2835-01-214-1071
Nonaircraft Gas Turbine Engine Combustion Chamber
2835012141071 012141071 623513 POSITION 2,6,8
The portion of a ENGINE, GAS TURBINE, NONAIRCRAFT in which fuel is burned. It may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case. View more Nonaircraft Gas Turbine Engine Combustion Chamber
November 2023
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United States (US) 4. 2835-01-214-1071 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2835-01-214-1071 RQST Updated Every Day 2835-01-214-1071 RQST NE Related Documents
2835012141071 012141071 browser . 2835-01-214-1071Nonaircraft Gas Turbine Engine Combustion Chamber2835012141071
012141071 623513 Restrictions 2840-21-856-9784 DEMIL: | DEMILI : | CRITICALITY : | HMIC : | PMIC : |
Restrictions 2835-01-214-1071
2835-01-214-1071 is a Nonaircraft Gas Turbine Engine Combustion Chamber 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. This item does not contain a precious metal.
Approved Sources 2835-01-214-1071
- Part Number
- Manufacturer
- Status
- 623513 POSITION 2,6,8
- Manufacturer
- 77445 - Rtx Corporation (Active)
- Primary Buy
- Primary Buy
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