To receive competitive purchasing options on part number 446169 by United Technologies Corporation, look no further than NSN Direct. For your reference, this item has the NSN 5340-00-344-2956 and is listed with the description “Bracket Angle.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other United Technologies Corporation parts produced under the CAGE Code 77445, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number 446169, you can glean from the first four digits of its NSN 5340-00-344-2956 that it belongs to the FSC 5340 Hardware Commercial. This being said, do not hesitate to request quotes on part number 446169 and any other NSN parts that we feature to experience unrivaled procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5340-00-344-2956 Item PartTypeName: BRACKET,ANGLE | 5340 | 003442956 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 446169 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | CASE ASSEMBLY,TURBINE; W/S: ENGINE,AIRCRAFT TF33-PW-102 (C-135E,EC-135H/K/P); ENGINE,AIRCRAFT,TF-33-P-7 (C-141A/B); AIRCRAFT,STRATOFORTRESS B-52; ENGINE,AIRCRAFT TF33-P-3/5/9 (C/EC-135,B-52H) |
| AHLF | SECOND LEG WIDTH | 1.509 INCHES NOMINAL |
| AHLG | SECOND LEG CORNER RADIUS | 0.250 INCHES NOMINAL |
| AHLK | FIRST LEG HOLE DIAMETER | 0.224 INCHES NOMINAL |
| AHLN | SECOND LEG HOLE DIAMETER | 0.286 INCHES NOMINAL |
| AHLP | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.009 INCHES NOMINAL |
| AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
| AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| AHPW | FIRST LEG THICKNESS | 0.062 INCHES NOMINAL |
| AHPX | SECOND LEG THICKNESS | 0.062 INCHES NOMINAL |
| AHQN | FIRST LEG WIDTH | 0.510 INCHES NOMINAL |
| AHRA | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
| AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| AJFP | FIRST LEG END RADIUS | 0.375 INCHES NOMINAL |
| AJZU | FIRST LEG STYLE | END RADIUS |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| AKBU | SECOND LEG STYLE | CORNER RADIUS |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CSSQ | FIRST LEG ANGLE | 130.0 DEGREES NOMINAL |
| CSSZ | SECOND LEG OFFSET ANGLE | 80.9 DEGREES NOMINAL |
| FEAT | SPECIAL FEATURES | THIS PART MEETS THE Y REQUIREMENTS DUE TO CRITICAL FEATURES,TOLERANCES,FIT RESTRICTIONS,MATERIAL PROPERTIES AND MANUFACTURING PROCESS. FAILURE COULD RESULT IN LOSS OR SUBSTANTIAL DAMAGE TO WEAPON SYSTEM,DEATH OR SERIOUS INJURY |
| MATT | MATERIAL | STEEL COMP 410 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | 66 FED STD SINGLE MATERIAL RESPONSE |
| STYL | STYLE DESIGNATOR | OFFSET ANGLE |
| ZZZV | FSC APPLICATION DATA | ENGINE,JET,AIRCRAFT |
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