Model: AMS 4919 TI 6242 0.125X36X96

Metal Sheet

Properties:

Fabrication Method
Hot rolled
Width
36.000 inches
Length
96.000 inches
Cross-sectional Thickness
0.1250 inches
End Application
Aircraft, b-2 bomber (atb)
Basic Shape Style
Solid
Edge Type
Square
Min. Tensile Strength (psi)
135000 pounds per square inch
Minimum Yield Strength
125000 pounds per square inch
Heat Treatment
Annealed
Material
Titanium alloy, ams 4919 ti 6242
Material
Titanium alloy, ams 4919 ti 6242
Surface Condition
Descaled
NSN
9535-01-473-8089
Part Number
AMS 4919 TI 6242 0.125X36X96
Description
Sheet,metal
CAGE
14153

Part AMS 4919 TI 6242 0.125X36X96 NSN 9535-01-473-8089

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:
U
ESD:
A
ESD:
A
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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