Model: 6004T21P01

Aircraft Gas Tu Compressor Rotor

Properties:

Overall Length
Between 11.508 inches and 11.512 inches
Diameter
11.000 inches
End Application
J-85 aircraft engine
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Gas turbine engine
Engine Section Location
Compressor
Material
Titanium alloy
NSN
2840-00-784-9681
Part Number
6004T21P01
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 6004T21P01 NSN 2840-00-784-9681

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:
14.3 X 14.3 X 14.5
Paclk Weight:
13.0000lbs
Item Weight:
10.0000lbs
Item Dim:
011501100110
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000003E46
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

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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