AMS 5560

MATERIAL TECHNICAL STANDARD - AMS 5560
MATERIAL CATEGORY - High Alloy Aerospace Material Steel Series
TECHNICAL SPECIFICATION - AMS 5560N
HS CODE - 72221100 / 72221900 / 72223000
OFFICIAL TEST REPORT - issued by TUV - SGS - BV
CHEMICAL COMPOSITIONS (WEIGHT - %)
C (％):    ≤ 0.08
Mn (％):  ≤ 2.00
Si (％):    ≤ 1.00
P (％)≤:   0.030
S (％)≤:   0.030
Cr (％):   18.0 ~ 20.0
Ni (%):    8.00 ~ 12.0
Mo (％):  ≤ 0.75
Cu (%):   ≤ 0.75
MECHANICAL PROPERTIES UNDER ROOM TEMP.
Form: Tubings and forgings
Heat treatment condition: 1010 ~ 1070 Deg. C 
Tensile strength, σb/MPa: 685
Yield strength, σ0.2/MPa: -
Elongation, δ(％): 27.0
Reduction of area, ф(％): -
Hardness + solution annealed (HB): -
MELTING PROCESS & APPLICATION
This alloy is generally smelt in Basic Electric Furnace or VIM + Electroslag remelting (ESR). For a purpose of superior quality, it should be smelt via technology of vacuum refining or by agreement.
It is suitable for applications such as high tensile shafts, bolts and nuts, gears, pinions spindles and so on.
AVAILABLE FORMS & DIMENSIONS
Round bar: 5.5mm to 400mm
Square bar / Flat bar: 10mm to 610mm
Wire rod: 0.5mm to 13.0mm
Steel strip: THK0.5 ~ 3.0mm, Width 10 ~ 500mm
Length: Fixed length or random length or based on the customer's special requirement.
Other different shapes based on OEM. 
TECHNICAL SALES ASSISTANCE & SERVICE
If you meet further on any technical enquiry, pleased to EMAIL our resident team of qualified production engineers. E-mail: sales@cnlhss.com