Model: AMS-QQ-A-250/4

Metal Sheet

Properties:

Fabrication Method
Rolled
Width
6.000 inches
Length
36.000 inches
Cross-sectional Thickness
0.0630 inches
End Application
Fuselage f4f jet aircraft
Basic Shape Style
Solid
Physical Form
Flat stock
Usage Design
Aircraft
Min. Tensile Strength (psi)
63000 pounds per square inch
Minimum Yield Strength
42000 pounds per square inch
Part Name Assigned By Controlling Agency
Aluminum alloy 2024, plate and sheet
Heat Treatment
T-3 solution heat treated
Material
Aluminum alloy, qq-a-250/4
Material
Aluminum alloy 2024
Material Specification
Qq-a-250/4 federal specification single material response
Specification Data
81343-sae-ams-qq-a-250/4a national std/spec
NSN
9535-01-531-5843
Part Number
AMS-QQ-A-250/4
Description
Sheet,metal
CAGE
81343

Part AMS-QQ-A-250/4 NSN 9535-01-531-5843

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

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
106140
UFC:
54590
LTL:
50.0
LCL:
--
WCC:
576
TCC:
Z
SHC:
9
ACC:
Construction Materials

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