9310 N & T

9310 Normalized & Tempered is a carburized grade steel alloy containing nickel, chromium and molybdenum. This alloy provides a high core hardness and high fatigue strength. The normalized and tempered condition offers the best machinability. This material is produced for the purpose of case hardening. It is used for applications where strength, toughness, and high wear resistance are required, making it an excellent choice for aircraft parts. Alloy 9310 is used for the production of aircraft engine gears & pinions, shafts, clutches, and piston pins. (UNS G93106)

Common Applications

  • AerospaceAerospace
  • DefenseDefense

Benefits

  • High Core Hardness
  • High Fatigue Strength
  • High Wear Resistance
  • Good Machinability

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9310 N & T

We Stock 9310 N & T to the Following Specifications:

  • AMS-2301
  • AMS-2304
  • AMS-6260
  • ASTM-A-322
  • HT-5042 CAP. OF
  • MIL-S-7393 COMP. 3

Chemical Makeup

ElementMinMax
Carbon, C0.070.13
Manganese, Mn0.40.7
Silicon, Si0.150.35
Phosphorus, P-0.025
Sulfur, S-0.025
Chromium, Cr11.4
Molybdenum, Mo0.080.15
Nickel, Ni33.5
Copper, Cu-0.35
Boron, B-0.001
Aluminum, Al0.020.05
Vanadium, V0.020.08
Columbium/Niobium, Nb0.020.05

Cross-Fittings

Round

There are 18 sizes and conditions.

  • 1-1/2 - T-HR-TL
  • 1-3/4 - T-HR-TL
  • 2 - T-HR-TL
  • 2-1/2 - T-HR-TL
  • 2-3/4 - T-HR-TL
  • 3 - T-HR-TL
  • 3-1/4 - T-HR-TL
  • 3-1/2 - T-HR-TL
  • 3-3/4 - T-HR-TL
  • 4 - T-HR-TL
  • 4-1/2 - T-HR-TL
  • 5 - T-HR-TL
  • 5-1/2 - T-HR-TL
  • 6 - T-HR-TL
  • 6-1/2 - T-HR-TL
  • 7 - T-HR-TL
  • 7-3/4 - T-HR-TL
  • 8 - T-HR-TL

Flat

There are no sizes and conditions for the flat cross-section.

Square

There are no sizes and conditions for the square cross-section.

Hex

There are no sizes and conditions for the hex cross-section.