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2840-01-167-2923
Aircraft Gas Turbine Engine Fan Case
2840011672923 011672923 9397M40G01 9397M40
A case that is an integral part of an ENGINE, GAS TURBINE, AIRCRAFT, designed to surround and protect a FAN, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Fan Case
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Related Documents 2840-01-167-2923 5+ Documents (More...)
United States (US) 4. 2840-01-167-2923 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-167-2923 RQST Updated Every Day 2840-01-167-2923 RQST NE Related Documents
537L915 9397M40G02 537L915G04 537L915G03 9684M50G13 537L915G05 9684M50 9397M40 1288M61 A case that is
Aircraft Gas Turbine Engine Fan Case 9397M40 A case that is an integral part of an ENGINE, GAS
9397M40G01 9397M40 537L915G04 537L915G03 9684M50G13 537L915G05 9684M50 9397M40 1288M61 A case that is
537L915 9397M40G02 537L915G04 537L915G03 9684M50G13 537L915G05 9684M50 9397M40 1288M61 A case that is
537L915 9397M40G02 537L915G04537L915G03 9684M50G13 537L915G05 9684M50 9397M40 1288M61 A case that is
9397M40G01 319-7015 Aircraft Gas Turbine Engine Fan Case Fan Case2840013197015 013197015 1288M61G04
537L915 9397M40G02 537L915G04 537L915G03 9684M50G13 537L915G05 9684M50 9397M40 1288M61 A case that is
Restrictions 2840-01-167-2923
IUID Required
2840-01-167-2923 is a Aircraft Gas Turbine Engine Fan Case that does not have a nuclear hardened feature, but does have another critical feature or features 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. This item does not contain a precious metal.
Import and Export 2840-01-167-2923
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-167-2923
- US Air Force (FXX4)
- Effective Date:
- 1 Sep 2000
- Former MOE Rule:
- FEE4
Approved Sources 2840-01-167-2923
- Part Number
- Manufacturer
- Status
- 9397M40G01
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
- 9397M40
- 07482 - General Electric Company (Active)
- Informational Drawing
- Informational Drawing
Datasheet 2840-01-167-2923
- Characteristic
- Specifications
- End Item Identification [AGAV]
- Specifications
- Acft Eng Tf39
- Criticality Code Justification [CRTL]
- Agav
- Design Type [APGF]
- Axial Compressor
- Diameter [ABMZ]
- 95.930 Inches Minimum And 95.950 Inches Maximum
- Engine Section Location [CZBJ]
- Fan
- Material [MATT]
- Aluminum Alloy Overall
- Material Document And Classification [MDCL]
- Ams4150 Assn Std Single Material Response Overall
- Reference Data And Literature [RDAL]
- T.O. 2J-Tf39-4, Fig 38, Ind 3
- Special Features [FEAT]
- 2Nd Stage; 1 Piece Extruded Case Replaced P/N 1288M61g01 And Reworked To P/N 9397M40g02
- Overall Length [ABHP]
- 23.433 Inches Minimum And 23.453 Inches Maximum
- Part Name Assigned By Controlling Agency [CXCY]
- Original Name Case And Nozzle Assembly,Turbine,Aircraft
NATO Stock Numbers Related to 2840-01-167-2923
Freight Information 2840-01-167-2923
2840-01-167-2923 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 133300. A Sub NMFC of Z. It has a NMFC Description of MACHINERY/MACHINES NOI. 2840-01-167-2923 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. 2840-01-167-2923 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. 2840-01-167-2923 is not classified as a special type of cargo when transported by water. 2840-01-167-2923 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.