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2530-01-246-4454

Brake Backing Plate

2530012464454 012464454 E4TZ-2211-B 3207917

A rigid circular shaped metal item with a centrally located aperture. It has mounting holes and is specifically designed to mount and position the components of a BRAKE (as modified). It also serves to prevent dirt and other foreign matter from entering the braking mechanism. Excludes items which are used as a dust shield only. View more Brake Backing Plate

2530-01-246-4454 PLATE,BACKING,BRAKE 2530012464454 012464454

Managed by United States
NSN Created on 13 Dec 1986
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
2530-01-246-4454 PLATE,BACKING,BRAKE 2530012464454 012464454 1/1
NSN 2530-01-246-4454 (Generic Image) 1/1

2530-01-246-4454 Stock and Availability Marketplace 2530-01-246-4454

2530-01-246-4454 Related Documents Related Documents 2530-01-246-4454 5+ Documents (More...)

May 1987 2530-01-246-4453 Brake Backing Plate 3207916RNCC: 5 | RNVC: 9 | DAC: 6 13 Dec 1986 2530-01-246-4454
2840-14-430-8967 2840144308967 144308967 is a single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. it consists of disks, blades, hubs, and the like. it is the moving part of a turbine assembly, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
2840-14-574-1225 2840145741225 145741225 is a single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. it consists of disks, blades, hubs, and the like. it is the moving part of a turbine assembly, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
2840-14-406-6492 2840144066492 144066492 is a single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. it consists of disks, blades, hubs, and the like. it is the moving part of a turbine assembly, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.

2530-01-246-4454 Demil Restrictions 2530-01-246-4454

DEMIL: A | DEMILI: | CRITICALITY: X | HMIC: P | PMIC: A | EDC: | ADPEC:

2530-01-246-4454 is a Brake Backing Plate 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 may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.

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