Model: MIL-T-9046

Metal Sheet

Properties:

Fabrication Method
Hot rolled
Width
36.000 inches
Length
8.000 feet
Cross-sectional Thickness
0.0320 inches
Basic Shape Style
Solid
Weight Per Unit Measure
18.912 pounds per piece
Min. Tensile Strength (psi)
125000 pounds per square inch
Minimum Yield Strength
110000 pounds per square inch
Heat Treatment
Annealed
Material
Titanium alloy, ams-t-9046, comp ab-1 or ab-2
Material
Titanium alloy, ams-t-9046, comp ab-1 or ab-2
Surface Condition
Descaled and dull
Surface Condition
Descaled and dull
Nondefinitive Specification/std Data
Composition ab-1 or ab-2, condition annealed
NSN
9535-00-596-2076
Part Number
MIL-T-9046
Description
Sheet,metal
CAGE
81349

Part MIL-T-9046 NSN 9535-00-596-2076

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:
30.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

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

End Items End applications NSN 9535-00-596-2076 is a component of

  • F-111 (fms Only) Aircraft
  • Galaxy C-5 Aircraft
  • Super Jolly H-53 Helicopter
  • F-117a Aircraft

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