Machinability Ratings by Material
Baseline: AISI 1212 free-machining steel = 100%. Higher percentage = easier to machine (higher speeds, longer tool life). Lower percentage = more difficult (reduced speeds, shorter tool life).
Carbon Steels (ISO P — Steel)
| Grade |
Condition |
Rating |
Hardness (HB) |
ISO 513 Subgroup |
Notes |
| 12L14 |
Leaded |
170% |
— |
P01–P05 |
Lead addition acts as chip breaker and lubricant |
| 1215 |
Hot rolled |
136% |
— |
P01–P05 |
High sulfur free-machining |
| 1117 |
Cold drawn |
100% |
— |
P05–P10 |
General purpose free-machining |
| 1018 |
Cold drawn |
78% |
126 |
P10–P15 |
Most common low-carbon steel |
| 1020 |
Annealed |
72% |
111 |
P10–P15 |
Low carbon, slightly gummy |
| 1045 |
As-rolled |
57% |
163–179 |
P15–P20 |
Most common medium-carbon steel for shafts |
| 1045 |
Q&T |
45% |
250–300 |
P20–P25 |
Prehardened condition |
| 1095 |
Annealed |
42% |
190 |
P20–P25 |
High carbon, abrasive carbides |
Alloy Steels (ISO P — Steel)
| Grade |
Condition |
Rating |
Hardness (HB) |
ISO 513 Subgroup |
Notes |
| 4140 |
Annealed |
66% |
197 |
P15–P20 |
Standard Cr-Mo alloy |
| 4140 |
Q&T (prehardened) |
45% |
269–302 |
P20–P25 |
28–32 HRC — common for shafts |
| 4140 |
Q&T (high strength) |
35% |
350 |
P25–P30 |
Reduced speeds required |
| 4340 |
Annealed |
57% |
217 |
P15–P20 |
High-strength Ni-Cr-Mo |
| 4340 |
Q&T (aircraft grade) |
38% |
340–430 |
P25–P30 |
36–45 HRC — difficult |
| 8620 |
Annealed |
66% |
190 |
P15–P20 |
Carburizing grade |
| 300M |
Annealed |
40% |
— |
P25–P30 |
Aerospace, very high strength |
| 4130 |
Normalized |
65% |
187 |
P15–P20 |
Commonly used for aircraft structures |
Stainless Steels (ISO M — Stainless Steel)
| Grade |
Condition |
Rating |
Hardness (HB) |
ISO 513 Subgroup |
Notes |
| 416 |
Free-machining |
85–110% |
— |
M10–M15 |
High sulfur, best stainless for machining |
| 303 |
Free-machining |
78% |
160 |
M10–M15 |
Lead/sulfur added |
| 304 |
Annealed |
45% |
135–175 |
M15–M20 |
Work-hardens severely — use sharp tools |
| 316 |
Annealed |
36–45% |
135–175 |
M20–M25 |
Tougher than 304, lower speeds |
| 316L |
Annealed |
38% |
135 |
M20–M25 |
Lower carbon variant |
| 420 |
Annealed |
45% |
190 |
M15–M20 |
Martensitic, can be heat treated |
| 17-4 PH |
H900 aged |
38% |
350–430 |
M25–M30 |
Precipitation-hardened |
| Duplex 2205 |
Annealed |
30–35% |
250 |
M25–M35 |
Very difficult — high cutting forces |
| Super duplex 2507 |
Annealed |
25–28% |
270 |
M30–M40 |
Highest strength stainless, most difficult |
Cast Iron (ISO K — Cast Iron)
| Grade |
Condition |
Rating |
Hardness (HB) |
ISO 513 Subgroup |
Notes |
| Gray iron Class 20 |
As-cast |
110% |
150–200 |
K10–K15 |
Excellent machinability, graphite lubricates |
| Gray iron Class 30 |
As-cast |
95% |
187–241 |
K10–K15 |
Most common engineering gray iron |
| Gray iron Class 40 |
As-cast |
80% |
180–260 |
K15–K20 |
Higher strength, more abrasive |
| Ductile iron 60-40-18 |
Annealed |
85% |
130–180 |
K15–K20 |
Ferritic, good machinability |
| Ductile iron 80-55-06 |
As-cast |
65% |
170–230 |
K20–K25 |
Pearlitic, more abrasive |
| Ductile iron 120-90-02 |
Q&T |
40% |
248–352 |
K25–K30 |
High strength, difficult |
| CGI (compacted graphite) |
As-cast |
60–70% |
170–230 |
K20–K30 |
Intermediate between gray and ductile |
| Malleable iron |
Annealed |
120% |
130–160 |
K10–K15 |
Easiest cast iron family |
Aluminum and Non-Ferrous (ISO N — Non-Ferrous)
| Grade |
Condition |
Rating |
Hardness (HB) |
ISO 513 Subgroup |
Notes |
| C360 brass |
Free-cutting |
300% |
80–100 |
N05–N10 |
Easiest common metal, sharp tools |
| C932 bearing bronze |
As-cast |
85% |
60–80 |
N10–N15 |
Leaded bronze |
| C510 phosphor bronze |
Hard |
80% |
149–202 |
N10–N15 |
Work-hardens |
| C954 aluminum bronze |
As-cast |
60% |
160–210 |
N15–N20 |
Treat like tough steel |
| 6061-T6 |
T6 |
200–270% |
95–100 |
N05–N10 |
Most common structural aluminum |
| 7075-T6 |
T6 |
140–240% |
150–160 |
N05–N10 |
High-strength aluminum |
| 2024-T4 |
T4 |
180% |
120 |
N05–N10 |
Aircraft aluminum |
| Copper C110 |
Annealed |
70% |
35–80 |
N10–N15 |
Gummy chips — use polished carbide |
| Magnesium AZ31 |
— |
500%+ |
— |
N05 |
Extremely easy (fire hazard — no water coolant) |
Titanium and Superalloys (ISO S — Heat-Resistant Alloys)
| Grade |
Condition |
Rating |
Hardness (HB) |
ISO 513 Subgroup |
Notes |
| Ti-6Al-4V |
Annealed |
22% |
310–340 |
S15–S20 |
Low thermal conductivity — heat at cutting edge |
| Ti-6Al-4V |
Aged |
18% |
370–400 |
S20–S25 |
Higher strength, even harder to machine |
| Ti-6Al-2Sn-4Zr-2Mo |
Annealed |
20% |
330 |
S15–S20 |
High-temperature titanium |
| Inconel 718 |
Aged |
12–15% |
370–470 |
S25–S30 |
Work-hardens severely |
| Inconel 718 |
Solution treated |
15% |
330–360 |
S20–S25 |
Slightly easier than aged |
| Inconel 625 |
Annealed |
15% |
235–270 |
S20–S25 |
Similar difficulty to 718 |
| Hastelloy X |
Annealed |
12% |
235–270 |
S25–S30 |
Very difficult |
| Waspaloy |
Aged |
10% |
— |
S30–S40 |
Most difficult common alloy |
| Rene 41 |
Aged |
10% |
— |
S30–S40 |
Similar to Waspaloy |
| Grade |
Condition |
Rating |
Hardness (HB/HRC) |
ISO 513 Subgroup |
Notes |
| P20 |
Pre-hardened |
55–65% |
270–300 (28–32 HRC) |
P15–P20 |
Best mold steel for machining |
| H13 |
Annealed |
50–60% |
210–235 (20 HRC) |
P15–P20 |
Pre-machine before heat treat |
| H13 |
Hardened |
20–25% |
430–560 (45–55 HRC) |
H15–H25 |
AlCrN coating recommended |
| A2 |
Annealed |
55–65% |
220–235 |
P15–P20 |
Moderate machinability |
| A2 |
Hardened (57–62 HRC) |
15% |
600–700 |
H25–H30 |
Very poor, use AlCrN |
| D2 |
Annealed |
40% |
220–240 |
P20–P25 |
High carbide content, abrasive |
| D2 |
Hardened (58–64 HRC) |
12% |
600–750 |
H30–H40 |
Extremely difficult |
| O1 |
Annealed |
85% |
190–200 |
P10–P15 |
Easiest tool steel to machine |
| S7 |
Annealed |
75% |
220–230 |
P15–P20 |
Good machinability |
| S7 |
Hardened (48–58 HRC) |
18% |
460–600 |
H25–H30 |
Very difficult |
ISO 513 Classification Notes
ISO 513 classifies workpiece materials into six groups, each with a subgroup number (01–50) indicating the required balance of hardness and toughness:
| Group |
Color |
Material Types |
Deep Hole Drilling Notes |
| P |
Blue |
Steel and alloy steel |
Most common; P15–P25 for general gun drilling |
| M |
Yellow |
Stainless steel |
M15–M25 for austenitic; M25–M35 for duplex |
| K |
Red |
Cast iron |
K10–K20 for gray iron; K20–K30 for ductile |
| N |
Green |
Non-ferrous |
N05–N10 for aluminum/brass; N10–N15 for bronze |
| S |
Orange |
High-temp alloys / titanium |
S15–S25 for titanium; S25–S35 for Inconel |
| H |
Grey |
Hardened steel (>45 HRC) |
H15–H25 for 45–55 HRC; H25–H40 for >55 HRC |
Lower subgroup number (01–15) = higher wear resistance, higher speeds, finishing operations.
Higher subgroup number (25–50) = higher toughness, lower speeds, roughing operations.
Drilling Speed Adjustment Factor
To estimate the cutting speed for a material relative to 1045 carbon steel (57% baseline, typical Vc = 70 m/min for carbide gun drilling):
| Rating |
Speed Factor vs 1045 |
Example Vc (carbide gun drill, m/min) |
| 300% (C360 brass) |
× 3.5 |
245 |
| 200% (6061-T6 Al) |
× 2.5 |
175 |
| 100% (1117 steel) |
× 1.75 |
123 |
| 57% (1045 baseline) |
× 1.0 |
70 |
| 45% (304 SS) |
× 0.8 |
56 |
| 30% (2205 duplex) |
× 0.55 |
39 |
| 22% (Ti-6Al-4V) |
× 0.4 |
28 |
| 12% (Inconel 718) |
× 0.25 |
18 |
Formula: Estimated Vc = (Material rating ÷ 57) × 70 m/min. Always verify with manufacturer data and adjust based on observed tool wear and chip formation.
Cost Impact of Low Machinability in Deep Hole Drilling
| Rating |
Relative Tool Wear |
Relative Cycle Time |
Relative Cost per Hole |
Example |
| 200%+ (Aluminum) |
0.3× |
0.3× |
0.3× |
6061-T6 |
| 57% (1045 baseline) |
1.0× |
1.0× |
1.0× |
1045 steel |
| 45% (304 SS) |
1.5× |
1.3× |
1.5–2.0× |
304 stainless |
| 30% (2205 duplex) |
2.5× |
1.5× |
2.5–3.5× |
Duplex stainless |
| 22% (Ti-6Al-4V) |
3.0× |
2.5× |
3.0–5.0× |
Titanium |
| 12% (Inconel 718) |
5.0× |
4.0× |
5.0–8.0× |
Inconel 718 |
Key takeaway: A material with a machinability rating of 22% (titanium) will cost approximately 3–5× more per hole than 1045 steel at equivalent geometry, due to reduced cutting speeds, shorter tool life, and increased inspection frequency.
Factors That Reduce Machinability
| Factor |
Effect on Rating |
Common Materials |
| Work hardening |
Reduces 25–50% |
Stainless steel, duplex, Inconel |
| Abrasive carbides |
Reduces 30–60% |
D2 tool steel, Inconel, CGI |
| Low thermal conductivity |
Reduces 40–60% |
Titanium, Inconel, stainless |
| High ductility (gummy chips) |
Reduces 20–40% |
Copper, low-carbon steel |
| High hardness (> 350 HB) |
Reduces 40–70% |
Hardened steel, 2507 super duplex |
| Casting scale / surface defects |
Reduces 10–20% at entry |
Cast iron, cast stainless |
Using Machinability Ratings for Parameter Selection
Machinability ratings provide a starting point for estimating cutting parameters when manufacturer data is not available:
- Identify the material’s machinability rating from the tables above
- Find the base cutting speed for 1045 steel for the specific operation (gun drilling, BTA, or conventional)
- Multiply by the speed factor from the adjustment table
- Reduce further by L/D correction factors (typically 10–30% for holes exceeding 10×D)
- Adjust feed rate proportionally to maintain chip load — lower machinability generally requires both reduced speed and reduced feed
- Verify with a test cut and adjust based on chip form and tool wear
For detailed cutting parameters by method and diameter, see the Speeds and Feeds Reference for Deep Hole Drilling. For material-specific parameter guides, see the 4140/4340 Alloy Steel Guide and the Deep Hole Drilling Troubleshooting Guide.
Sources: ISCAR Die & Molds Guide; PMPA Craftsman; MSCI machinability ratings; SawbladeUniversity; EOXS; Stanford Advanced Materials; Engineers Edge; Outokumpu machining guidelines; Admiral Metals; Aobo Steel.