Model: 4063722

Turbine Ring Segment

Properties:

End Application
Aircraft eng f100
General Description
Rockwell c 34-44 hardness, 27.362 min in. 27.422 max in. Od, 1.836 min in. 1.840 max in. W, 26.470 min in. 26.480 max in. Id, 0.240 min in. 0.260 max in. Diameter through 4 holes, stg 3
NSN
2840-01-173-8628
Part Number
4063722
Description
Ring Segment,turbine
CAGE

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:
370.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000002XC8
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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