Model: 23036879

Aircraft Tu Turbine Blade Damper

Properties:

End Application
T406-ad-400 engine, ae2100a, c engine, ae2100d2, d3, j engine
Part Name Assigned By Controlling Agency
No. 5 bearing single stage damper
NSN
2840-01-502-1137
Part Number
23036879
Description
Damper,turbine Blade,aircraft Tu
CAGE
63005

A device used to reduce high cycle fatigue on a blade, turbine rotor, aircraft gas turbine engine. it also acts as a seal. it may be of various shapes and cross sections.

Part 23036879 NSN 2840-01-502-1137

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50557
FIIG:
A10700
Concept No.:
App. Key:
A
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:
A
ESD:
A
MMAC:
CRITL:
X

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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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