Model: 108R818P1

Aircraft Gas Tu Compressor Blade

Special Features:

Original name blade, compressor rotor, turbine engine

Properties:

End Application
J-47, j-79, t-58, t-64 aircraft eng
Design Type
Compressor
Blade Attachment Method
Slot
Criticality Code Justification
Agav
Engine Section Location
High pressure compressor
Stage Number
15
NSN
2840-00-798-7935
Part Number
108R818P1
Description
Blade,compressor,aircraft Gas Tu
CAGE
07482

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

Part 108R818P1 NSN 2840-00-798-7935

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50531
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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