Model: 1359M16G06-110B

Aircraft Gas Tu Compressor Rotor

Special Features:

Supports stage 4-9 blades, provideds seal teeth to prevent air recirculation under stages 4-9 vane shroud and transmits torque between the hpt shaftand hpc front shaft

Properties:

Overall Length
14.500 inches
Diameter
17.000 inches
End Application
F110-100b 2j-f100-4
Criticality Code Justification
Agav
Engine Section Location
High pressure compressor
Material
Nickel alloy
NSN
2840-01-475-3393
Part Number
1359M16G06-110B
Description
Rotor,compressor,aircraft Gas Tu
CAGE
07482

A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. it consists of disks, blades, hubs, and the like. it is the moving part of compressor, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.

Part 1359M16G06-110B NSN 2840-01-475-3393

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50587
FIIG:
A10700
Concept No.:
App. Key:
J
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:
PR
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
671
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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