Model: 1361M85G01

Aircraft Gas Turbi Turbine Frame

Properties:

Overall Length
Between 3.460 inches and 3.520 inches
Outside Diameter
Between 17.320 inches and 17.360 inches
End Application
F118-ge-100
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Centerbody, forward
Material
Stainless steel
Reference Data And Literature
2j-f118-4 f59 i19
NSN
2840-01-505-5823
Part Number
1361M85G01
Description
Frame,turbine,aircraft Gas Turbi
CAGE
07482

A frame used for and part of a turbine assembly,aircraft gas turbine engine. May include struts.

Part 1361M85G01 NSN 2840-01-505-5823

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52349
FIIG:
A522Q0
Concept No.:
1
App. Key:
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:
CRITL:
Y

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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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