Model: 5103T26P01

A Inner Augmentor Nozzle Section

Properties:

End Application
Ge f414-4000 engine
NSN
2840-01-443-4137
Part Number
5103T26P01
Description
Augmentor Nozzle Section,inner,a
CAGE
99207

A rigid item designed to help direct the flow of hot gases from an afterburner,turbine engine. it is an integral part of a nozzle,augmentor exhaust, aircraft gas turbine engine. the item is to the rear of and hinged to an augmentor nozzle section,convergent, aircraft gas turbine engine.

Part 5103T26P01 NSN 2840-01-443-4137

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
53241
FIIG:
A526N0
Concept No.:
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:
X

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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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