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NSN 2840-01-192-0856, 2840011920856
BLADE,TURBINE ROTOR,AIRCRAFT GAS

Federal Supply Classification
FSC 2840 - Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
National Item Identification Number
NIIN 011920856
Codification Country
United States
Item Name Code
INC 50535
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 2840-01-192-0856

National Stock Number (NSN) 2840-01-192-0856, or NIIN 011920856, (blade,turbine rotor,aircraft gas) was assigned October 16, 1984 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There are 3 manufacturer part numbers associated with this NSN. 2 of those 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.

This NSN is assigned to Item Name Code (INC) 50535. [AN ITEM MOUNTED ON A DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO CREATE THE FLOW OF AIR IN THE TURBINE SECTION OF AN ENGINE, GAS TURBINE, AIRCRAFT.]. 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 2840011920856 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

END ITEM IDENTIFICATION
(AGAV) ACFT ENG F110
CRITICALITY CODE JUSTIFICATION
(CRTL) APGF AND CZBJ AND ABHP AND ABMZ
DESIGN TYPE
(APGF) AXIAL COMPRESSOR
DIAMETER
(ABMZ) 28.604 INCHES MINIMUM AND 28.644 INCHES MAXIMUM
ENGINE SECTION LOCATION
(CZBJ) HIGH PRESSURE TURBINE
OVERALL LENGTH
(ABHP) 2.767 INCHES MINIMUM AND 2.777 INCHES MAXIMUM
SPECIAL FEATURES
(FEAT) BLADE ATTACHMENT METHOD IS DOVETAIL

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