Model: 2183505

Aircraft Gas Turbine En Air Seal

Special Features:

T.O. 2j-tf30-44, fig 15, ind 6; rear compressor rotor

Properties:

Overall Length
Between 1.571 inches and 1.588 inches
Diameter
Between 14.877 inches and 14.897 inches
End Application
Aircraft eng tf30
Design Type
Axial compressor
Criticality Code Justification
Apgf and czbj and abhp and abmz and feat
Part Name Assigned By Controlling Agency
Original name seal, air, compressor, stage 11
Engine Section Location
Compressor
Stage Number
11
Material
Nickel alloy
Material Specification
Pwa1022 mfr ref single material response
NSN
2840-01-190-8191
Part Number
2183505
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 2183505 NSN 2840-01-190-8191

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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