Model: AMS-QQ-A-250/4-CDT351-0,625X8X36

Metal Plate

Properties:

Fabrication Method
Rolled
Width
8.000 inches
Length
36.000 inches
Cross-sectional Thickness
0.6250 inches
End Application
Fuselage f4f jet aircraft
Basic Shape Style
Solid
Usage Design
Aircraft
Min. Tensile Strength (psi)
63000 pounds per square inch
Minimum Yield Strength
42000 pounds per square inch
Heat Treatment
T-351 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
9535-01-531-6282
Part Number
AMS-QQ-A-250/4-CDT351-0,625X8X36
Description
Plate,metal
CAGE
81343

Part AMS-QQ-A-250/4-CDT351-0,625X8X36 NSN 9535-01-531-6282

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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