Model: 4085104

Aircraft Gas Turbine Rotor Blade

Special Features:

T.O. 2j-f100-14, fig 130, ind 9; interim blade replaces p/n 4067004 and is replaced by p/n 4084804 per ecp 95-na027

Properties:

Overall Length
Between 6.771 inches and 6.781 inches
Diameter
Between 29.004 inches and 29.404 inches
End Application
F100-pw-100 aircraft gas turbine engine
Design Type
Axial compressor
Blade Attachment Method
Fir tree
Hardness Rating
45.0 rockwell c and 55.0 rockwell c
Criticality Code Justification
Feat and abmz and abhp and czbj
Engine Section Location
Turbine
Stage Number
4
Material
Nickel alloy
Material Specification
Pwa658 mfr ref single material response
NSN
2840-01-445-2811
Part Number
4085104
Description
Blade,turbine Rotor,aircraft Gas
CAGE
77445

An item mounted on a disk, turbine, aircraft gas turbine engine. it is designed to create the flow of air in the turbine section of an engine, gas turbine, aircraft.

Part 4085104 NSN 2840-01-445-2811

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50535
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:
A
ESD:
ESD:
MMAC:
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
6.3 X 6.3 X 10.5
Paclk Weight:
2.0000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F010001XA1
SPI Rev.:
SPC Mkg:
00
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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