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Aircraft Gas Turbine Engine NSN 2840-01-525-2111

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 2840-01-525-2111 NSN: 2840-01-525-2111

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Features and Characteristics

End Application
Used on bombardier canadair challenger cl-604 executive jet aircraft
Special Features
1100 hp turbofan engine; op range 2000 plus nautical miles
FSC
2840 Prime Moving; And Components Aircraft Gas Turbines And Jet Engines
NIIN
015252111
NSN
2840015252111

Manufacturer Part Numbers

Part numbers registered to this national stock number.
Part Number
Cage
Status
MSDS
Part Number:
CF-3B
Cage Code:
99207
Status:
A
MSDS:
Part Number:
6089T11G01
Cage Code:
99207
Status:
A
MSDS:

Foreign Trade & Schedule B

What is a Schedule B number? Find more information at help.cbp.gov
  • Schedule B Number: 8411814050
  • NAICS: 336412
  • SITC: 71489
  • Description: Aircraft turbines (engines), except for use in civil aircraft, of a power not exceeding 5000 kw
  • End Use (Code 50020):
    Engines and turbines for military aircraft

Q & A

Frequently asked questions for NSN 2840-01-525-2111
What are the manufacturers of nsn 2840015252111?
Does this nsn 2840015252111 have a shelf life?
No. This NSN does not have an applicable shelf life.
What is the formal definition of nsn 2840015252111
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 2840015252111 contain any precious metals?
No precious metal content.
Does nsn 2840015252111 contain any hazardous materials?
No MSDS. No hazardous material.
What is the ESD classification of nsn 2840015252111?
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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