Model: AMS-QQ-A-250/4-T81-0.100X48X12

Metal Sheet

Properties:

Fabrication Method
Rolled
Width
12.000 inches
Length
48.000 inches
Cross-sectional Thickness
0.1000 inches
End Application
Fuselage f4f jet aircraft
Basic Shape Style
Solid
Usage Design
Aircraft
Min. Tensile Strength (psi)
67000 pounds per square inch
Minimum Yield Strength
58000 pounds per square inch
Heat Treatment
T-81 solution heat treated
Material
Aluminum alloy, qq-a-250/4
Material
Aluminum alloy 2024
Material Specification
Qq-a-250/4 federal specification 1st material response
NSN
9535-01-531-7138
Part Number
AMS-QQ-A-250/4-T81-0.100X48X12
Description
Sheet,metal
CAGE
81343

Part AMS-QQ-A-250/4-T81-0.100X48X12 NSN 9535-01-531-7138

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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