Model: QQ-A-250/11-T6-0.02X12X36

Metal Sheet

Properties:

Fabrication Method
Rolled
Width
12.000 inches
Length
36.000 inches
Cross-sectional Thickness
0.0200 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
9535-01-531-2527
Part Number
QQ-A-250/11-T6-0.02X12X36
Description
Sheet,metal
CAGE
81343

Part QQ-A-250/11-T6-0.02X12X36 NSN 9535-01-531-2527

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
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 indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
A
ESD:
A
MMAC:
CRITL:
X

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