Model: AMS-QQ-A-250/14
Metal SheetProperties:
Fabrication Method
Rolled
Width
12.000 inches
Length
48.000 inches
Cross-sectional Thickness
0.100 inches
End Application
Fixed wing aircraft, mcdonnel douglas f-4f phantom
Basic Shape Style
Solid
Min. Tensile Strength (psi)
40000 pounds per square inch
Minimum Yield Strength
21000 pounds per square inch
Material
Aluminum alloy, qq-a-250/14
Material
Aluminum alloy, qq-a-250/14
NSN
9535-01-524-2401
Part Number
AMS-QQ-A-250/14
Description
Sheet,metal
CAGE
Part AMS-QQ-A-250/14 NSN 9535-01-524-2401
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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