Model: 1881M89G02

Aircraft Gas Turb Turbine Nozzle

Special Features:

Original drawing name, nozzle, high pressure turbine-stage 1 machining ht90-b, this is part of the ht90 mod. For the tf39 engine

Properties:

Overall Length
Between 1.873 inches and 1.893 inches
Overall Width
Between 3.110 inches and 3.130 inches
End Application
Aircraft eng tf39
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
High pressure turbine
Stage Number
1
NSN
2840-01-444-8998
Part Number
1881M89G02
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 1881M89G02 NSN 2840-01-444-8998

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:
133320
UFC:
64100
LTL:
70.0
LCL:
--
WCC:
593
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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