If you have been searching for 676331 of Bracket Angle components with NSN 5340001531011 under FSC 5340 Hardware Commercial, look no further than Limitless Aerospace. 676331 part is listed alongside the other Bracket Angle parts, and it has been manufactured by Gould E A And Co (CAGE Code 03730). With current availability through our website, we invite you to request a quick and competitive quote for 676331 by filling out and submitting the RFQ form below. By providing us with information such as your target price and when you need your parts by, we can ensure that we offer a personalized solution that accommodates your individual needs and requirements.
NSN parts are those that follow the NSN system as dictated by the NATO Standardization Agreements, and they contain a 13-digit serial number to optimize the procurement, stocking, and issuing of items through the federal supply system. On Limitless Aerospace, we make finding the NSN parts and components you need easy, and customers may peruse our robust NSN part catalogues or use our search engine to find specific items with ease. As the only independent distributor with a no China sourcing pledge, we choose to only stock items from top global manufacturers such as Gould E A And Co. Get started on the purchasing process for 676331 today and see how we can serve as your strategic sourcing partner for all of your operational needs.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5340-00-153-1011 Item Description: Bracket Angle | 5340 | 001531011 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
676331 | 2 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ADLK | FIRST LEG LENGTH | 1.307 INCHES NOMINAL |
ADLL | SECOND LEG LENGTH | 1.769 INCHES MINIMUM AND 1.779 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | W/S:ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); 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-30 |
AHLK | FIRST LEG HOLE DIAMETER | 0.216 INCHES MINIMUM AND 0.226 INCHES MAXIMUM |
AHLN | SECOND LEG HOLE DIAMETER | 0.276 INCHES MINIMUM AND 0.286 INCHES MAXIMUM |
AHLP | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.173 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 | 0.200 INCHES MINIMUM AND 0.210 INCHES MAXIMUM |
AHPW | FIRST LEG THICKNESS | 0.056 INCHES MINIMUM AND 0.062 INCHES MAXIMUM |
AHPX | SECOND LEG THICKNESS | 0.056 INCHES MINIMUM AND 0.062 INCHES MAXIMUM |
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 | 0.250 INCHES NOMINAL |
AJZU | FIRST LEG STYLE | END RADIUS AND TAPERED |
AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
CSSQ | FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
MATT | MATERIAL | STEEL COMP 410 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5504 ASSN STD SINGLE MATERIAL RESPONSE |
STYL | STYLE DESIGNATOR | ANGLE |
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