Thank you for considering United Technologies Corporation part number 815686, an item we carry that is listed with the NSN 2840-01-458-2761 and product description “Case Compressor Aircraft Gas Tur.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number 815686 was specifically produced by United Technologies Corporation under CAGE Code 77445, and with the NSN 2840-01-458-2761, it belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number 815686 today, knowing we will be in touch shortly after reviewing your information.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-458-2761 Item PartTypeName: CASE,COMPRESSOR,AIRCRAFT GAS TUR | 2840 | 014582761 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 815686 | 3 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMZ | Diameter | 35.433 INCHES MINIMUM AND 35.443 INCHES MAXIMUM |
| RDAL | Reference Data And Literature | T.O. 2J-TF33-44, FIG 11, IND 1; 2J-TF33-14, FIG 13, IND 1 |
| CZBJ | Engine Section Location | COMPRESSOR |
| FEAT | Special Features | THIS IS A REDESIGNED CASE FEATURING A REINFORCED 6TH STATOR SUPPORT LAND; REPLACES P/N 454832 |
| ABHP | Overall Length | 18.028 INCHES MINIMUM AND 18.032 INCHES MAXIMUM |
| CXCY | Part Name Assigned By Controlling Agency | ORIGINAL NAME CASE,FRONT COMPRESSOR |
| MRC | Decoded Requirement | Clear Text Reply |
| MATT | Material | STEEL OVERALL |
| CRTL | Criticality Code Justification | ABHP AND ABMZ AND FEAT AND CZBJ |
| CQFM | Hardness Rating | 26.0 ROCKWELL C MINIMUM OVERALL AND 32.0 ROCKWELL C MAXIMUM OVERALL |
| AGAV | End Item Identification | TF33 AIRCRAFT GAS TURBINE ENG |
| APGF | Design Type | AXIAL COMPRESSOR |
| MDCL | Material Document And Classification | AMS6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
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