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2840-01-475-2556
Aircraft Gas Turbine Engine
2840014752556 014752556 9521M10G01
A continuous combustion type engine. Consists primarily of a COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE, CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE and a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It may have an AFTERBURNER, TURBINE ENGINE and/or a fan section. Air is compressed and heated by a combustible fuel and expanded through the turbine. It is designed to furnish a source of rotary shaft, pneumatic power or thrust power. The pneumatic power is obtained by a bleedoff of the engine compressor. For a complete operating power unit, mounted on a base, see POWER UNIT, GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine
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Restrictions 2840-01-475-2556
IUID Required
2840-01-475-2556 is a Aircraft Gas Turbine Engine that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item where key elements must be removed and destroyed to prevent this item being restored or repaired. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-475-2556
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-475-2556
- US Air Force (FXX4)
- Effective Date:
- 1 May 2000
Approved Sources 2840-01-475-2556
- Part Number
- Manufacturer
- Status
- 9521M10G01
- Manufacturer
- 58828 - Cfm International Inc (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-475-2556
- Characteristic
- Specifications
- FIIG
- Specifications
- A526A0
- Fuel Type [FUEL]
- Jet Fuel
- Power Output For Which Designed [AXKD]
- Pneumatic/Shaft
- Mounting Type [AAXX]
- Any Acceptable
- Reference Data And Literature [RDAL]
- 2J-F110-4
- Criticality Code Justification [CRTL]
- Agav
- End Item Identification [AGAV]
- F110-100 Engine
DLA Procurement Analysis 2840-01-475-2556
Management Data 2840-01-475-2556
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2002
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
Air Force
- Fund:
- AF
- HQ USAF regulated
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- IN
- ENGINES, COMPLETE
- Price Validation Code:
- N
- The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of āLā or āFā, then it must be evaluated locally where purchased or fabricated.
- Expendability
Recoverability
Repairability: - T
- Expendable. Reparable. Condemn at Depot. AF Recoverable Assembly Management System (AFRAMS).
NATO Stock Numbers Related to 2840-01-475-2556
Freight Information 2840-01-475-2556
2840-01-475-2556 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 114215. A Sub NMFC of Z. It has a NMFC Description of ASSEMBLIES JET AIRCRAFT ENGINE. 2840-01-475-2556 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. 2840-01-475-2556 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 671 for ocean manifesting and military sealift. 2840-01-475-2556 is not classified as a special type of cargo when transported by water. 2840-01-475-2556 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.