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2840-01-582-2318

Turbo-Jet Engine

2840015822318 015822318 5100T20G01

A continuous-combustion type power unit, may be with or without container, designed to exert thrust. It's prime physical characteristics include air compressor(s), combustion chamber(s) and gas turbine. The operating principle is as follows: atmospheric air is inducted into the unit at its front, compressed, heated by combustion of a fuel, expanded through the gas turbine, and ejected at high velocity. It may incorporate features to vary direction of the thrust. View more Turbo-Jet Engine

2840-01-582-2318 ENGINE,TURBO-JET 2840015822318 015822318

Managed by United States
NSN Created on 11 Feb 2010
Data Last Changed
July 2023
NATO Update Count
6
NATO Data Quality
2840-01-582-2318 ENGINE,TURBO-JET 2840015822318 015822318 1/1
NSN 2840-01-582-2318 (Generic Image) 1/1

2840-01-582-2318 Product Information Product Information 2840-01-582-2318

The General Electric F414 is an American afterburning turbofan engine in the 22,000-pound (98 kN) thrust class produced by GE Aviation. GE evolved the F404 into the F412-GE-400 non-afterburning turbofan for the McDonnell Douglas A-12 Avenger II. After the cancellation of the A-12, the research was directed toward an engine for the F/A-18E/F Super Hornet. The F414 originated from GE’s widely used F404 turbofan, enlarged and improved for use in the Boeing F/A-18E/F Super Hornet and EA-18G Growler electronic attack with significant survivability and payload improvement compared to earlier weapon systems.

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2840-01-582-2318 Related Documents Related Documents 2840-01-582-2318 5+ Documents (More...)

2840144435016 144435016 364-7506 Turbo-Jet Engine 2840123647506 123647506 912-6444 2840-99-645-9394 2840-01-582-2318
2840-14-538-4707 000-8534 Turbo-Jet Engine 2840160008534 160008534 912-6444 2840-99-645-9394 2840-01-582-2318
2840-14-538-4707 042-0312 Turbo-Jet Engine 2840140420312 140420312 912-6444 2840-99-645-9394 2840-01-582-2318
2840-16-000-8534 Turbo-Jet Engine 2840160008534 160008534 443-5016 2840-14-538-6344 645-9394 2840-01-582-2318
Turbo-Jet Engine 2840123647506 123647506 538-6337 2840-14-443-5016 2840-14-538-6344 645-9394 2840-01-582-2318
www.nsnlookup.com /fsg-28/fsc-2840/de 2840-12-364-7506 Turbo-Jet Engine 2840123647506 123647506 645-9394 2840-01-582-2318
-2840/de 2840-12-364-7506 Turbo-Jet Engine 2840123647506 123647506 912-6444 2840-99-645-9394 2840-01-582-2318
-2840/cz 2840-16-000-8534 Turbo-Jet Engine 2840160008534 160008534 912-6444 2840-99-645-9394 2840-01-582-2318
-2840/fr 2840-14-042-0312 Turbo-Jet Engine 2840140420312 140420312 912-6444 2840-99-645-9394 2840-01-582-2318
364-7506 Turbo-Jet Engine 2840123647506 123647506 364-7506 2840-21-912-6444 2840-99-645-9394 2840-01-582-2318
000-8534 Turbo-Jet Engine 2840160008534 160008534 000-8534 2840-21-912-6444 2840-99-645-9394 2840-01-582-2318
RNVC 2 DAC 6 NATO Stock Numbers Related to 2840-14-538-6337 2840-21-912-6444 2840-99-645-9394 2840-01-582-2318
2840144435016 144435016 364-7506 Turbo-Jet Engine 2840123647506 123647506 912-6444 2840-99-645-9394 2840-01-582-2318
2840-14-538-4707 000-8534 Turbo-Jet Engine 2840160008534 160008534 912-6444 2840-99-645-9394 2840-01-582-2318
RNVC 9 DAC 9 NATO Stock Numbers Related to 2840-99-645-9394 2840-21-912-6444 2840-99-645-9394 2840-01-582-2318

2840-01-582-2318 Demil Restrictions 2840-01-582-2318

DEMIL: C | DEMILI: 1 | CRITICALITY: F | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

2840-01-582-2318 is a Turbo-Jet Engine that is an aviation critical safety item or flight safety critical aircraft part. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item where key elements must be removed and destroyed to prevent this item being restored or repaired. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-582-2318 End Users End Users 2840-01-582-2318

Australia (ZA01)
Effective Date:
1 Feb 2010

2840-01-582-2318 Manufacturers Approved Sources 2840-01-582-2318

2840-01-582-2318 Technical Data Datasheet 2840-01-582-2318

Characteristic
Specifications
FIIG
A526A0
Part Name Assigned By Controlling Agency [CXCY]
Model F414-Ge-400 Turbofan Engine

2840-01-582-2318 Stock, Inventory and Procurement DLA Procurement Analysis 2840-01-582-2318

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2840-01-582-2318 Related Items NATO Stock Numbers Related to 2840-01-582-2318

2840-01-582-2318 Freight Data Freight Information 2840-01-582-2318

2840-01-582-2318 has freight characteristics managed by Australia.. 2840-01-582-2318 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

2840-01-582-2318 Contracting Technical Data File (CTDF) Contracting Technical Data File (CTDF) 2840-01-582-2318 October 2021

Criticality and Quality

Critical Item Code:
X
Flight Safety:
Life Support:
Certified Samples:
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First Article Test (FAT):
Certificate of Quality Compliance:
Production Lot Testing:
Special Testing:
Qualified Products List (QPL):

Commercial Properties

Government Furnished Material:
Government Furnished Tooling:
Government Furnished Property:
Price Evaluation Code:
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Warranty:
Commerical Off The Shelf (COTS):
End Item Application:
Auctioning Candidate:
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Contract Option:

Restrictions

Boeing Rights Guard:
Export Controlled:
Controlled Technical Data Package (TDP):
Restricted Technical Data Package (TDP):
Contains Classified Material
Weapons System Indicator Code (WSIC):
N

Packaging Requirements

Packaging Determination Table:
Packaging Review Code:
Y
Special Packaging Instruction Number (SPIN):
Special Packaging Instruction Number Revision:
Special Packaging Instruction Number Date:
Pallet Reference Number Required: