Model: AMS-QQ-A-250/4
Metal SheetProperties:
Fabrication Method
Rolled
Width
12.000 inches
Length
48.000 inches
Cross-sectional Thickness
0.0600 inches
End Application
Fuselage f4f jet aircraft
Basic Shape Style
Solid
Usage Design
Aircraft
Min. Tensile Strength (psi)
63000 pounds per square inch
Minimum Yield Strength
42000 pounds per square inch
Material
Aluminum alloy, qq-a-250/4
Material
Aluminum alloy 2024
Material Specification
Qq-a-250/4 federal specification 1st material response
NSN
9535-01-531-5842
Part Number
AMS-QQ-A-250/4
Description
Sheet,metal
CAGE
Part AMS-QQ-A-250/4 NSN 9535-01-531-5842
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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