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Carbon & alloy steel · AMS 6427 (aircraft quality) · AMS 6411 (vacuum-arc remelted)

4330V Modified Alloy Steel

A 4340-class steel with lower carbon and a vanadium addition for toughness: 220 to 240 ksi with good impact resistance — the aerospace and oil-tool grade for highly stressed components.

UNS K23080Alloy AISI 4330 modified (vanadium)Type Nickel-chromium-molybdenum-vanadium alloy steel, high toughness
Material overview

What 4330V is.

4330V (4330 modified) is a nickel-chromium-molybdenum steel with about 0.30 percent carbon and a small vanadium addition. The lower carbon improves toughness and resistance to shock loading compared with 4340, at the cost of some attainable strength, and the vanadium improves hardenability and impact strength. It is quenched and tempered, most often to 220 to 240 ksi, for airframe parts, bolting, drilling tools and other highly stressed components.

We machine 4330V components, studs and shafts from certified aerospace-quality bar and heat treat to the strength and hardness range on the drawing, with magnetic particle inspection as standard on request.

Get a QuoteDownload the 4330V data sheet (PDF)
Tensile, AMS 6411 min220 ksi
Yield, AMS 6411 min185 ksi
Charpy V-notch, AMS 6411 min15 ft·lbf (longitudinal)
Carbon0.28–0.33 %
Vanadium0.05–0.10 %
MagneticYes
Nominal composition
Fe balance ≈ 95.7%1.65–2.00 ≈ 1.65%0.75–1.00 ≈ 0.75%0.75–1.00 ≈ 0.65%0.28–0.33, 0.025, 0.025, 0.15–0.35, 0.35–0.50, 0.05–0.10, 0.35 trace

Midpoints of the specification ranges, for orientation only. Limits are in the table below.

Specifications & technical data

Chemical composition.

Download the data sheet (PDF) →
Chemical composition — 4330V (UNS K23080)
ElementAMS 6427AMS 6411
Carbon0.28–0.330.28–0.33
Manganese0.75–1.000.65–1.00
Phosphorus, max0.0250.015
Sulfur, max0.0250.015
Silicon0.15–0.350.15–0.35
Nickel1.65–2.001.65–2.00
Chromium0.75–1.000.75–1.00
Molybdenum0.35–0.500.35–0.50
Vanadium0.05–0.100.05–0.10
Copper, max0.350.35

AMS 6427 limits confirmed by Michlin Metals and Aircraft Materials; AMS 6411 limits by Service Steel Aerospace, Michlin Metals and Tech Steel. Percent maximum unless a range is shown.

Physical properties (typical)
Density0.283 lb/in³ (7.84 g/cm³)
MagneticYes
Specifications & technical data

Mechanical properties.

Mechanical properties — 4330V
ConditionTensile strength (ksi)Yield strength 0.2% offset (ksi)Elongation (%)Reduction of area (%)Hardness
AMS 6411 minimum, 220 ksi level (longitudinal)2201851035—
Typical, tempered at 600 °F225193114747 HRC

AMS 6411 minimums for the 220 ksi level, longitudinal, confirmed by Service Steel Aerospace, EMJ and Tech Steel; Charpy V-notch 15 ft·lbf min. Typical values are from the Latrobe (Carpenter) Lescalloy 4330+V VAR datasheet. Strength follows the tempering temperature: 220 to 240 ksi needs a temper of about 500 to 700 °F.

Heat treatmentNormalize at 1600 to 1700 °F. Harden by austenitizing at 1550 to 1600 °F and oil quenching, then double temper (2 + 2 h) at 500 to 700 °F for 220 to 240 ksi; the full tempering range is about 500 to 1100 °F depending on the strength required. Stress relieve at about 400 °F after machining at full strength.
Standards

Specifications that apply.

AMS 64274330 modified bars and forgings, aircraft quality (AMS 2301), vacuum degassed
AMS 64114330 modified bars and forgings, consumable-electrode vacuum remelted (AMS 2300 premium quality)
Forms we supply

How 4330V ships from Houston.

  • Machined components from certified bar
  • Studs, threaded rod and U-bolts
  • Hex bolts and cap screws
  • Nuts, washers and spacers
  • Pins, shafts and bushings
Companion grades
Ultra-high-strength relative300M Ultra-High-Strength Alloy Steel
General-purpose alloy steelAISI 4140 Alloy Steel (UNS G41400)
Where 4330V is used
Drilling tools, subs and crossoversLanding-gear and aircraft structural partsCrankshafts, connecting rods and highly stressed shaftsHigh-pressure valve and wellhead componentsFracture-critical studs and pins
The buyer’s guide

What is 4330V steel?

4330V is an aircraft-quality nickel-chromium-molybdenum steel designed for toughness. Where 4340 uses 0.40 percent carbon, 4330V drops it to about 0.30 percent and adds vanadium, so it can be tempered to 220 ksi and still meet a Charpy requirement. It is supplied to AMS 6427 in aircraft quality or to AMS 6411 vacuum-arc remelted, and is used for airframe components, bolting and oil tools where a brittle failure is unacceptable.

Testing, certification and marking

  • Tensile, hardness and Charpy per heat-treat lot on request
  • Magnetic particle inspection after heat treatment on request
  • Manufacturer's identification and heat number on every piece
  • EN 10204 3.1 material test report; 3.2 witness available

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