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NSN 2840-01-118-3602, 2840011183602
CASE AND NOZZLE ASSEMBLY,TURBINE

Federal Supply Classification
FSC 2840 - Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
National Item Identification Number
NIIN 011183602
Codification Country
United States
Item Name Code
INC 50539
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.
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DLMS® Summary

National Stock Number 2840-01-118-3602

National Stock Number (NSN) 2840-01-118-3602, or NIIN 011183602, (case and nozzle assembly,turbine) was assigned September 2, 1981 in the Federal Logistics Information System (FLIS). 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 Sep 02, 2020, this NSN's acquisition method was noted as: Not established. Not established.

This NSN is assigned to Item Name Code (INC) 50539. [A NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE WITH A CASE (3), TURBINE, AIRCRAFT 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 2840011183602 does not contain precious metals.

This information was last updated on .


Technical Characteristics

CRITICALITY CODE JUSTIFICATION
(CRTL) AGAV
DESIGN TYPE
(APGF) AXIAL COMPRESSOR
END ITEM IDENTIFICATION
(AGAV) ACFT END TF39
OVERALL WIDTH
(ABMK) 5.683 INCHES MINIMUM AND 5.703 INCHES MAXIMUM
III MATERIAL
(MATT) TITANIUM ALLOY OVERALL
MATERIAL
(MATT) TITANIUM ALLOY OVERALL
ENGINE SECTION LOCATION
(CZBJ) TURBINE
DIAMETER
(ABMZ) 95.930 INCHES MINIMUM AND 95.950 INCHES MAXIMUM
SPECIAL FEATURES
(FEAT) ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE
OVERALL LENGTH
(ABHP) 11.659 INCHES NOMINAL

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