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2950-01-459-8206

Non-Aircraft Engine Turbo Supercharger

2950014598206 014598206 1143600

A mechanism for forcing additional air and increasing pressure in the cylinders of a reciprocating engine to increase power produced by the engine. The air utilized may come from the exhaust of the engine. View more Non-Aircraft Engine Turbo Supercharger

2950-01-459-8206 TURBO SUPERCHARGER,ENGINE,NON-AIRCRAFT 2950014598206 014598206

Managed by United States
NSN Created on 15 Oct 1998
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
2950-01-459-8206 TURBO SUPERCHARGER,ENGINE,NON-AIRCRAFT 2950014598206 014598206 1/1
NSN 2950-01-459-8206 (Generic Image) 1/1

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2950-01-459-8206 Demil Restrictions 2950-01-459-8206

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

2950-01-459-8206 is a Non-Aircraft Engine Turbo Supercharger 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.

2950-01-459-8206 HTS and ScheduleB Import and Export 2950-01-459-8206

2950-01-459-8206 End Users End Users 2950-01-459-8206

Canada (ZC01)
Effective Date:
1 Oct 1998

2950-01-459-8206 Manufacturers Approved Sources 2950-01-459-8206

2950-01-459-8206 Technical Data Datasheet 2950-01-459-8206

Characteristic
Specifications
FIIG
T135-J
End Item Identification [AGAV]
Dive Tender Air Inlet And Exhaustsystem;Part Number 1131119

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2950-01-459-8206 Freight Data Freight Information 2950-01-459-8206

2950-01-459-8206 has freight characteristics managed by Canada.. 2950-01-459-8206 has a variance between NMFC and UFC when transported by rail and the description should be consulted.