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2840-01-445-2811
Aircraft Gas Turbine Engine Turbine Rotor Blade
2840014452811 014452811 4085104
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
January 2023
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United States (US) 4. 2840-01-445-2811 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 2840-01-445-2811
2840-01-445-2811 is a Aircraft Gas Turbine Engine Turbine Rotor Blade that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 2840-01-445-2811
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-445-2811
- Republic of Korea (ZH01)
- Effective Date:
- 1 Aug 1998
- Netherlands (ZN01)
- Effective Date:
- 1 Sep 1997
- Denmark (ZS01)
- Effective Date:
- 1 Jan 1998
Approved Sources 2840-01-445-2811
- Part Number
- Manufacturer
- Status
- 4085104
- Manufacturer
- 77445 - Rtx Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-445-2811
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- F100-Pw-100 Aircraft Gas Turbine Engine
- Blade Attachment Method [BGLW]
- Fir Tree
- Criticality Code Justification [CRTL]
- Feat And Abmz And Abhp And Czbj
- Design Type [APGF]
- Axial Compressor
- Diameter [ABMZ]
- 29.004 Inches Minimum And 29.404 Inches Maximum
- Engine Section Location [CZBJ]
- Turbine
- Hardness Rating [CQFM]
- 45.0 Rockwell C Minimum Overall And 55.0 Rockwell C Maximum Overall
- Material Document And Classification [MDCL]
- Pwa658 Mfr Ref Single Material Response Overall
- Material [MATT]
- Nickel Alloy Overall
- Overall Length [ABHP]
- 6.771 Inches Minimum And 6.781 Inches Maximum
- Special Features [FEAT]
- T.O. 2J-F100-14, Fig 130, Ind 9; Interim Blade Replaces P/N 4067004 And Is Replaced By P/N 4084804 Per Ecp 95-Na027
- Stage Number [CZCJ]
- 4
NATO Stock Numbers Related to 2840-01-445-2811
Freight Information 2840-01-445-2811
2840-01-445-2811 has freight characteristics.. 2840-01-445-2811 has a variance between NMFC and UFC when transported by rail and the description should be consulted.
Packaging Data 2840-01-445-2811
- 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
- --
- --
- --
- Over 10lb
- Less than 85G
- Special Requirement
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- --
- 6.3" H x 6.3" W x 10.5" L
- --
- --
- Physical Protection
- Any Suitable Process
- 6.3" H x 6.3" W x 10.5" L
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- No Requirement
- --
- --
- --
- PPP-B-1672, Type II, Folding Convoluted Cushioning in Reusable Box
- No special marking
- --
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- ASTM-D5118, Type CF, Class Domestic, Corrugated Fiberboard Box