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NSN 2840-01-475-2542, 2840014752542
ENGINE,GAS TURBINE,AIRCRAFT

Federal Supply Classification
FSC 2840 - Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
National Item Identification Number
NIIN 014752542
Codification Country
United States
Item Name Code
INC 50488
Criticality
(F) This item is a Flight Safety Critical Aircraft Part (FSCAP).
Hazardous Material Indicator Code
(N) There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials.
Availability: Readily Available Qualified Suppliers: Currently qualifying suppliers

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DLMS® Summary

National Stock Number 2840-01-475-2542

National Stock Number (NSN) 2840-01-475-2542, or NIIN 014752542, (engine,gas turbine,aircraft) was assigned May 26, 2000 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There is only one manufacturer part number associated with this NSN. None of the associated part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by one supplier. Today, one supplier is listed as an Active supplier for this NSN. Of the active suppliers, only one supplier is deemed design controlled or valid supply parts.

This part number has not been procured by the US Government in over 5 years.

There has been very little demand for this national stock number. The demand for this NSN originated from less than 5 countries. Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on May 27, 2000, this NSN's acquisition method was noted as: Not established. Not established.

This NSN is assigned to Item Name Code (INC) 50488. [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.]. This item is a Flight Safety Critical Aircraft Part (FSCAP). There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 2840014752542 does not contain precious metals.

This NSN is associated to Schedule B 8411124050: turbojet aircraft turbines (engines) other than for civil aircraft, of a thrust exceeding 25 kn. The Schedule B End Use is listed as engines and turbines for military aircraft. NAICS classification category 336412: aircraft engine and engine parts manufacturing.

This information was last updated on .


Technical Characteristics

MOUNTING TYPE
(AAXX) ANY ACCEPTABLE
END ITEM IDENTIFICATION
(AGAV) F100-220F ENGINE
CRITICALITY CODE JUSTIFICATION
(CRTL) AGAV
FUEL TYPE
(FUEL) JET FUEL
POWER OUTPUT FOR WHICH DESIGNED
(AXKD) PNEUMATIC/SHAFT
REFERENCE DATA AND LITERATURE
(RDAL) 2J-F100-46-1

Manufacturer Part Numbers


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