Model: 5900T51P04

Aircraft Gas Turb Turbine Nozzle

Special Features:

T.O. 2j-j85-94, fig 19, ind 22

Properties:

Overall Length
Between 1.649 inches and 1.683 inches
Diameter
Between 16.855 inches and 16.859 inches
End Application
Engine, acft, turbojet model no. J85-ge-21
Criticality Code Justification
Abhp and abmz and czcj and czbj
Engine Section Location
Turbine
Stage Number
2
Material
Steel
NSN
2840-01-017-2360
Part Number
5900T51P04
Description
Nozzle,turbine,aircraft Gas Turb
CAGE
99207

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 5900T51P04 NSN 2840-01-017-2360

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:
OK
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
593
TCC:
Z
SHC:
Z
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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