Model: 4108T25P01

Aircraft Tu Turbine Blade Damper

Properties:

Overall Length
Between 2.073 inches and 2.093 inches
End Application
F404 engine
Engine Section Location
Turbine
Stage Number
2
Material
Nickel alloy
NSN
2840-01-396-8510
Part Number
4108T25P01
Description
Damper,turbine Blade,aircraft Tu
CAGE
99207

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 4108T25P01 NSN 2840-01-396-8510

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:
ESD:
MMAC:
CRITL:
F

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
593
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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