Model: 1864M32G01

Aircraft Gas Turb Turbine Nozzle

Special Features:

Different from 1864m32g02 note location of holes drilled on stacking axis of airfoils, also note this is part of the ht90 mod for the tf39 engine, also note the drawing name is nozzle, high pressure turbine-stage 2 machining, and nozzle is coated with nickel plating, also length is 4.11745

Properties:

Overall Length
4.117 inches
End Application
Aircraft eng tf39
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
High pressure turbine
Stage Number
2
Material
Nickel
NSN
2840-01-444-6553
Part Number
1864M32G01
Description
Nozzle,turbine,aircraft Gas Turb
CAGE
07482

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 1864M32G01 NSN 2840-01-444-6553

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:
NY
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
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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