Model: AMS-QQ-A-250/24 T76 0.225X48X144

Metal Sheet

Properties:

Fabrication Method
Any acceptable
Width
48.000 inches
Length
144.000 inches
Cross-sectional Thickness
0.2250 inches
End Application
B-2 bomber
Basic Shape Style
Solid
Usage Design
Aircraft
Min. Tensile Strength (psi)
73000 pounds per square inch
Minimum Yield Strength
62000 pounds per square inch
Heat Treatment
T-76 solution heat treated
Material
Aluminum alloy, qq-a-250/24, alloy 7075
Material
Aluminum alloy, qq-a-250/24, alloy 7075
Specification Data
81348/qq-a-250/24 government specification
NSN
9535-01-466-5072
Part Number
AMS-QQ-A-250/24 T76 0.225X48X144
Description
Sheet,metal
CAGE
81343

Part AMS-QQ-A-250/24 T76 0.225X48X144 NSN 9535-01-466-5072

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:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
030740
UFC:
14990
LTL:
60.0
LCL:
--
WCC:
576
TCC:
Z
SHC:
9
ACC:
Construction Materials

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