Browse Standards AMS5617H
Historical Revised 2000-09-01

Steel, Corrosion Resistant, Bars, Wire, and Forgings 12cr 8.5ni 1.2ti 2.0cu Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable AMS5617H

This specification covers two grades of a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.

These products have been used typically for parts requiring corrosion resistance and high strength up to 800F (425C). The steel can be precipitation hardened to minimum tensile strengths up to 225,000 psi (1550 Mpa).

Certain design and processing procedures may causes these products to become susceptible to stress-corrosion cracking after heat treatment; ARP 1110 recommends practices to minimize such conditions.

AMS5617J
2012-02-09
Latest
Reaffirmed
AMS5617H
2000-09-01
Historical
Revised
AMS5617G
1994-04-01
Historical
Reaffirmed
AMS5617F
1988-07-01
Historical
Revised
AMS5617E
1981-04-01
Historical
Revised
AMS5617D
1979-01-01
Historical
Revised
AMS5617C
1977-07-01
Historical
Revised
AMS5617B
1976-01-01
Historical
Revised
AMS5617A
1973-12-01
Historical
Revised
AMS5617
1969-05-01
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Purchase more aerospace standards and aerospace material specifications and save! AeroPaks off a customized subscription plan that lets you pay for just the documents that you neeed, when you need them.

Get Involved

Want to participate in updating this standard?

X