Model: 2189121

Aircraft Gas Turbine En Air Seal

Special Features:

T.O. 2j-tf30-44

Properties:

Overall Length
Between 1.777 inches and 1.787 inches
Diameter
Between 8.590 inches and 8.610 inches
Material Thickness
Between 0.075 inches and 0.085 inches
End Application
Tf-30 aircraft eng
Criticality Code Justification
Agav
Engine Section Location
Turbine
Stage Number
2
Material
Nickel alloy
Material Specification
Pwa1007 mfr ref single material response
NSN
2840-01-353-0897
Part Number
2189121
Description
Seal,air,aircraft Gas Turbine En
CAGE
77445

A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an engine, gas turbine, aircraft. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.

Part 2189121 NSN 2840-01-353-0897

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50595
FIIG:
A10700
Concept No.:
App. Key:
H
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:
PQ
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
713
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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