We appreciate your interest in United Technologies Corporation part number 711412, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 711412 is listed with the NSN 2840-00-947-7115 and description “Blade Compressor Aircraft Gas Tu.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by United Technologies Corporation under the CAGE Code 77445 or that similarly fall under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 2840-00-947-7115 parts and Blade Compressor Aircraft Gas Tu items your operations require, so request a quote today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-00-947-7115 Item PartTypeName: BLADE,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 009477115 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
711412 | 1 | 2 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 2.782 INCHES MINIMUM AND 2.791 INCHES MAXIMUM |
ABMK | OVERALL WIDTH | 1.160 INCHES MINIMUM AND 1.170 INCHES MAXIMUM |
ABPX | MATERIAL THICKNESS | 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | ENGINE MODEL J57 |
APGF | DESIGN TYPE | COMPRESSOR |
CQFM | HARDNESS RATING | 32.0 ROCKWELL C MINIMUM BLADE AND 38.0 ROCKWELL C MAXIMUM BLADE |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
FEAT | SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
MATT | MATERIAL | STEEL BLADE |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
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