Model: 5115T28G06

Aircraft Gas Turbine Front Frame

Properties:

End Application
Ge f414-400 turbine engine
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Frame assembly, front
Reference Data And Literature
A1-f414a-ipb-400, fig 04 00
NSN
2840-01-487-3530
Part Number
5115T28G06
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 5115T28G06 NSN 2840-01-487-3530

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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
--
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
03
LVL_A:
E
LVL_B:
Q

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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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