2183505

Aircraft Gas Turbine En Air Seal

NSN 2840-01-190-8191

DEMIL
Shelf Life
UOM
NIIN
Demil:
DEMIL/MLI
Shelf Life:
N/A
UOM:
1 EA
NIIN:
011908191

Product Features

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

Product Technical Spec.

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
Item Name:
Seal,air,aircraft Gas Turbine En
Cage Code:
02382

Cross Referenced Parts

Part Number
Cage
RNCC
RNVC
RNAAC
Status
MSDS
SADC
Part Number:
2183505
Cage Code:
77445
RNCC:
3
RNVC:
2
RNAAC:
SB
Status:
A
MSDS:
SADC:
Part Number:
2183505
Cage Code:
54850
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
2183505
Cage Code:
32816
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
2183505
Cage Code:
50381
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
2183505
Cage Code:
15014
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
2183505
Cage Code:
60822
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:

Part Identification

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50595
FIIG:
A10700
Concept No.:
App. Key:
H
Cond. Code:
1
Status:
A

Part Materials

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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Pricing & Availability

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Privacy | Terms

Definition Definition of approved item name (AIN): "Aircraft Gas Turbine En Air Seal"

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.

MOE Major Organizational Entities

Entity
DSOR
User:
DEPARTMENT OF THE AIR FORCE Dept. of the Air Force
DSOR:
Import / Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

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


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