Model: 3091106-6

Aircraft Gas Turbine Front Frame

Properties:

Inside Diameter
12.480 inches
Overall Length
Between 4.718 inches and 5.738 inches
Outside Diameter
20.660 inches
End Application
Pacer dawn
Criticality Code Justification
Abkv and aarx and abhp
Part Name Assigned By Controlling Agency
Original name frame assembly, turbine engine
Number Of Variable Guide Vanes
20
Material
Titanium alloy
Material Specification
Ems54914, ti6-4 mfr ref single material response
Reference Data And Literature
2j-f1042-4, fig 87, ind 100
NSN
2840-01-347-6914
Part Number
3091106-6
Description
Frame,front,aircraft Gas Turbine
CAGE

A frame used for and part of the front section of an aircraft gas turbine engine. May include struts with or without variable guide vanes.

Part 3091106-6 NSN 2840-01-347-6914

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52345
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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