Model: 110R343P05

Aircraft Gas Turbine Rotor Blade

Properties:

Overall Length
4.890 inches
End Application
J-47, j-79, t-58 and t-64 aircraft engine
Design Type
Axial compressor
Criticality Code Justification
Abhp and czbj
Engine Section Location
Turbine
NSN
2840-00-502-3079
Part Number
110R343P05
Description
Blade,turbine Rotor,aircraft Gas
CAGE
07482

An item mounted on a disk, turbine, aircraft gas turbine engine. it is designed to create the flow of air in the turbine section of an engine, gas turbine, aircraft.

Part 110R343P05 NSN 2840-00-502-3079

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50535
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:
Y

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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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