2835-01-682-1942

Turbine Engine Cooling Plate

2835016821942 016821942 3681059

An item of various cross sections used to exhaust heat from the gas generator turbine rotor of a turbine engine. View more Turbine Engine Cooling Plate

2835-01-682-1942 PLATE,COOLING,TURBINE ENGINE 2835016821942 016821942

Managed by United States
NSN Created on 26 Jul 2019
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2835-01-682-1942 PLATE,COOLING,TURBINE ENGINE 2835016821942 016821942 1/1
NSN 2835-01-682-1942 (Generic Image) 1/1

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2835-01-682-1942 Turbine Engine Cooling Plate 2835016821942
3681059 An item of various cross sections used to exhaust heat from the gas generator turbine rotor
United States (US) 4. 2835-01-682-1942 Marketplace Restrictions Approved Sources Datasheet Management
Updated Every Day 2835-01-682-1942 RQST NE Updated Every Day 2835-01-682-1942 RQST Updated Every Day

2835-01-682-1942 Demil Restrictions 2835-01-682-1942

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

2835-01-682-1942 is a Turbine Engine Cooling Plate 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.

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2835-01-682-1942 Manufacturers Approved Sources 2835-01-682-1942

Part Number
Manufacturer
Status
3681059
15434 - Cummins Inc. (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 3

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