Model: 2110M32P01

Aircraf Turbine Nozzle Lock Ring

Special Features:

width; 23.91 inch

Properties:

Overall Thickness
0.030 inches
End Application
Engine, f101-ge-100 (b1)
Part Name Assigned By Controlling Agency
Ring, support liner, nozzle
Material
Titanium alloy
Material Specification
Ams 4911 assn standard single material response
NSN
2840-01-482-2555
Part Number
2110M32P01
Description
Lock Ring,turbine Nozzle,aircraf
CAGE
07482

A round metallic item designed to retain a nozzle, nozzle assembly, or nozzle segment, turbine, aircraft gas turbine engine in a case and nozzle assembly, turbine, aircraft gas turbine engine. It may be a complete 360 degrees circle or a section thereof.

Part 2110M32P01 NSN 2840-01-482-2555

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52365
FIIG:
A522R0
Concept No.:
App. Key:
Cond. Code:
1
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:
--
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:
106460
UFC:
54740
LTL:
70.0
LCL:
--
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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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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