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 711514, a United Technologies Corporation item that is listed alongside the description “Blade Compressor Aircraft Gas Tu” and the NSN 2840008224834. To guarantee a swift procurement process for NSN part number 711514, 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 711514 is manufactured by United Technologies Corporation, it is specifically done so under CAGE Code 77445, 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 2840-00-822-4834, 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 |
---|---|---|---|---|---|---|
2840-00-822-4834 Item PartTypeName: BLADE,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 008224834 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
753014 | 3 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 2.269 INCHES MINIMUM AND 2.274 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | ENGINE MODEL J57 |
APGF | DESIGN TYPE | COMPRESSOR |
CQFM | HARDNESS RATING | 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
FEAT | SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
ABMK | OVERALL WIDTH | 1.017 INCHES MINIMUM AND 1.027 INCHES MAXIMUM |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
MATT | MATERIAL | STEEL BLADE |
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