Model: AMS-T-9046,CP-1,CDA,0.160

Metal Sheet

Properties:

Fabrication Method
Rolled
Width
36.000 inches
Length
8.000 feet
Cross-sectional Thickness
0.1600 inches
End Application
W/s: aircrafts, eagle f-15, harrier av-8b, and b-2 bomber (atb)
Basic Shape Style
Solid
Min. Tensile Strength (psi)
80000 pounds per square inch
Minimum Yield Strength
70000 pounds per square inch
Heat Treatment
Annealed
Material
Titanium, ams-t-9046, cp-1, cda
Material
Titanium, ams-t-9046, cp-1, cda
Nondefinitive Specification/std Data
Composition cp-1 and condition a
NSN
9535-01-238-6024
Part Number
AMS-T-9046,CP-1,CDA,0.160
Description
Sheet,metal
CAGE
14153

Part AMS-T-9046,CP-1,CDA,0.160 NSN 9535-01-238-6024

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

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
120.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
ZZ
LVL_A:
Z
LVL_B:

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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