Model: 1796M20G01

Aircraft Gas Turbine En Air Seal

Special Features:

T.O. 2j-tf39-4, fig 62, ind 31; ecp 369; dcn 97-37; honeycombed; intersstage; repl p/n 9083m60g05 but not to be grpd per ecp/dcn; whole new configuration; as the old config is repl by tcto kits with the new items, the old config is thrown away, not i&sable

Properties:

Overall Length
Between 2.370 inches and 2.450 inches
Diameter
Between 28.730 inches and 28.850 inches
End Application
Tf-39 aircraft gas turbine engine
Design Type
Axial compressor
Criticality Code Justification
Abhp and abmz and feat
Engine Section Location
High pressure turbine
Stage Number
2
Material
Titanium alloy
Material Specification
B50tf25 cl-a mfr ref single material response
NSN
2840-01-444-7013
Part Number
1796M20G01
Description
Seal,air,aircraft Gas Turbine En
CAGE
07482

A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an engine, gas turbine, aircraft. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.

Part 1796M20G01 NSN 2840-01-444-7013

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50595
FIIG:
A10700
Concept No.:
App. Key:
H
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:
194090
UFC:
95100
LTL:
60.0
LCL:
--
WCC:
713
TCC:
Z
SHC:
9
ACC:
Construction Materials

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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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