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

Page 11 of 15

NSN Format for Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Codified by Canada

284021XXXXXXX
Group
FSG
ClassNCBIdentifier
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.

FSC 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components - Canada (CA)
FSC 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components - Canada (CA)

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 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 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.

Stock Items From Supply Class 2840 Stock Items From Supply Class 2840 Page 11 of 15

200053308
3106196-01
RNCC: 3 | RNVC: 2
218504181
15654
RNCC: 3 | RNVC: 2
218716479
714251CL13
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218569916
482220
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218062102
BK21358
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218088827
11A00088P011
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219203095
ST3268-069
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218416206
5005T57G01
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200079561
3033063CL
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200051070
3070435-01
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218719249
3029174
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218088825
37R601213P132
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200064549
3049049-01
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218961444
12A00399G02
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200007638
3117761-01
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218582225
349342
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218961655
699766,699767,699768AND699769
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218442283
4002T59P13
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218442291
12A00115P17
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218457628
5005T80G06
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200008624
3018111
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(241)001983018111
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218694400
615002
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615002
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218416408
37C302307P123
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218425241
6840899
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218458574
3008T00P01
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219045208
192031
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218442381
4011T97G01
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218055102
BK19716
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218797110
6896462
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23052070
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37E502188P101
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219090529
3029394CL4
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219215844
3119361-01
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218059976
BK16635
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218055111
BK19725
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219045610
3017600/PT6T-3B
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218569748
567690
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218127994
10A121G1
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218715263
5039T54G01
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219090958
PT6A135
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85-694-3241
RNCC: 6 | RNVC: 9
218055124
BK19786
RNCC: 3 | RNVC: 2
218054370
BK20051
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200024619
C4P1814-21
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218490600
6003T50G004REVF
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11A00109G02
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6003T50G04
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200026923
PWC38278
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219207710
3108923-01
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218490117
37R601232P114
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37R601232P114
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200052418
215T93860-2
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01R3117664-01
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5013T60G01
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200038267
01R3037068
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200004244
3109562-01
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200026239
3036829CL1
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218055165
BK22684
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219213819
3033914
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3004T47P01
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218457276
11A00086P01
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RK14009
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12A00430P16
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12A00115P16
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200046256
11A00110G18
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3029394CL9
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529603
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5310HF7967711
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200004070
3045349-01
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200069936
3111335-01
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218081754
BK22182
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219002489
12A00097P01
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218055074
BK18650
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219203106
ST3268-080
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200015819
3113391-01
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200038340
3036829CL4
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218961722
C6L1022-27
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C6L1022-27
RNCC: 5 | RNVC: 2
219211374
3054820-01
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218434249
3006T55P01
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219213456
3039548CL
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218442342
12A00075G01
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6920T09G01
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6004T31G01
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219002681
11A00228G02
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200080514
3076213-01
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219002653
126758-6-2
RNCC: 3 | RNVC: 2
126758-3
RNCC: 5 | RNVC: 9
126758-5
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126758-5
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218416451
4009T96P01
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218054379
BK20129
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218442294
12A00115P20
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KB7110
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310461-01
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3056685-01
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200069213
3042000
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JT15D-5A
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218062129
BK24462
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219002069
12A00105G07
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12A00105G06
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218425247
6856479
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12A00115P05
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12A00396G01
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218416054
3009T72P01
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200011482
ST3700-06
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200079958
3078347-01
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3076702-01
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200038338
3036829CL2
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3001T44P01
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219205453
3050299-01
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218601028
Z215
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218443338
10A222G3
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10A222G2
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200002372
3120495-01
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200026919
PWC37495
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218674576
545133
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219214440
3111481-01
RNCC: 3 | RNVC: 2
200002350
3019353
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200049786
3028047
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218055117
BK19764
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218054411
D37322
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219090805
12A00525G02
RNCC: 3 | RNVC: 2