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Aircraft Gas Turbine Engine NSN 2840-01-475-2565

Item Description

A continuous combustion type engine. consists primarily of a compressor, aircraft gas turbine engine, chamber, combustion, aircraft gas turbine engine and a turbine assembly, aircraft gas turbine engine. it may have an afterburner, turbine engine and/or a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft, pneumatic power or thrust power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.

NSN 2840-01-475-2565 NSN: 2840-01-475-2565

Features and Characteristics

Mounting Type
Any acceptable
End Application
F100-100 engine
Power Output For Which Designed
Pneumatic/shaft
Criticality Code Justification
Agav
Fuel Type
Jet fuel
Reference Data And Literature
2j-f100-46-1
FSC
2840 Prime Moving; And Components Aircraft Gas Turbines And Jet Engines
NIIN
014752565
NSN
2840014752565

Manufacturer Part Numbers

Part numbers registered to this national stock number.
Part Number
Cage
Status
MSDS
Part Number:
4074200
Cage Code:
77445
Status:
A
MSDS:

Foreign Trade & Schedule B

What is a Schedule B number? Find more information at help.cbp.gov
  • Schedule B Number: 8411124050
  • NAICS: 336412
  • SITC: 71441
  • Description: Turbojet aircraft turbines (engines) other than for civil aircraft, of a thrust exceeding 25 kn
  • End Use (Code 50020):
    Engines and turbines for military aircraft

Q & A

Frequently asked questions for NSN 2840-01-475-2565
What are the manufacturers of nsn 2840014752565?
Does this nsn 2840014752565 have a shelf life?
No. This NSN does not have an applicable shelf life.
What is the formal definition of nsn 2840014752565
A continuous combustion type engine. consists primarily of a compressor, aircraft gas turbine engine, chamber, combustion, aircraft gas turbine engine and a turbine assembly, aircraft gas turbine engine. it may have an afterburner, turbine engine and/or a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft, pneumatic power or thrust power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.
Does nsn 2840014752565 contain any precious metals?
No precious metal content.
Does nsn 2840014752565 contain any hazardous materials?
No MSDS. No hazardous material.
What is the ESD classification of nsn 2840014752565?
No known electrostatic discharge.

Identification Group

Item Identification Guide (IIG) and Item Name Code (INC)
INC
FIIG
App. Key
Cond. Code
Status
INC:
50488
FIIG:
A526A0
App. Key:
Cond. Code:
1
Status:
A

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