Model: 4084243CLR

Aircraft Turbine Nozzle Assembly

Special Features:

T.O. 2j-f100-24, fig 109; flow area 4.689-4.714 square inch area

Properties:

Overall Length
2.820 inches
Overall Height
Between 4.717 inches and 4.737 inches
Overall Width
Between 2.036 inches and 2.084 inches
Diameter
Between 13.410 inches and 13.450 inches
End Application
F100-pw-100/200 aircraft gas turbine engine
Design Type
Axial compressor
Blade Attachment Method
Slot
Criticality Code Justification
Matt and abkw and abmk and abhp and feat
Part Name Assigned By Controlling Agency
Original name vane, turbine stator
Engine Section Location
Low pressure turbine
Stage Number
3
Material
Nickel alloy
NSN
2840-01-447-4918
Part Number
4084243CLR
Description
Nozzle Assembly,turbine,aircraft
CAGE
77445

A stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, aircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, aircraft gas turbine engine. it may have an inner support shroud. the assembled item forms a complete circle.

Part 4084243CLR NSN 2840-01-447-4918

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50581
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:
NZ
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
6.3 X 5.3 X 4.0
Paclk Weight:
1.3000lbs
Item Weight:
0.9000lbs
Item Dim:
004800360020
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000001XC2
SPI Rev.:
SPC Mkg:
17
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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