Model: 4082943CLR

Aircraft Gas Turb Turbine Nozzle

Special Features:

T.O. 2j-f100-14, fig 132; flow area 4.689-4.714

Properties:

Overall Length
Between 2.246 inches and 2.254 inches
Overall Height
Between 4.717 inches and 4.737 inches
Overall Width
Between 2.036 inches and 2.084 inches
End Application
F100-pw-100 aircraft gas turbine engine
Design Type
Axial compressor
Criticality Code Justification
Abmk and abhp and abkw and feat and czcj
Engine Section Location
Turbine
Stage Number
3
Material
Nickel alloy
NSN
2840-01-445-5374
Part Number
4082943CLR
Description
Nozzle,turbine,aircraft Gas Turb
CAGE
77445

A single 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.

Part 4082943CLR NSN 2840-01-445-5374

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50585
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:
030660
UFC:
14960
LTL:
70.0
LCL:
--
WCC:
576
TCC:
Z
SHC:
9
ACC:
Construction Materials

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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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