Thank you for taking interest in the United Technologies Corporation part number 4038404, a Bracket Angle product that we stock that is presented alongside the NSN 5340-00-377-5658 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 4038404 specifically traces back to United Technologies Corporation through the CAGE Code 77445, a distinct identifier for one of their physical locations. Moreover, with the NSN 5340-00-377-5658, this listing falls within Federal Supply Code (FSC) 5340 Hardware Commercial, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 4038404 here on Aero OEM Parts at your earliest convenience.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5340-00-377-5658 Item PartTypeName: BRACKET,ANGLE | 5340 | 003775658 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4038404A | 2 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
STYL | STYLE DESIGNATOR | ANGLE |
ADLK | FIRST LEG LENGTH | 0.405 INCHES MINIMUM AND 0.435 INCHES MAXIMUM |
ADLL | SECOND LEG LENGTH | 0.630 INCHES MINIMUM AND 0.650 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | W/S: ENGINE,AIRCRAFT,F100-PW-200 (F-16A/B/C/D); AIRCRAFT,EAGLE F-15; SUPPORT EQUIPMENT,C-5 AIRCRAFT; AIRCRAFT,F-16; ENGINE,AIRCRAFT,F100-PW-100 (F-15A/B/C/D); ADVANCE AIR TRAFFIC CONTR. & LAND. SYS (ATCALS) 404L; AIRCRAFT,F-111; ENG |
AHLF | SECOND LEG WIDTH | 0.190 INCHES MINIMUM AND 0.210 INCHES MAXIMUM |
AHLK | FIRST LEG HOLE DIAMETER | 0.160 INCHES MINIMUM AND 0.170 INCHES MAXIMUM |
AHPW | FIRST LEG THICKNESS | 0.023 INCHES MINIMUM AND 0.027 INCHES MAXIMUM |
AHPX | SECOND LEG THICKNESS | 0.023 INCHES MINIMUM AND 0.027 INCHES MAXIMUM |
AHQN | FIRST LEG WIDTH | 0.330 INCHES MINIMUM AND 0.350 INCHES MAXIMUM |
AHRA | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.165 INCHES MINIMUM AND 0.175 INCHES MAXIMUM |
AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.165 INCHES MINIMUM AND 0.175 INCHES MAXIMUM |
AJFP | FIRST LEG END RADIUS | 0.165 INCHES MINIMUM AND 0.175 INCHES MAXIMUM |
AJFQ | SECOND LEG END RADIUS | 0.095 INCHES MINIMUM AND 0.105 INCHES MAXIMUM |
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 | NO HOLE |
CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
CSSQ | FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
MATT | MATERIAL | STEEL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5540 ASSN STD SINGLE MATERIAL RESPONSE |
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