Model: 6092/SIC/XXP/.125

Metal Sheet

Special Features:

F-16 aircraft: metal matrix composites composed of titanium 0.15, manganese, 0.15, zinc 0.25, copper 0.7-1.0, oxygen 0.05-0.50, chromium 0.15, silicon 0.4-0.8, magnesium 0.8-1.2, iron 0.3, impuriyies 0.15, aluminum remaining; discontinuously reinforced aluminum sheet; aircraft ventral fins

Properties:

Fabrication Method
Any acceptable
Width
30.000 inches
Length
50.000 inches
Cross-sectional Thickness
0.1250 inches
Basic Shape Style
Solid
Min. Tensile Strength (psi)
66000 pounds per square inch
Minimum Yield Strength
57000 pounds per square inch
Material
Aluminum alloy
Material
Aluminum alloy
NSN
9535-01-407-8847
Part Number
6092/SIC/XXP/.125
Description
Sheet,metal
CAGE
1N655

Part 6092/SIC/XXP/.125 NSN 9535-01-407-8847

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:
WF
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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