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2835-01-371-8902
Nonaircraft Gas Turbine Engine Exhaust Cone
2835013718902 013718902 L21316P06
A conical shaped item designed to attach to the rear of an ENGINE, GAS TURBINE, NONAIRCRAFT. It is the inner portion of a DUCT AND CONE, EXHAUST, NONAIRCRAFT GAS TURBINE ENGINE. It may be attached directly to the engine. View more Nonaircraft Gas Turbine Engine Exhaust Cone
January 2023
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Nonaircraft Gas Turbine Engine Exhaust Cone www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-371-8902
Nonaircraft Gas Turbine Engine Exhaust Cone www.nsnlookup.com /fsg-28/fsc-2835/us 2835-01-371-8902
Nonaircraft Gas Turbine Engine Exhaust Cone Related to 2835-01-371-8902 2835-01-371-8903 /us 2835
Restrictions 2835-01-371-8902
2835-01-371-8902 is a Nonaircraft Gas Turbine Engine Exhaust Cone that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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 2835-01-371-8902
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2835-01-371-8902
- Spain (YB01)
- Effective Date:
- 1 Sep 2003
- Australia (ZA01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Dec 2005
Approved Sources 2835-01-371-8902
- Part Number
- Manufacturer
- Status
- L21316P06
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2835-01-371-8902
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- End Item Identification [AGAV]
- Ffg Guided Missile Frigate
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Freight Information 2835-01-371-8902
2835-01-371-8902 has freight characteristics managed by Australia.. 2835-01-371-8902 has a variance between NMFC and UFC when transported by rail and the description should be consulted.