Model: 4084743CLR

Aircraft Turbine Nozzle Assembly

Special Features:

Drawing name vane, turbine stator, 3 stage, assy of; length is flow area of nozzle

Properties:

Overall Length
Between 4.689 inches and 4.714 inches
End Application
Aircraft eng f100pw100
Design Type
Axial compressor
Blade Attachment Method
Slot
Criticality Code Justification
Agav
Engine Section Location
Low pressure compressor
Stage Number
3
Material
Nickel alloy vane
NSN
2840-01-445-3716
Part Number
4084743CLR
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 4084743CLR NSN 2840-01-445-3716

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:
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133320
UFC:
64100
LTL:
70.0
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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