Premium Information is available for this item - Upgrade for $1 a day
2915-01-529-9144
Aircraft Engine Tube Assembly
2915015299144 015299144 5074T65G01
An aircraft engine component designed to convey fluid. It may be bent or straight, flexible or rigid. It may include fittings to join one or more tubes together. For tube assembly designed to convey fuel from the cell or tank to the engine, see: FUEL LINE,AIRCRAFT. View more Aircraft Engine Tube Assembly
January 2023
2
Marketplace 2915-01-529-9144
Request a Quotation from participating marketplace vendors
Related Documents 2915-01-529-9144 2+ Documents (More...)
Restrictions 2915-01-529-9144
2915-01-529-9144 is a Aircraft Engine Tube Assembly 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. This item does not contain a precious metal.
Import and Export 2915-01-529-9144
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2915-01-529-9144
- Spain (YB01)
- Effective Date:
- 1 May 2005
- Malaysia (YW01)
- Effective Date:
- 1 Sep 2008
Approved Sources 2915-01-529-9144
- Part Number
- Manufacturer
- Status
- 5074T65G01
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2915-01-529-9144
- Characteristic
- Specifications
- FIIG
- Specifications
- A11700
- End Item Identification [AGAV]
- Ct7-9 Turboprop Engine For Cn-235 Transport Aircraft
NATO Stock Numbers Related to 2915-01-529-9144
Freight Information 2915-01-529-9144
2915-01-529-9144 has freight characteristics.. 2915-01-529-9144 has a variance between NMFC and UFC when transported by rail and the description should be consulted.