Model: 3091728-2

Aircraft Gas Turb Turbine Nozzle

Special Features:

Forward impingement nozzle

Properties:

Overall Length
Between 2.327 inches and 2.357 inches
Overall Width
Between 0.440 inches and 0.460 inches
End Application
Pacer dawn
Criticality Code Justification
Agav
Engine Section Location
High pressure turbine
Material
Nickel alloy vane
NSN
2840-01-349-0429
Part Number
3091728-2
Description
Nozzle,turbine,aircraft Gas Turb
CAGE
99193

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 3091728-2 NSN 2840-01-349-0429

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

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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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