Model: AMS-QQ-A-250/11-CT651-0,375X8X36

Metal Plate

Properties:

Fabrication Method
Rolled
Width
8.000 inches
Length
36.000 inches
Cross-sectional Thickness
0.3750 inches
End Application
Fuselage, f4f jet aircraft
Basic Shape Style
Solid
Min. Tensile Strength (psi)
42000 pounds per square inch
Minimum Yield Strength
35000 pounds per square inch
Material
Aluminum alloy, ams-q-250/11, alloy 6061
Material
Aluminum alloy, ams-q-250/11, alloy 6061
NSN
9535-01-531-2534
Part Number
AMS-QQ-A-250/11-CT651-0,375X8X36
Description
Plate,metal
CAGE

Part AMS-QQ-A-250/11-CT651-0,375X8X36 NSN 9535-01-531-2534

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
37013
FIIG:
A13100
Concept No.:
App. Key:
AK
Cond. Code:
2
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
A
ESD:
A
MMAC:
CRITL:
X

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