Aerospace Engineering Solutions is proud to offer immediate purchasing options on Beta Engineering Inc part number 578289, a Bracket Angle product we carry that is listed with the NSN 5340-00-989-8502 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to Beta Engineering Inc through the CAGE Code 33436, as well as categorized under FSC 5340 Hardware Commercial based on the first four digits of the NSN 5340-00-989-8502. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number 578289 and other NSN items of need.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5340-00-989-8502 Item PartTypeName: BRACKET,ANGLE | 5340 | 009898502 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 578289 | 2 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ADLK | FIRST LEG LENGTH | 0.860 INCHES NOMINAL |
| ADLL | SECOND LEG LENGTH | 0.960 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | W/S:ENGINE,AIRCRAFT TF33-PW-102 (C-135E,EC-135H/K/P); ENGINE,AIRCRAFT TF33-P-3/5/9 (C/EC-135,B-52H); ENGINE,AIRCRAFT,TF-33-P-7 (C-141A/B); AIRCRAFT,F-111 |
| AHLF | SECOND LEG WIDTH | 0.560 INCHES NOMINAL |
| AHLK | FIRST LEG HOLE DIAMETER | 0.344 INCHES NOMINAL |
| AHLN | SECOND LEG HOLE DIAMETER | 0.280 INCHES NOMINAL |
| AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.280 INCHES NOMINAL |
| AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.280 INCHES NOMINAL |
| AHPW | FIRST LEG THICKNESS | 0.059 INCHES NOMINAL |
| AHPX | SECOND LEG THICKNESS | 0.059 INCHES NOMINAL |
| AHQN | FIRST LEG WIDTH | 0.560 INCHES NOMINAL |
| AHRA | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.280 INCHES NOMINAL |
| AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.280 INCHES NOMINAL |
| AJFP | FIRST LEG END RADIUS | 0.500 INCHES NOMINAL |
| AJFQ | SECOND LEG END RADIUS | 0.500 INCHES NOMINAL |
| AJZU | FIRST LEG STYLE | END RADIUS |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| AKBU | SECOND LEG STYLE | END RADIUS |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CSSQ | FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| MATT | MATERIAL | TITANIUM ALLOY |
| STYL | STYLE DESIGNATOR | ANGLE |
| ZZZV | FSC APPLICATION DATA | ENGINE,AIRCRAFT |
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