Whether you are in search of military and defense parts, aerospace parts, or other similar product solutions, Satellite To Submarine Parts is your one-stop shop. Thank you for your interest in part number 9992M69G40, a Cfm International Inc item that is listed alongside the description “Case Compressor Aircraft Gas Tur” and the NSN 2840011892633. To guarantee a swift procurement process for NSN part number 9992M69G40, be sure to request a quote by filling out and submitting the RFQ form below, and one of our experts will offer a customized solution for your comparisons in response.
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We list everything with as much relevant information as possible to ensure that customers can swiftly identify and procure the exact products they need. For instance, while part number 9992M69G40 is manufactured by Cfm International Inc, it is specifically done so under CAGE Code 58828, a unique identifier assigned to a particular facility by the DLA that supplies to various government or defense agencies. Additionally, using the first digits of the NSN 2840-01-189-2633, one can also determine that this part falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Keeping this in mind, initiate the purchasing process today to see why so many customers depend on us for the NSN items they require.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-189-2633 Item PartTypeName: CASE,COMPRESSOR,AIRCRAFT GAS TUR | 2840 | 011892633 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1276M13G04 | 2 | 2 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 22.000 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | ACFT ENG F108 |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | CASE ASSY-FRONT & EXTENSION CPRSR STTR |
CZBJ | ENGINE SECTION LOCATION | TURBINE |
FEAT | SPECIAL FEATURES | ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE |
MATT | MATERIAL | TITANIUM OVERALL |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14 FIG 72-32-00-05 IND 400L |
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