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2840-00-111-1018
Aircraft Gas Turbine Engine Air Seal
2840001111018 001111018 9686M18P07
A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an ENGINE, GAS TURBINE, AIRCRAFT. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal. View more Aircraft Gas Turbine Engine Air Seal
January 2023
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Aircraft Gas Turbine Engine Air Seal United States (US) 4. 2840-00-111-1018 Marketplace Restrictions
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Restrictions 2840-00-111-1018
2840-00-111-1018 is a Aircraft Gas Turbine Engine Air Seal that does not have a nuclear hardened feature or any other critical feature 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. The precious metals content of this item is unknown.
Import and Export 2840-00-111-1018
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-00-111-1018
- Australia (ZA01)
- Effective Date:
- 1 Apr 1991
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
- Italy (ZR01)
- Effective Date:
- 1 Jul 1997
Approved Sources 2840-00-111-1018
- Part Number
- Manufacturer
- Status
- 9686M18P07
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-00-111-1018
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Acft Eng Tf-39
- Engine Section Location [CZBJ]
- High Pressure Turbine
- Material Thickness [ABPX]
- 0.004 Inches Minimum And 0.007 Inches Maximum
- Material [MATT]
- Nickel Alloy Overall
- Material Document And Classification [MDCL]
- Ams5536 Assn Std Single Material Response Overall
- Overall Length [ABHP]
- 1.240 Inches Minimum And 1.260 Inches Maximum
- Overall Width [ABMK]
- 0.245 Inches Minimum And 0.255 Inches Maximum
- Special Features [FEAT]
- T.O. 2J-Tf39-4; Turbine Nozzle
- Stage Number [CZCJ]
- 2
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Freight Information 2840-00-111-1018
2840-00-111-1018 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 194120. A Sub NMFC of H. It has a NMFC Description of WASHERS/GASKETS/PCKG DVCS NOI SUB8. 2840-00-111-1018 is rated as class 85 when transported by Less-Than Truckload (LTL) freight. 2840-00-111-1018 is rated as class 100 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 95100 which rates the freight between FCL and LCL. It has a Water Commodity Code (WCC) of 671 for ocean manifesting and military sealift. 2840-00-111-1018 is not classified as a special type of cargo when transported by water. 2840-00-111-1018 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.