Model: AMS-QQ-A-250/1-CDH18-0,016X12X48

Metal Sheet

Properties:

Fabrication Method
Rolled
Width
12.000 inches
Length
48.000 inches
Cross-sectional Thickness
0.0160 inches
End Application
Fuselage f4f jet aircraft
Basic Shape Style
Solid
Min. Tensile Strength (psi)
22000 pounds per square inch
Material
Aluminum alloy, qq-a-250/1
Material
Aluminum alloy 1100
Material Specification
Qq-a-250/1 federal specification 1st material response
NSN
9535-01-531-2518
Part Number
AMS-QQ-A-250/1-CDH18-0,016X12X48
Description
Sheet,metal
CAGE
81343

Part AMS-QQ-A-250/1-CDH18-0,016X12X48 NSN 9535-01-531-2518

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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