Premium Information is available for this item - Upgrade for $1 a day
2840-01-205-1302
Aircraft Gas Turbine Engine Compressor Shroud
2840012051302 012051302 4060645
Managed by United States
NSN Created on 4 Apr 1985
Data Last Changed
May 2023
May 2023
NATO Update Count
20
20
NATO Data Quality
Marketplace 2840-01-205-1302
Need Help?
Request a Quotation from participating marketplace vendors
Request a Quotation from participating marketplace vendors
Related Documents 2840-01-205-1302 5+ Documents (More...)
Documents 2840-01-429-6321 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-205-1302
2840012051302 012051302,4060645 2840-01-205-1302 2840012051302 012051302 SHROUD,COMPRESSOR,AIRCRAFT
2840012051302 012051302,4060645 2840-01-205-1302 2840012051302 012051302 SHROUD,COMPRESSOR,AIRCRAFT
2840-00-345-3657 2840003453657 003453657 is an item within a case, compressor, aircraft gas turbine engine, designed to surround or partially surround a rotor, compressor, aircraft gas turbine engine. it's primary purpose is to protect other components of the engine in the event of an impeller or rotor break up.
Aircraft Gas Turbine Engine Turbine Nozzle Support 9526M11G03RNCC: 5 | RNVC: 2 | DAC: 5 4 Dec 1985 2840-01-205-1302
5340-14-406-0645 5340144060645 144060645 is a rigid item usually fabricated from flat material, forming two alternate or two adjacent interior angles, both which are less than 180 degrees (3.141 radians). it is designed to position, align, and/or support an item. it may be reinforced. see also bracket, angle and bracket (1), mounting.
5325-00-406-0645 5325004060645 004060645 is a cylindrical item which may have wrenching and/or driving facilities and/or shoulders. it is designed to be inserted in a drilled, tapped or a pretapped hole, or molded or pressed into soft material to reduce the size of a tapped hole; to provide threads; to add strength, and/or to prevent stripping. it is one of the following: (1) a one-piece, flanged or unflanged, internally threaded item which may have external threads, and/or serrations around the periphery of the collar, designed to engage a serrated lock ring which is not included with the item; (2) a one-piece precision coiled wire; (3) a two-piece item consisting of an internally threaded cylinder and a mating externally threaded part; or (4) a one-piece internally threaded item whose outside diameter is tapered and/or knurled and/or with fin(s). the internal thread of the item may have a locking feature. excludes items having a sleeve on on its under portion which can be clinched or crimped. excludes bushing,machine thread; nut,plain,knurled; nut,plain,round; nut,plain,clinch and nut,self-locking,clinch. see also nut,plain,plate
Restrictions 2840-01-205-1302
IUID Required
2840-01-205-1302 is a Aircraft Gas Turbine Engine Compressor Shroud that is an aviation critical safety item or flight safety critical aircraft part. 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. This item does not contain a precious metal.
Import and Export 2840-01-205-1302
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-205-1302
- US Air Force (FXX4)
- Effective Date:
- 1 Sep 2000
- Former MOE Rule:
- FEE4
- Belgium (ZB01)
- Effective Date:
- 1 Mar 2005
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1991
- Netherlands (ZN01)
- Effective Date:
- 1 Apr 1991
- Portugal (ZP01)
- Effective Date:
- 1 Nov 1997
- Denmark (ZS01)
- Effective Date:
- 1 Jan 2006
- Norway (ZT01)
- Effective Date:
- 1 Apr 1996
Approved Sources 2840-01-205-1302
- Part Number
- Manufacturer
- Status
- 4060645
- Manufacturer
- 9Y765 - Numet Machining Techniques, Llc (Active)
- Primary Buy
- Primary Buy
- 4060645
- 77445 - Rtx Corporation (Active)
- Secondary Buy
- Secondary Buy
Datasheet 2840-01-205-1302
- Characteristic
- Specifications
- FIIG
- Specifications
- A23900
- End Item Identification [AGAV]
- Acft Eng F100-Pw-220
- Criticality Code Justification [CRTL]
- Adav And Feat
- Overall Diameter [ADAV]
- 16.908 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Original Name Case,Combustion Chamber,Acft Gte
- Special Features [FEAT]
- T.O. 2J-F100-24, Fig 144, Ind 21;5Th Stage Disk And Blades, Case And Stators
Management Data 2840-01-205-1302
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2022
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2021
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2020
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- Oct 2019
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- MOE
- USC
- Code
- Statement
- Order of Use
- Jump To Code
- Qty Per Assy
- UOM
- Technical Document
- Quantative Expression
- Code
- Department of the Air Force (DF)
- L
- 7
- Substitute For 2840-00-345-3657
- AAA
- 7
- Department of the Air Force (DF)
- L
- G
- Replaces 2840-01-429-6321
- ABA
- G
- Department of the Air Force (DF)
- L
- R
- Refer To Net Price 2161.38
- NET PRICE 2161.38
- R
- Department of the Air Force (DF)
- L
- Dod I&S Family Master Nsn - - -
- ABB
Air Force
- Fund:
- RO
- Major Repair
- Budget:
- 8
- 97X4830.FCL4 - Materiel Support DIV (MSD) - Materiel Support Division (MSD), which includes those Air Force Centrally Managed Investment Items (ERRC XD1=C and XD2=T) except for those still managed in budget programs (BP) 15, 25, 82, 83, and 84 as stock fund exempt. MSD also includes items centrally procured and managed as Expense Items (ERRC XB3=N and XF3=P). Reference AFMAN 23–110, Volume 1, Part 3, Chapter 7, Paragraph 7.3.1
- Aggregation Code:
- NZ
- PRATT & WHITNEY JET ENGINES & COMPONENTS, F-100–P-100
- Price Validation Code:
- V
- The current standard price has been validated.
The item has been analyzed in conjunction with the Zero Overpricing Program and is in the accepted price range.
The item was procured under open competition and under the competitive arena the price is considered fair and reasonable.
ZOP or Standard price challenges are permissible but must be supported by adequate justification.
- Expendability
Recoverability
Repairability: - T
- Expendable. Reparable. Condemn at Depot. AF Recoverable Assembly Management System (AFRAMS).
NATO Stock Numbers Related to 2840-01-205-1302
2510-15-209-3009 2520-99-446-6108 6220-15-204-1528 9999-37-515-0085 5310-15-139-2426 9915-15-219-4601 1730-25-105-4112 1220-14-266-0252 4030-15-175-3668 6685-14-380-3542 1560-99-601-1385 1680-99-600-3219 1005-13-103-5661 2540-15-138-4766 4920-14-441-3681 5340-14-436-9248 2910-12-148-8383 5820-15-138-1601
Freight Information 2840-01-205-1302
2840-01-205-1302 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 114215. A Sub NMFC of Z. It has a NMFC Description of ASSEMBLIES JET AIRCRAFT ENGINE. 2840-01-205-1302 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. 2840-01-205-1302 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 671 for ocean manifesting and military sealift. 2840-01-205-1302 is not classified as a special type of cargo when transported by water. 2840-01-205-1302 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.
Packaging Data 2840-01-205-1302
- Responsible Activity
- Packaging Data Source
- Primary Inventory Control Activity (PICA)
- --
Item Pack Level (Unpackaged)
- Item Size
- Item Weight
- Characteristics
- Weight/Dimensions Category
- Fragility
- Item Preservation
- Item Weight
- 17.0" H x 17.0" W x 1.7" L
- --
- --
- Over 10lb
- Less than 85G
- No Requirement
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- 1
- 20.5" H x 20.5" W x 6.5" L
- --
- --
- Physical Protection
- Any Suitable Process
- 20.5" H x 20.5" W x 6.5" L
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- No Requirement
- MIL-DTL-17667, Neutral Wrapping Paper
- PPP-C-795, Cellular Plastic Film Cushioning; or A-A-3129, Open Cell Plastic Cushioning; or PPP-C-1797, Polypropylene Foam Cushioning; or A-A-59136, Polyethylene Foam Cushioning
- 1/2 inch thick
- ASTM-D5118, Type CF, Class Weather-Resistant, Corrugated Fiberboard Box
- Reusable container
- MIL-DTL-17667, Neutral Wrapping Paper
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --
- No Requirement