Model: AMS-QQ-A-250/5-O-0.050X6X36

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; tensile strength 30000.0 pounds per square inch; yield strength 14000.0 pounds per square inch

Properties:

Fabrication Method
Rolled
Width
6.000 inches
Length
36.000 inches
Cross-sectional Thickness
0.0500 inches
End Application
Fuselage f4f jet aircraft
Basic Shape Style
Solid
Usage Design
Aircraft
Heat Treatment
O-annealed
Material
Aluminum alloy, qq-a-250/5
Material
Aluminum alloy 2024
Material Specification
Qq-a-250/5 federal specification 1st material response
NSN
9535-01-532-0308
Part Number
AMS-QQ-A-250/5-O-0.050X6X36
Description
Sheet,metal
CAGE
81343

Part AMS-QQ-A-250/5-O-0.050X6X36 NSN 9535-01-532-0308

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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