Model: 1881M89G01

Aircraft Gas Turb Turbine Nozzle

Special Features:

T.O. 2j-tf39-4, fig 61, ind 2; ecp 369, dcn 97-37; 1.451 in. Between nozzle air flow cavities oc; 1.703 length of nozzle fin; 1.415 width of nozzle fin; repl p/n 9082m95g15; not to be grped per ecp/dcn; whole new configuration; as the old config is replaced by tcto kits with the new item, the old config is then thrown away

Properties:

Overall Length
Between 1.883 inches and 1.888 inches
Overall Height
3.351 inches
End Application
Tf-39 aircraft gas turbine engine
Design Type
Axial compressor
Criticality Code Justification
Abhp and abkw and feat
Engine Section Location
High pressure turbine
Stage Number
1
NSN
2840-01-444-6999
Part Number
1881M89G01
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 1881M89G01 NSN 2840-01-444-6999

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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