Model: 6009T02P01

Aircraft Gas Tu Compressor Blade

Special Features:

Original name blade, compressor rotor, turbine engine

Properties:

Overall Length
4.821 inches
End Application
J-85 aircraft engine
Design Type
Compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Titanium alloy blade
Material Specification
Ams4928 assn standard single material response blade
NSN
2840-00-832-3314
Part Number
6009T02P01
Description
Blade,compressor,aircraft Gas Tu
CAGE
99207

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 6009T02P01 NSN 2840-00-832-3314

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:
U
ESD:
ESD:
MMAC:
OK
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.1000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114990
UFC:
58952
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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