Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components - Canada (CA)
Federal Supply Class (FSC): 2840
NATO Supply Classification Class (NSC): 2840
Federal Supply Group (FSG): 28 Engines, Turbines, and Components
NATO Supply Classification Group (NSG): 28 Engines, Turbines, and Components
Items Managed by Canada (CA) - NCB is 20 or 21
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NSN Format for Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Codified by Canada
| 28 | 40 | 21 | XXX | XXXX | |||
|---|---|---|---|---|---|---|---|
| Group FSG | Class | NCB | Identifier | ||||
| FSC Federal Supply Class | NIIN | ||||||
| NSN | |||||||
NATO Supply Class 2840 is a classification used by the North Atlantic Treaty Organization (NATO) to categorize gas turbines and jet engines, specifically those used in aircraft as prime movers. This class also includes the components associated with these engines.
The purpose of this classification is to provide a standardized system for the identification and categorization of military equipment and supplies. By organizing items into specific classes and groups, NATO aims to facilitate logistics, procurement, and interoperability among member nations.
Gas turbines and jet engines in this class are typically used to power aircraft, providing the necessary thrust for propulsion. These engines are designed to operate under high temperatures and pressures, and they are crucial for the performance and efficiency of military aircraft.
Components included in this class can vary but generally encompass parts and accessories that are directly related to gas turbines and jet engines. This may include items such as fuel systems, exhaust systems, air intake systems, combustion chambers, and engine controls.
NATO Supply Class 2840 falls under NATO Supply Group 28, which is dedicated to engines, turbines, and their components. This group encompasses a wide range of equipment used in military applications, including land, sea, and air vehicles.
Overall, NATO Supply Class 2840 plays a vital role in the standardization and organization of gas turbines and jet engines used in military aircraft, ensuring efficient logistics and interoperability among NATO member nations.
Includes Compressor and Turbine Rotors; Blades; Combustion Chamber; Accessory Gear Box; Afterburner; Exhaust Cone; Reservoirs, Hydraulic; Tank, Oil.
Excludes Oil, Air, Anti-icing, and Hydraulic Regulators, Valves, and Pumps specially designed for Gas Turbines and Jet Engines (FSC 2995); Control Assemblies, Push-Pull (FSC 2995); Engine Mounted Control Assemblies (FSC 2995); Fuel System Components (FSC 2915); Engine Electrical System Components (FSC 2925); Engine Cooling System Components (FSC 2935); Engine Air/Oil Cleaner/Filter/Strainers (FSC 2945).
Frequently Asked Questions(FAQ) for Federal Supply Class 2840
- What is Federal Supply Class 2840?
- FSC 2840 is the Federal Supply Class (formally known as NATO Supply Classification Class NSC 2840) in the USA for supply items codified in the category of Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components.
- What is NATO Supply Classification Class 2840?
- NSC 2840 is the NATO Supply Classification Class (also known as Federal Supply Class FSC 2840 in the USA) for supply items codified in the category of Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components.
- Which Federal Supply Group is FSC 2840 in?
- FSC 2840 is in Federal Supply Group (FSG) 28 which contains Engines, Turbines, and Components.
- Which NATO Supply Classification Group is NSC 2840 in?
- NSC 2840 is in NATO Supply Classification Group (NSG) 28 which contains Engines, Turbines, and Components.
Supply Items Included in Federal Supply Class 2840
- What is a Turbo-Jet Engine? 11 Items
- A Turbo-Jet Engine (ENGINE,TURBO-JET) is a continuous-combustion type power unit, may be with or without container, designed to exert thrust. It's prime physical characteristics include air compressor(s), combustion chamber(s) and gas turbine. The operating principle is as follows: atmospheric air is inducted into the unit at its front, compressed, heated by combustion of a fuel, expanded through the gas turbine, and ejected at high velocity. It may incorporate features to vary direction of the thrust.
- What is a Turbo-Prop Aircraft Engine? 21 Items
- A Turbo-Prop Aircraft Engine (ENGINE,AIRCRAFT,TURBO-PROP) is a combustion type power unit, may be with or without container, designed to use superheated air to spin a turbine rotor attached to the propeller shaft through reduction gears.
- What is a Turbo-Shaft Aircraft Engine? 14 Items
- A Turbo-Shaft Aircraft Engine (ENGINE,AIRCRAFT,TURBO-SHAFT) is a continuous-combustion type engine, may be with or without container, designed to use superheated air to drive a turbine rotor which is connected to the rotorshaft of a helicopter by way of reduction gears.
- What is a Turbine Engine Bleed Valve? 38 Items
- A Turbine Engine Bleed Valve (VALVE,BLEED,TURBINE ENGINE) is an item which is a component of a turbine engine with multistage compressors and which reduces and neutralizes the pressure surges resulting from differing operating conditions thus preventing surging.
- What is an Aircraft Gas Turbine Engine Combustion Chamber? 21 Items
- An Aircraft Gas Turbine Engine Combustion Chamber (CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE) is the portion of an ENGINE, GAS TURBINE, AIRCRAFT 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.
- What is an Aircraft Gas Turbine Engine Exhaust Duct? 13 Items
- An Aircraft Gas Turbine Engine Exhaust Duct (DUCT,EXHAUST,AIRCRAFT GAS TURBINE ENGINE) is a cylindrical shaped item designed to direct the hot gases that are discharged from an ENGINE, GAS TURBINE, AIRCRAFT. It is the outer portion of a DUCT AND CONE, EXHAUST, AIRCRAFT GAS TURBINE ENGINE. It may be attached directly to the engine.
- What is an Aircraft Gas Turbine Engine Combustion Chamber Liner? 28 Items
- An Aircraft Gas Turbine Engine Combustion Chamber Liner (LINER,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE) is a cylindrical shaped item positioned inside the CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. It is designed to direct the flow of hot gasses to the TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE.
- What is an Aircraft Gas Turbine Engine Lubricating Nozzle? 13 Items
- An Aircraft Gas Turbine Engine Lubricating Nozzle (NOZZLE,LUBRICATING,AIRCRAFT GAS TURBINE ENGINE) is an item designed to direct and control a mist, spray, or stream of lubricating oil inside an ENGINE, GAS TURBINE, AIRCRAFT.
- What is an Aircraft Gas Turbine Engine Heat Shield? 16 Items
- An Aircraft Gas Turbine Engine Heat Shield (SHIELD,HEAT,AIRCRAFT GAS TURBINE ENGINE) is a rigid item, fabricated from a heat resistant allow, with or without insulation material added. Designed to protect parts, areas or systems of an ENGINE, GAS TURBINE, AIRCRAFT from excessive heat damage. See also INSULATION BLANKET, THERMAL, AIRCRAFT GAS TURBINE ENGINE.
- What is an Aircraft Gas Turbine Engine Modification Kit? 15 Items
- An Aircraft Gas Turbine Engine Modification Kit (MODIFICATION KIT,GAS TURBINE ENGINE,AIRCRAFT) is a modification kit designed to be used on an ENGINE, GAS TURBINE, AIRCRAFT.
- What is an Aircraft Gas Turbine Engine Compressor Blade? 43 Items
- An Aircraft Gas Turbine Engine Compressor Blade (BLADE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE) is an item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT.
- What is an Aircraft Gas Turbine Engine Fan Blade? 18 Items
- An Aircraft Gas Turbine Engine Fan Blade (BLADE,FAN,AIRCRAFT GAS TURBINE ENGINE) is an item mounted on a DISK, FAN, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the fan section of a ENGINE, GAS TURBINE, AIRCRAFT.
- What is an Aircraft Gas Turbine Engine Turbine Rotor Blade? 37 Items
- An Aircraft Gas Turbine Engine Turbine Rotor Blade (BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE) is an item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT.
- What is an Aircraft Gas Turbine Engine Turbine Case And Nozzle Assembly? 12 Items
- An Aircraft Gas Turbine Engine Turbine Case And Nozzle Assembly (CASE AND NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE) is a NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE with a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE.
- What is an Aircraft Gas Turbine Engine Turbine Case? 16 Items
- An Aircraft Gas Turbine Engine Turbine Case (CASE,TURBINE,AIRCRAFT GAS TURBINE ENGINE) is a case that is an integral part of an ENGINE, GAS TURBINE, AIRCRAFT, designed to surround and protect a NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
- What is an Aircraft Gas Turbine Engine Compressor? 19 Items
- An Aircraft Gas Turbine Engine Compressor (COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE) is a single or multistage item designed to receive, compress, and deliver air to the combustion area at a required pressure and velocity. It consists of a CASE (3) AND VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
- What is an Aircraft Gas Turbine Engine Turbine Disk? 13 Items
- An Aircraft Gas Turbine Engine Turbine Disk (DISK,TURBINE,AIRCRAFT GAS TURBINE ENGINE) is an item having provisions on the outer periphery for attaching a designated number of BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
- What is an Aircraft Gas Turbine Engine Thermal Insulation Blanket? 35 Items
- An Aircraft Gas Turbine Engine Thermal Insulation Blanket (INSULATION BLANKET,THERMAL,AIRCRAFT GAS TURBINE ENGINE) is a flexible covering, fabricated from appropriate insulating materials, designed to reduce thermal radiation in the hot section of an ENGINE, GAS TURBINE, AIRCRAFT. See also SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE.
- What is an Aircraft Gas Turbine Engine Turbine Nozzle Assembly? 10 Items
- An Aircraft Gas Turbine Engine Turbine Nozzle Assembly (NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE) is a stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle.
- What is an Aircraft Gas Turbine Engine Turbine Nozzle? 33 Items
- An Aircraft Gas Turbine Engine Turbine Nozzle (NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE) is a single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud.
- What is an Aircraft Gas Turbine Engine Compressor Rotor? 10 Items
- An Aircraft Gas Turbine Engine Compressor Rotor (ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE) is a single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
- What is an Aircraft Gas Turbine Engine Turbine Rotor? 30 Items
- An Aircraft Gas Turbine Engine Turbine Rotor (ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE) 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.
- What is an Aircraft Gas Turbine Engine Air Seal? 20 Items
- An Aircraft Gas Turbine Engine Air Seal (SEAL,AIR,AIRCRAFT GAS TURBINE ENGINE) is a rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an ENGINE, GAS TURBINE, AIRCRAFT. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.
- What is an Aircraft Gas Turbine Engine Metallic Seal? 15 Items
- An Aircraft Gas Turbine Engine Metallic Seal (SEAL,METALLIC,AIRCRAFT GAS TURBINE ENGINE) is a single or multi-piece item of metallic construction, specifically designed to form either a tight fuel or oil seal in an ENGINE, GAS TURBINE, AIRCRAFT.
- What is an Aircraft Gas Turbine Engine Turbine Shaft? 16 Items
- An Aircraft Gas Turbine Engine Turbine Shaft (SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE) is an item designed to transfer rotary motion from a ROTARY, TURBINE, AIRCRAFT GAS TURBINE ENGINE to a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE. It may include the HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may include provisions for mounting bearings and/or seals.
- What is an Aircraft Gas Turbine Engine Turbine Shroud Segment? 51 Items
- An Aircraft Gas Turbine Engine Turbine Shroud Segment (SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE) is a stationary arched metal segment used to establish clearance and a seal for the tip of a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. The inner dimension may have open honeycomb or composition filled surface or may be formed by the knife edge metal protrusions of a SEAL RING, LABYRINTH, AIRCRAFT GAS TURBINE ENGINE.
- What is an Aircraft Gas Turbine Engine Compressor Vane? 28 Items
- An Aircraft Gas Turbine Engine Compressor Vane (VANE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE) is a component of a VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.
- What is an Aircraft Gas Turbine Engine Seal Housing? 17 Items
- An Aircraft Gas Turbine Engine Seal Housing (HOUSING,SEAL,AIRCRAFT GAS TURBINE ENGINE) is a housing designed to surround, retain, support and protect a seal used in an ENGINE, GAS TURBINE, AIRCRAFT.
- What is a Turbine Engine Accessory Drive Gearbox? 33 Items
- A Turbine Engine Accessory Drive Gearbox (GEARBOX,ACCESSORY DRIVE,TURBINE ENGINE) is a complete assembly of gears, bearings, shafts, seals, and necessary miscellaneous parts, encased in a housing, designed for driving and/or attaching various aircraft or engine accessories and components.