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NSN 2840-01-425-7595, 2840014257595
CASE,TURBINE,AIRCRAFT GAS TURBIN

Federal Supply Classification
FSC 2840 - Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
National Item Identification Number
NIIN 014257595
Codification Country
United States
Item Name Code
INC 50553
Criticality
(Y) This item does not have a nuclear hardened feature but does have other critical feature(s) such as tolerance, fit restriction or application.
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 2840-01-425-7595

National Stock Number (NSN) 2840-01-425-7595, or NIIN 014257595, (case,turbine,aircraft gas turbin) was assigned February 27, 1996 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There are no manufacturer part numbers associated to this NSN.

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 Feb 28, 1996, this NSN's acquisition method was noted as: Not established. Not established.

This NSN is assigned to Item Name Code (INC) 50553. [A CASE THAT IS AN INTEGRAL PART OF AN ENGINE, GAS TURBINE, AIRCRAFT, DESIGNED TO SURROUND AND PROTECT A NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE.]. This item does not have a nuclear hardened feature but does have other critical feature(s) such as tolerance, fit restriction or application. There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 2840014257595 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

CRITICALITY CODE JUSTIFICATION
(CRTL) CZBJ AND APGF AND ABHP AND ABMZ AND FEAT
DESIGN TYPE
(APGF) AXIAL COMPRESSOR
DIAMETER
(ABMZ) 41.230 INCHES NOMINAL
END ITEM IDENTIFICATION
(AGAV) TF33 AIRCRAFT GAS TURBINE ENGINE
ENGINE SECTION LOCATION
(CZBJ) TURBINE
OVERALL LENGTH
(ABHP) 11.640 INCHES NOMINAL
SPECIAL FEATURES
(FEAT) T.O. 2J-TF33-4; FIG 38, 39, 40, 50 ALL INDEXS AND FIG 37, INDEX 1. EXHAUST CASE TO TURBINE NOZZLE CASE REAR FLANGE AND EXHAUST CASE REAR FLANGE PROVIDES A MOUNTING FLANGE FOR AIRCRAFT TAILPIPE

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