Model: 1-140-420-04

Aircraft Gas Turb Turbine Nozzle

Special Features:

23 vanes, 2.025 in.Min, 2.035 in.Max o/a lg, 14.700 in.Nom od, 2.615 in.Min, 2.168 in.Max id support, 44 holes 0.220 in.Nom diameter through nozzle flange equally spaced on 14.250 in.Nom bolt circle dia, 12 holes 0.0975 in.Min, 0.1025 in.Max through support on 3.220 in.Bolt circle dia;

Properties:

End Application
T-53 series engines
NSN
2840-00-085-3880
Part Number
1-140-420-04
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 1-140-420-04 NSN 2840-00-085-3880

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:
U
ESD:
A
ESD:
A
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
92.5
WCC:
593
TCC:
Z
SHC:
9
ACC:
Trailers/Vehicles

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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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