Model: 111R107P7

Aircraft Gas Tu Compressor Blade

Special Features:

Original name blade, compressor rotor, turbine engine

Properties:

Overall Length
9.690 inches
Overall Width
2.170 inches
Material Thickness
Between 0.010 inches and 0.020 inches
End Application
Aircraft eng j79
Design Type
Compressor
Criticality Code Justification
Abhp and abmk and abpx and czbj
Engine Section Location
Low pressure compressor
Stage Number
1
Material
Steel blade
NSN
2840-01-106-2587
Part Number
111R107P7
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 111R107P7 NSN 2840-01-106-2587

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

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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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