895 MPa 828 MPa ≥10%
Gr23 ELI (F136) 860 MPa 790 MPa ≥10%

STA Gr5 per AMS 4965: ~1100+ MPa UTS (size-dependent). Values on MTC are lot-measured, not brochure minima.

UT & Inspection Menu (PO-Selectable)

  • UT: AMS 2631 / AMS 2154 Class A or AA, immersion, FBH calibre stated
  • PT/ET per PO; PMI on request
  • Macro/micro grain, beta fleck, alpha-case on forged head stock
  • Straightness ≤0.5–1mm/m ground bar; chamfer 30–45° for feeder
  • Each blank tagged: heat No. + PO ref + condition (ANN/STA)

Export Packaging for Aerospace Lots

  • VCI + PE sleeve, ends capped, no carbon-steel contact
  • ISPM-15 plywood crate, desiccant, humidity card on long-sea
  • Sealed cert pouch: 3.1 MTC + UT report + process route summary
  • Pre-ship photos: bundle / crate / label / pouch

Enquiry Template (Copy-Paste for Fastener QEs)

Grade: Gr5(TC4) / Gr23 ELI ___
Spec: AMS4928(ann) / AMS4965(STA) / ASTM F136 ___
Diameter: Ø___ mm (or SW___ hex)
Length: ___ mm × ___ pcs (blank vs finish-machined?)
Tolerance: h9 / h6 / per drawing
Condition: annealed / STA (heat-treat PO?)
Melt: VAR double / triple ___
UT: AMS2631 Class A / AA, FBH ___ mm
Ends: chamfer ___° / sawn / faced
Surface: centerless ground Ra___ / peeled
Head route: cold-head / hot-forge / CNC turn
Cert: 3.1 / 3.2 (TPI: ___)
AS9100 / NADCAP scope needed? Y/N
Incoterm: EXW Baoji / FOB Shanghai / DAP ___

FAQ — Titanium Rod for Aerospace Fasteners

Q1: Is industrial B348 Gr5 acceptable for aerospace fasteners?
A: Only if the procurement doc accepts B348. Airframe programs usually require AMS 4928 (annealed) or AMS 4965 (STA) + VAR melt + UT level. We supply both routes; PO names the spec.

Q2: Can you ship STA from stock?
A: No. Annealed is default. STA = PO-stated solution treat + age, re-MTC, size-dependent strength. Quoted lead honest, not "shelf STA".

Q3: Gr23 vs Gr5 for my bolt?
A: Gr5 for high static load + weight. Gr23 ELI for fracture-critical / fatigue / cryogenic / implant-adjacent. ELI costs more and buys toughness, not raw strength.

Q4: Cold heading without cracking?
A: Annealed Gr5 + clean lube + same-heat trial. STA not headable. We support a pre-production header sample before full lot.

Q5: UT level guaranteed?
A: Per PO — AMS 2631 Class A/AA, immersion, FBH calibre written into order. "Zero defect" not contracted; acceptance threshold is.

Q6: MTC with real numbers?
A: Yes — measured chemistry + tensile + heat No. + melt route. Not minima-only.

Q7: Traceability depth?
A: Ingot heat → forge stock → bar → blank. One number crosses the cut. AS9100 process docs on qualification.

Q8: Hex blank for bolt head?
A: SW cold-drawn h11/h9, chamfered, feeder-ready. Skips hex-mill, keeps grain in head.

Q9: Welding STA fastener blanks?
A: Not without PWHT re-evaluation. Head attach by friction weld reviewed per procedure.

Q10: Lead time?
A: In-stock annealed Gr5 heat + PO → same-week cut/dispatch. STA/ELI/UT-class critical → forge+melt schedule quoted before PI.

Request a Quote

Email: sales@[yourdomain].com

Send spec (AMS clause) + grade + Ø + length + qty + UT/class. Reply in 24h: melt route, heat status, condition, MTC type, dispatch date.


About: Baoji Titanium Valley aerospace-blank supplier. Titanium rod for aerospace fasteners — Gr5(TC4) AMS4928/AMS4965 and Gr23 ELI F136 chain, VAR melt, UT per AMS2631, EN 10204 3.1 with measured values. Annealed default; STA PO-stated. No industrial B348 relabeled as "aero". Ingot-to-fastener traceability, or it didn't happen.

titanium rod for aerospace fasteners / AMS4928 TC4 fastener blank Baoji

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Контактная информация

Контактное лицо: Wang Xiaoning

Телефон: +86-917-355-7966

Эл. почта: sales@sxqytd.com

WhatsApp: +86 188 2967 9311

Компания: Shaanxi Qianyi Tuoda Technology Co., Ltd

Адрес: Floor 4, Building 4, No. 188 Gaoxin Avenue, High-tech Zone, Baoji City, Shaanxi Province, China

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