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2840-01-448-7540
Aircraft Gas Turbine Engine Turbine Case
2840014487540 014487540 4083210
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. View more Aircraft Gas Turbine Engine Turbine Case
Managed by United States
NSN Created on 9 Sep 1997
Data Last Changed
May 2023
May 2023
NATO Update Count
8
8
NATO Data Quality
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Related Documents 2840-01-448-7540 5+ Documents (More...)
Aircraft Gas Turbine Engine Turbine Component Support 4084713RNCC: 5 | RNVC: 2 | DAC: 5 11 Jul 1997 2840-01-448-7540
3040-01-408-3210 3040014083210 014083210 is a cylinder designed to house a piston and other necessary component parts of a cylinder assembly, actuating, linear. do not use if a more specific name applies.
2805-99-408-3210 2805994083210 994083210
5999-14-408-3210 5999144083210 144083210 is a grouping of two or more physically connected or related electrical an/or electronic parts capable of dissassemblage. each component of the assemblage must be capable of functioning in accordance with its own item name. consists of a single printed circuit board or terminal board upon which are mounted separately manufactured electronic components such as capacitors, inductors, resistors, and the like. it may also include printed electronic components. the item is generally part of a subassembly and cannot be assigned a more definite item name. for items having a complete individual electrical/electronic function, use applicable item name such as amplifier (as modified); power supply; or the like. for items not having a complete individual electrical/electronic function, see applicable subassembly name, such as amplifier subassembly; power supply subassembly; or the like. for an assembly of electrical/electronic components mounted on other than a single printed wiring board, see electronic components assembly. excludes printed circuit boar
5950 Aircraft Gas Turbine Engine Turbine Case 6071T54G02RNCC: 3 | RNVC: 2 | DAC: 1 29 Jul 1991 2840-01-448-7540
Restrictions 2840-01-448-7540
IUID Required
2840-01-448-7540 is a Aircraft Gas Turbine Engine Turbine Case 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 2840-01-448-7540
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-448-7540
- US Air Force (FXX4)
- Effective Date:
- 1 Sep 2000
- Former MOE Rule:
- FEE4
- Singapore (YJ01)
- Effective Date:
- 1 Sep 2003
- Republic of Korea (ZH01)
- Effective Date:
- 1 Oct 2012
Approved Sources 2840-01-448-7540
- Part Number
- Manufacturer
- Status
- 4083210
- Manufacturer
- 77445 - Rtx Corporation (Active)
- Primary Buy
- Primary Buy
- 4083210
- 9Y765 - Numet Machining Techniques, Llc (Active)
- Secondary Buy
- Secondary Buy
- 4083210
- 1645F - Hanwha Aerospace Co., Ltd (Active)
- NATO Reproduction
- NATO Reproduction
Datasheet 2840-01-448-7540
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- F100-Pw-229 Aircraft Gas Turbine Engine
- Criticality Code Justification [CRTL]
- Czbj And Abmz And Abhp And Feat
- Design Type [APGF]
- Axial Compressor
- Diameter [ABMZ]
- 28.330 Inches Minimum And 28.350 Inches Maximum
- Engine Section Location [CZBJ]
- Turbine
- Material Document And Classification [MDCL]
- Pwa1010 Mfr Ref Single Material Response Overall
- Material [MATT]
- Nickel Alloy Overall
- Overall Length [ABHP]
- 5.809 Inches Minimum And 5.813 Inches Maximum
- Special Features [FEAT]
- Nt.O. 2J-F100-54, Fig 89, Ind 71; Use Only On P/N 4084522-800, -801, -802, 4082654-803, And 4082657-808; Location Near No. 4 Bearing Front Air Sealing Ring, Front Seal Assy, Compressor Exit Stator And Diffuser Case
Management Data 2840-01-448-7540
- 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
- R
- Refer To Net Price 6862.98
- NET PRICE 6862.98
- R
Air Force
- Fund:
- SF
- Stock fund applicable to items managed for the Air Force by the respective Inventory Control Point
- 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 2840-01-448-7540
2840-99-562-5828 2840-14-409-7555 2840-14-349-4214 2840-14-527-8784 2840-14-345-1112 2840-14-340-9505 2840-20-000-0123 2840-14-421-7157 2840-14-373-2982 2840-14-484-7982 2840-14-378-8330 2840-14-313-2585 2840-14-392-5517 2840-14-348-8818 2840-14-399-2874 2840-14-345-1139 2840-14-385-3836 2840-66-133-3009
Freight Information 2840-01-448-7540
2840-01-448-7540 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 120780. A Sub NMFC of C. It has a NMFC Description of ENGINE PARTS USED SUB3. 2840-01-448-7540 is rated as class 70 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 08134 which rates the freight between FCL and LCL. 2840-01-448-7540 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. 2840-01-448-7540 is not classified as a special type of cargo when transported by water. 2840-01-448-7540 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 2840-01-448-7540
- 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
- 28.4" H x 28.4" W x 5.3" 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
- 33.1" H x 33.1" W x 6.9" L
- --
- --
- --
- Special Requirements
- 33.1" H x 33.1" W x 6.9" L
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- No Requirement
- Special Requirements – see Specific Instructions or Drawings provided
- Special Requirements. See Specific Instructions or Drawings Provided
- Special Requirements. See Specific Instructions or Drawings Provided
- Special requirement – See specific instructions or drawings provided
- Special requirements
- Special Requirements – see Specific Instructions or Drawings provided
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --
- No Requirement