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2840-00-971-6287

Aircraft Gas Turbine Engine Turbine Rotor Blade

2840009716287 009716287 1-190-008-02

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. View more Aircraft Gas Turbine Engine Turbine Rotor Blade

2840-00-971-6287 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840009716287 009716287

Managed by United States
NSN Created on 28 Sep 1966
Data Last Changed
January 2023
NATO Update Count
17
NATO Data Quality
2840-00-971-6287 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840009716287 009716287 1/1
NSN 2840-00-971-6287 (Generic Image) 1/1

2840-00-971-6287 Stock and Availability Marketplace 2840-00-971-6287

2840-00-971-6287 Related Documents Related Documents 2840-00-971-6287 1+ Documents (More...)

1-190-008-02 An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
United States (US) 4. 2840-00-971-6287 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-00-971-6287 RQST Updated Every Day 2840-00-971-6287 RQST NE Related

2840-00-971-6287 Demil Restrictions 2840-00-971-6287

DEMIL: B | DEMILI: | CRITICALITY: X | HMIC: N | PMIC: U | EDC: | ADPEC: 0

2840-00-971-6287 is a Aircraft Gas Turbine Engine Turbine Rotor Blade that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. The precious metals content of this item is unknown.

2840-00-971-6287 HTS and ScheduleB Import and Export 2840-00-971-6287

2840-00-971-6287 End Users End Users 2840-00-971-6287

Brazil (YA01)
Effective Date:
1 Dec 2008
Spain (YB01)
Effective Date:
1 Apr 1991
Singapore (YJ01)
Effective Date:
1 Aug 1996
New Zealand (ZE01)
Effective Date:
1 Apr 1991
Germany (ZG01)
Effective Date:
1 Apr 1991
Republic of Korea (ZH01)
Effective Date:
1 Apr 1991

2840-00-971-6287 Manufacturers Approved Sources 2840-00-971-6287

2840-00-971-6287 Technical Data Datasheet 2840-00-971-6287

Characteristic
Specifications
FIIG
A10700
Part Name Assigned By Controlling Agency [CXCY]
Blade,Turbine,Rotor Turbine Engine
Special Features [FEAT]
Nickel Alloy M3602 Fscm 91547,Rockwell C Scale 35 Min,40 Max Hardness,0.988 In. Min,0.991 In. Max O/A W

2840-00-971-6287 Related Items NATO Stock Numbers Related to 2840-00-971-6287

2840-00-971-6287 Freight Data Freight Information 2840-00-971-6287

2840-00-971-6287 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 114990. A Sub NMFC of Z. It has a NMFC Description of BLADES BLAST/BLOWER WHEEL ETC. 2840-00-971-6287 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 2840-00-971-6287 is rated as a variable freight class when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 58952 which rates the freight between FCL and LCL. 2840-00-971-6287 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 593 for ocean manifesting and military sealift. 2840-00-971-6287 is not classified as a special type of cargo when transported by water. 2840-00-971-6287 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.