Model: 3092067-8

Aircraft Gas Turbine En Oil Sump

Properties:

Overall Length
Between 3.058 inches and 3.062 inches
Diameter
Between 8.843 inches and 8.845 inches
End Application
Pacer dawn
Criticality Code Justification
Agav
Engine Section Location
Turbine
Material
Titanium alloy
NSN
2840-01-385-3474
Part Number
3092067-8
Description
Sump,oil,aircraft Gas Turbine En
CAGE
99193

A chamber surrounding the main bearings for a shaft, turbine, aircraft gas turbine engine. The chanber is used to collect lubricating fluid for recirculation.

Part 3092067-8 NSN 2840-01-385-3474

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52549
FIIG:
A10700
Concept No.:
App. Key:
G
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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