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2840-00-610-2726
Aircraft Gas Turbine Engine Component Mounting Plate
2840006102726 006102726 619E249G1
A metallic item of various shapes designed to reduce vibration and to secure a component part of an ENGINE, GAS TURBINE, AIRCRAFT to the engine case or housing as modified. For mounting accessories to the outside of the engine, see PLATE, MOUNTING. View more Aircraft Gas Turbine Engine Component Mounting Plate
January 2023
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Related Documents 2840-00-610-2726 1+ Documents (More...)
United States (US) 4. 2840-00-610-2726 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-00-610-2726 RQST Updated Every Day 2840-00-610-2726 RQST NE Related
Restrictions 2840-00-610-2726
2840-00-610-2726 is a Aircraft Gas Turbine Engine Component Mounting Plate 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 considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-00-610-2726
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-00-610-2726
- Italy (ZR01)
- Effective Date:
- 1 Apr 1991
- Greece (ZU01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 2840-00-610-2726
- Part Number
- Manufacturer
- Status
- 619E249G1
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
- 619E249G1
- 24446 - General Electric Company (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 2840-00-610-2726
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- End Item Identification [AGAV]
- Acft Eng
- Criticality Code Justification [CRTL]
- Agav
- Engine Section Location [CZBJ]
- Compressor
- Material [MATT]
- Steel Overall
- Overall Length [ABHP]
- 6.880 Inches Minimum And 6.920 Inches Maximum
- Part Name Assigned By Controlling Agency [CXCY]
- Bleed Pad Connector
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Freight Information 2840-00-610-2726
2840-00-610-2726 has freight characteristics.. 2840-00-610-2726 has a variance between NMFC and UFC when transported by rail and the description should be consulted.
Packaging Data 2840-00-610-2726
- Responsible Activity
- Packaging Data Source
- Primary Inventory Control Activity (PICA)
- Packaging Data does not meet current MIL-STD-2073-1E
Item Pack Level (Unpackaged)
- Item Size
- Item Weight
- Characteristics
- Weight/Dimensions Category
- Fragility
- Item Preservation
- Item Weight
- --
- --
- --
- --
- --
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- --
- --
- --
- --
- Physical Protection
- Any Suitable Process
- --
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- No Requirement
- MIL-PRF-121, Greaseproof, Waterproof Barrier
- A-A-1898, Grade II, Water Resistant Cellulosic Cushioning
- --
- ASTM-D5118, Type CF, Class Domestic, Corrugated Fiberboard Box
- --
- MIL-PRF-121, Greaseproof, Waterproof Barrier
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- ASTM-D5118, Type CF, Class Domestic, Corrugated Fiberboard Box