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NSN 2840-01-160-3218, 2840011603218
VANE,COMPRESSOR,AIRCRAFT GAS TUR

Federal Supply Classification
FSC 2840 - Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
National Item Identification Number
NIIN 011603218
Codification Country
United States
Item Name Code
INC 50611
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 2840-01-160-3218

National Stock Number (NSN) 2840-01-160-3218, or NIIN 011603218, (vane,compressor,aircraft gas tur) was assigned August 19, 1983 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.

Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on Apr 01, 2007, this NSN's acquisition method was noted as: Acquire directly from the actual manufacturer, whether or not the prime contractor is the actual manufacturer. The rights to use the data needed to purchase this part from additional sources are not owned by the Government and cannot be purchased. Valid AMCs: 1, 2, 3, 4 and 5.

This NSN is assigned to Item Name Code (INC) 50611. [A COMPONENT OF A VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO RECEIVE AIR FROM THE PRECEDING COMPRESSOR BLADES AND DELIVER IT TO THE SUCCEEDING ROW OF COMPRESSOR BLADES, DIFFUSER, OR COMBUSTION AREA AT CORRECT PRESSURE, VELOCITY AND DIRECTION.]. 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 2840011603218 does not contain precious metals.

This NSN is associated to Schedule B 8411997050: parts of gas turbine aircraft engines, other than for use in civil aircraft. 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

SPECIAL FEATURES
(FEAT) ORIGINAL NAME COMPRESSOR,AXIAL,TURBINE ENGINE
MATERIAL
(MATT) STEEL CORROSION RESISTING OVERALL
END ITEM IDENTIFICATION
(AGAV) ACFT ENG TF33
CRITICALITY CODE JUSTIFICATION
(CRTL) FEAT
DESIGN TYPE
(APGF) AXIAL COMPRESSOR
DIAMETER
(ABMZ) 27.720 INCHES MINIMUM AND 27.740 INCHES MAXIMUM
ENGINE SECTION LOCATION
(CZBJ) COMPRESSOR
OVERALL LENGTH
(ABHP) 1.241 INCHES MINIMUM AND 1.243 INCHES MAXIMUM
PART NAME ASSIGNED BY CONTROLLING AGENCY
(CXCY) COMPRESSOR STATOR 15 STAGE,ASSY OF
MATERIAL
(MATT) UNABLE TO DECODE
REFERENCE DATA AND LITERATURE
(RDAL) T.O. 2J-TF33-4 FIG 17, IND 39
SPECIAL FEATURES
(FEAT) TOLERANCE, FIT AND FUNCTION
CRITICALITY CODE JUSTIFICATION
(CRTL) AGAV
III MATERIAL
(MATT) STEEL CORROSION RESISTING OVERALL

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