Model: 108R857G29

Aircraft Gas Tu Compressor Rotor

Special Features:

Includes stages 1-17; was compressor rotor, axial, turbine engine

Properties:

Overall Length
58.854 inches
Diameter
Between 14.230 inches and 14.245 inches
End Application
Aircraft eng j79
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Stage Number
17
Material
Steel
NSN
2840-01-109-6248
Part Number
108R857G29
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 108R857G29 NSN 2840-01-109-6248

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:
XV
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
93.0 X 43.5 X 52.0
Paclk Weight:
1,449.0000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F005947240
SPI Rev.:
SPC Mkg:
ZZ
LVL_A:
LVL_B:

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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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