Model: AMS-QQ-A-250/5-CDT351-1,0X6X24

Metal Plate

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 2.5 percent of composite thickness or 2.0 percent of finished plate thickness

Properties:

Fabrication Method
Rolled
Width
6.000 inches
Length
24.000 inches
Cross-sectional Thickness
1.0000 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
42000 pounds per square inch
Heat Treatment
T-351 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
9535-01-531-7800
Part Number
AMS-QQ-A-250/5-CDT351-1,0X6X24
Description
Plate,metal
CAGE
81343

Part AMS-QQ-A-250/5-CDT351-1,0X6X24 NSN 9535-01-531-7800

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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