Material Inconel 718 DA

Technical Reference Library

Inconel 718 DA

UNS N07718 Condition Direct-Aged AMS 5664

Material Overview

Inconel 718 DA is the direct-aged process variant of standard Inconel 718 (UNS N07718) - the most widely used nickel-based superalloy in industry, built around a niobium-and-titanium precipitation-hardening system in a nickel-chromium-iron matrix. "DA" refers to the heat-treatment route, not a different alloy: instead of the conventional full solution treatment followed by aging, direct-aged material is aged directly from the hot-worked or forged condition. Skipping the high-temperature solution anneal suppresses grain growth and produces a finer, more uniform grain structure, which raises yield strength and improves low-cycle fatigue life relative to conventionally solution-treated-and-aged (STA) 718.

This processing route is used specifically for highly stressed rotating components such as turbine disks and rotor hardware, where the finer grain size and higher strength are worth the tighter forging-process control that direct aging demands. Because the chemistry is unchanged from standard 718, the composition table below is identical to the base alloy - what differs is hardness and strength, which run somewhat higher than standard STA 718 and shift the machining parameters accordingly.

International Designation Equivalents

Standard Designation
UNS (base alloy) N07718
WNr / DIN (base alloy) 2.4668
DIN / EN-ISO (base alloy) NiCr19Fe19Nb5Mo3
AMS (direct-age forging stock) 5664
Condition Direct-Aged (DA)

Base-alloy standards are shared with standard Inconel 718 - DA is a heat-treatment condition of the same material, not a separate registered alloy.

Chemical Composition

Element Content
Nickel (Ni) 50.0 – 55.0%
Chromium (Cr) 17.0 – 21.0%
Iron (Fe) Balance (~17 – 21%)
Niobium + Tantalum (Nb+Ta) 4.75 – 5.50%
Molybdenum (Mo) 2.80 – 3.30%
Titanium (Ti) 0.65 – 1.15%
Aluminum (Al) 0.20 – 0.80%
Cobalt (Co) 1.00% max
Carbon (C) 0.08% max

Composition is essentially identical to standard Inconel 718 (see the base-alloy page) - DA is a process/temper variant, not a distinct chemistry. Reused here after verifying against the base 718 record rather than treating this as a separately-sourced material.

Machinability Explained

Inconel 718 DA machines like standard 718 in every fundamental respect - low thermal conductivity concentrates heat at the cutting edge, the alloy work-hardens aggressively under mechanical and thermal stress, it retains strength and hardness at elevated temperature rather than softening like steel, and it is prone to galling and built-up edge against common tool materials. What changes with the direct-aged condition is degree: the finer grain structure and typically higher hardness (often in the 43-44 HRC range versus roughly 42 HRC for standard STA 718) intensify tool wear and make the work-hardening problem slightly less forgiving.

Because the material is somewhat harder and stronger, cutting speeds should sit at the lower end of the standard-718 range or below it, and feed rates need to stay high enough to consistently cut beneath the previous pass's work-hardened layer. Rigid, vibration-free setups, sharp positive-rake carbide with a wear-resistant coating, and generous coolant delivery remain the standard countermeasures, applied with slightly more conservative parameters than on standard 718.

Recommended Cutting Speeds

Operation Vc (m/min) Vc (SFM)
Turning 30 – 40 100 – 130
Milling 25 – 30 80 – 100
Parting 20 – 25 70 – 80
Grooving 25 – 35 80 – 110
Drilling 25 – 35 80 – 110

Slightly more conservative than standard Inconel 718, reflecting the higher hardness typical of the direct-aged condition. Values assume favorable cutting conditions: a well-matched insert grade, rigid tool and workpiece clamping, good-quality raw material, and short tool overhang. Adjust down further for interrupted cuts or poor rigidity.

Recommended FM Carbide Grades by Operation

Turning

Grade Coating ISO Application Range
FM524 CVD S05 – S10
FM2533 CVD S15

Parting / Grooving

Grade Operation Coating ISO Application Range
FM2543 Parting CVD S20
FM2553 Parting CVD S30
FM2533 Grooving CVD S10

Milling

Grade Coating ISO Application Range
FM125 PVD S15 – S35

Ready to cut Inconel 718 DA? Shop FM Carbide inserts matched to this alloy's turning, parting, grooving, and milling requirements.

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Recommended Insert Cutting-Edge Geometry

Parameter Value
Honing Size 0.02 – 0.05 mm / 0.001 – 0.002"
Rake Angle 13° – 18°
Land Angle Neutral
Land Width 0.10 – 0.20 mm / 0.004 – 0.008"
Ground Insert Recommended