Model: 555665

Aircraft Gas Turbine En Air Seal

Special Features:

T.O. 2j-j75-4, fig 13, ind 12; case-rear compressor front

Properties:

Overall Length
Between 1.134 inches and 1.154 inches
Diameter
24.900 inches
End Application
J-75 aircraft engine
Design Type
Axial compressor
Hardness Rating
30.0 rockwell c
Criticality Code Justification
Czbj and sftt and abmz and abhp and feat
Part Name Assigned By Controlling Agency
Original name ring, compressor rotor, aircraft gas turbine engine
Engine Section Location
Compressor
Stage Number
10
Material
Steel
Surface Treatment
Nickel and cadmium
Surface Treatment Specification
Ams2416 assn standard single treatment response
NSN
2840-00-227-8889
Part Number
555665
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 555665 NSN 2840-00-227-8889

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:
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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