TPM ENGINEERING SNAPSHOT · Nº 03

WHAT IS 17-4PH?

The aerospace workhorse stainless: strength of alloy steel + corrosion resistance.

True Precision Machining
1 What it is

A precipitation-hardening martensitic stainless (UNS S17400): chromium–nickel–copper chemistry that gains its strength from a low-temperature copper-precipitate aging cycle — not from quench hardening.

The payoff: alloy-steel strength with stainless-class corrosion resistance — one bar stock, four service conditions.

Fe Bal. · Cr 15.5–17.5 · Ni 3.0–5.0 · Cu 3.0–5.0 · Nb+Ta 0.15–0.45

UNS S17400 AMS 5643

Precipitation-hardening stainless

2 The conditions — the H-number is the aging temperature in °F
Condition Aging temp UTS (ksi) Hardness (HRC) Character
Cond. A Solution annealed — no age ~33 Machine it here
H900 900 °F / 482 °C 190 44 Peak strength
H1025 1025 °F / 552 °C 155 38 Best balance
H1075 1075 °F / 580 °C 145 36 Marine + chloride
H1150 1150 °F / 621 °C 135 33 Toughest
3
Key
properties
UTS
190 ksi
0.2% YS
170 ksi
HARDNESS
HRC 40-44 (H900)
DENSITY
0.280 lb/in³
MACHINABILITY
45 / 100
SPEC
AMS 5643
4
Typical
uses
Aerospace landing gear hardwareHydraulic valve bodiesPump shaftsDefense ordnanceMarine
5 Machinist's note — order of operations
  • Machine in Condition A (solution annealed, ~33 HRC): rough & semi-finish, then heat-treat to the H-condition the drawing calls out.
  • H900 aging CONTRACTS ~0.04–0.06% — a predictable shrinkage, not growth.
  • Thin sections: leave 0.005–0.010″ finish stock for post-aging cleanup. Thicker work usually fits inside standard tolerance as-aged.

Drawing says H900? Machine it in Condition A, age at 900 °F, then passivate. Full datasheet: trueprecisionmachining.com/engineering/datasheets/stainless-17-4ph