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9310 ALLOY STEEL AMS 6265 VAR UNS 93106

9310 ALLOY STEEL AMS 6265 VAR UNS 93106

9310 VAR AMS 6265 is a Chromium-Nickel-Molybdenum Alloy used as a Carburizing Grade for Aircraft Parts. Users can obtain high case hardness coupled with high core strength and toughness. High alloy content makes it suitable for use in relatively large cross-sections. Its combination of high alloy and low carbon content can achieve high core hardness with a narrow range between thicker and thinner part cross sections.

This alloy can be used in some applications without case-hardening, as it exhibits strength with excellent toughness and ductility. Carburizing offers a highly wear-resistant surface. Service Steel Aerospace stocks Premium Aircraft Quality produced double melted in an Electric Furnace, followed by a VAR, or Vacuum Arc Remelt (also known as CEVM). Standard air-melted Aircraft Quality AMS 6260 Air Melt material is available on request. 9310 VIM-VAR material is also available on request.

<<9310 ALLOY STEEL AMS 6265 VAR UNS 93106 DATA SHEET>>

9310 VAR steel is typically used in the following applications:

Aircraft engine gears & pinions

Shafts

Clutch Parts

Boring bars

Piston pins

Aluminum rolling mill rolls

 

Common Trade Names:

Lescalloy 9310 Vac-Arc

European Designation 10NiCrMo13-5

9310 VAR

AISI 9310

SAE 9310

 

Common Specifications:

AMS 6265 VAR (CEVM)

AMS 6267 Type 2

AMS 2300 Cleanliness

AMS 6260 Air Melt Aircraft Quality (except VAR)

BPS 299-947-032

MIL-S-7393 Comp 3 (except VAR)

EMS 56729

EMS 56280

 

Chemical Composition:

Symbol Element Min % Max %
C Carbon 0.07% 0.13%
Mn Manganese 0.40% 0.70%
Si Silicon 0.15% 0.35%
P Phosphorus 0.015%
S Sulfur 0.015%
Cr Chromium 1.00% 1.40%
Ni Nickel 3.00% 3.50%
Mo Molybdenum 0.08% 0.15%
B Boron 0.001% (10 ppm)
Cu Copper 0.035%

 

Hardenability Requirements:

Jominy: J 1/16 inch: 41 RC Hardness max

Jominy: J 6/16 inch: 32 RC Hardness max

For Material Normalized 1700° F (927° C) with Test Specimen Annealed 1500° F (816° C)

 

Heat Treatment:

Type Process
Annealing Heat throughout to 1475° – 1575° F, then furnace cool
Normalizing Heat throughout to 1650° – 1750° F, then air cool
Carburizing & Hardening Carburize at 1650° – 1700° F, slow cool. To harden, oil quench from 1425-1545 F
Temper At 250° – 350° F
Approx Case Hardness 60 – 62 HRC
Approx Core Hardness 331 – 363 BHN

 

Typical Core Properties after Pseudo-Carburizing:

Heat Treatment Tensile Strength Yield Strength Elongation in 2″ Reduction of Area Core Hardness
Pseudo Carburized 1700° F for 8 hours. Oil quenched, Tempered at 300° F for 2 hours 187 ksi 155 ksi 15% 51% 375 Bhn
Pseudo Carburized 1700° F for 8 hours. Slow cool to room temperature. Heat to 1425° F, oil quench. Tempered at 300° F for 2 hours 155 ksi 130 ksi 15.5% 52% 331 Bhn
Pseudo Carburized 1700° F for 8 hours. Slow cool to room temperature. Heat to 1525° F, oil quench. Tempered at 300° F for 2 hours 175 ksi 155 ksi 16% 53% 363 Bhn

Pseudo Carburized: Heat Treat with same process as for Carburizing, but without the presence of Carburizing Gas Furnace Atmosphere.

We also supply
MARS190 D6AC AMS 4130
AMS 4340 MOD AMS 4340 AMS 4330 MOD
AMS 9310 AMS 13-8 PH AMS 15-5 PH
AMS 17-4 PH AMS 625 AMS 718
AerMet® 100 Maraging 250 Maraging 300
Maraging 350 Titanium Grade 5 Ti-6Al-4V ELI Titanium

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Founded in 1998, FuShun covers an area of 3000 square meters, annual sales volume of 20000 tons. We are engaged in the manufacture and export of Tool Steel, Nickel Alloy, Stainless Steel and other special steel products…,View more content About Me.

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