2835-00-098-3405

Nonaircraft Gas Turbine Engine Turbine Rotor

2835000983405 000983405 607463

A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, NONAIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. View more Nonaircraft Gas Turbine Engine Turbine Rotor

2835-00-098-3405 ROTOR,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835000983405 000983405

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
January 2023
NATO Update Count
11
NATO Data Quality
2835-00-098-3405 ROTOR,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835000983405 000983405 1/1
NSN 2835-00-098-3405 (Generic Image) 1/1

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2835-00-098-3405 Related Documents Related Documents 2835-00-098-3405 3+ Documents (More...)

Nonaircraft Gas Turbine Engine Turbine Rotor 37D400131G006RNCC: 5 | RNVC: 2 | DAC: 2 1 Jan 1963 2835-00-098-3405
instructions how to enable JavaScript in your web browser . 5330-15-131-5448Anello5330151315448 151315448 607463
5330-12-702-9551 5330127029551 127029551 is a deformable material which prevents the passage of matter through the joint formed when two faces are joined. it may be metallic or nonmetallic, lubricated or impregnated, solid or hollow cross section. it may be made to any predetermined dimension and shape. excludes flat disks, items made of felt material and items having joints. for round metal and plastic items with an aperture and a solid rectangular cross section, see washer, flat; shim; bearing, washer, thrust; and spacer ring. excludes disk, valve; seal, nonmetallic angle; seal, nonmetallic channel; seal, nonmetallic special shaped section; shielding gasket, electronic; and ring, sealing jar.

2835-00-098-3405 Demil Restrictions 2835-00-098-3405

DEMIL: D | DEMILI: | CRITICALITY: | HMIC: N | PMIC: U | EDC: | ADPEC:

2835-00-098-3405 is a Nonaircraft Gas Turbine Engine Turbine Rotor This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. The precious metals content of this item is unknown.

2835-00-098-3405 HTS and ScheduleB Import and Export 2835-00-098-3405

2835-00-098-3405 End Users End Users 2835-00-098-3405

Greece (ZU01)
Effective Date:
1 Apr 1991

2835-00-098-3405 Manufacturers Approved Sources 2835-00-098-3405

2835-00-098-3405 Related Items NATO Stock Numbers Related to 2835-00-098-3405

2835-00-098-3405 Freight Data Freight Information 2835-00-098-3405

2835-00-098-3405 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 132560. A Sub NMFC of X. It has a NMFC Description of TURBINES STEAM/GAS/WATER/PARTS NOI. 2835-00-098-3405 is rated as class 77.5 when transported by Less-Than Truckload (LTL) freight. 2835-00-098-3405 is rated as class 85 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 61410 which rates the freight between FCL and LCL. It has a Water Commodity Code (WCC) of 593 for ocean manifesting and military sealift. 2835-00-098-3405 is not classified as a special type of cargo when transported by water. 2835-00-098-3405 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.