Model: AMS 4908-0,2X8X36
Metal SheetProperties:
Fabrication Method
Hot rolled
Width
8.000 inches
Length
36.000 inches
Cross-sectional Thickness
0.200 inches
End Application
Phantom aircraft
Basic Shape Style
Solid
Min. Tensile Strength (psi)
860 megapascals
Minimum Yield Strength
760 megapascals
Material
Titanium alloy, ams 4908
Material
Titanium alloy uns r56080
Material Specification
Ams 4908 assn standard 1st material response
NSN
9535-01-517-3546
Part Number
AMS 4908-0,2X8X36
Description
Sheet,metal
CAGE
Part AMS 4908-0,2X8X36 NSN 9535-01-517-3546
INC:
37015 FIIG:
A13100 Concept No.:
App. Key:
AN Cond. Code:
2 Status:
A Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsHMIC:
N
PMIC:
A
ESD:
A
ESD:
A MMAC:
CRITL:
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