Model: 869C113P1

Aircraft Gas Tur Bearing Support

Properties:

Inside Diameter
2.834 inches
Overall Length
Between 0.900 inches and 0.940 inches
Outside Diameter
Between 3.060 inches and 3.150 inches
Mounting Hole Diameter
0.281 inches
Mounting Hole Quantity
4
End Application
Aircraft eng
Criticality Code Justification
Agav
Material
Steel
Material Specification
Ams 6280 assn standard single material response
NSN
2840-00-715-5784
Part Number
869C113P1
Description
Support,bearing,aircraft Gas Tur
CAGE
07482

A support designed for a bearing used in an aircraft gas turbine engine. Excludes support,seal,aircraft gas turbine engine.

Part 869C113P1 NSN 2840-00-715-5784

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52565
FIIG:
A521B0
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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