Model: 111R115P11

Aircraft Gas Tu Compressor Blade

Properties:

Overall Length
Between 16.600 inches and 16.800 inches
End Application
Gas turbine and jet eng acfts
Design Type
Compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Titanium alloy
NSN
2840-00-083-6920
Part Number
111R115P11
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 111R115P11 NSN 2840-00-083-6920

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:
PL
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
593
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

End Items End applications NSN 2840-00-083-6920 is a component of

  • Gas Turbine And Jet Eng Acfts
  • Cfm 56 T 64 T 58 J 93 J 73 J 47 General Electric Jet Engines & Components
  • 010225222
  • Aircraft Gas Turbine Engine Compressor Rotor

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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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