Model: 6006T80G30

Aircraft Gas Tu Compressor Rotor

Special Features:

Was compressor rotor, axial, turbine engine

Properties:

Diameter
Between 16.706 inches and 16.720 inches
End Application
Aircraft eng j85-ge-21b
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Stage Number
9
Reference Data And Literature
2j-j85-54
NSN
2840-01-212-2127
Part Number
6006T80G30
Description
Rotor,compressor,aircraft Gas Tu
CAGE
99207

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 6006T80G30 NSN 2840-01-212-2127

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:
OK
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
24.5 X 23.0 X 17.5
Paclk Weight:
--
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
8013215450
SPI Rev.:
SPC Mkg:
03
LVL_A:
F
LVL_B:
F

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
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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