Model: AMS-QQ-A-250/5-CDT81-0,04X12X36

Metal Sheet

Special Features:

Thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 5.0 percent of composite thickness or 4.0 percent of finished sheet thickness

Properties:

Fabrication Method
Rolled
Width
12.000 inches
Length
36.000 inches
Cross-sectional Thickness
0.0400 inches
End Application
Fuselage f4f jet aircraft
Basic Shape Style
Solid
Usage Design
Aircraft
Min. Tensile Strength (psi)
62000 pounds per square inch
Minimum Yield Strength
54000 pounds per square inch
Heat Treatment
T-81 solution heat treated
Material
Aluminum alloy, qq-a-250/5
Material
Aluminum alloy 2024
Material Specification
Qq-a-250/5 federal specification 1st material response
NSN
9535-01-531-7795
Part Number
AMS-QQ-A-250/5-CDT81-0,04X12X36
Description
Sheet,metal
CAGE
81343

Part AMS-QQ-A-250/5-CDT81-0,04X12X36 NSN 9535-01-531-7795

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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