Model: MIL-S-18729
Metal SheetProperties:
Fabrication Method
Rolled
Cross-sectional Thickness
0.0630 inches
End Application
Aircraft, mcdonnell douglas, phantom f4f
Min. Tensile Strength (psi)
95000 pounds per square inch
Minimum Yield Strength
7500 pounds per square inch
Heat Treatment
Normalized
Material
Steel, ams 6345, alloy 4130
Material
Steel, ams 6345, alloy 4130
NSN
9515-01-517-3521
Part Number
MIL-S-18729
Description
Sheet,metal
CAGE
Part MIL-S-18729 NSN 9515-01-517-3521
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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