Thank you for your interest in United Technologies Corporation part number 4038404, a Bracket Angle item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 5340-00-377-5658, and you can obtain customized procurement solutions on this component from our team members by completing and submitting the form below. For our specialists to best deliver quotes that accommodate your specifications, please be sure we are presented with essential details like your target price, desired quantity, and anticipated fulfillment timeline. Once we have the opportunity to receive and review your submission, we will strive to provide a tailored response for your consideration within 15 minutes or less.
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Besides part number 4038404, you may browse our platform further for similar components produced by United Technologies Corporation under the CAGECode 77445, as well as additional products that are categorized under FSC 5340 Hardware Commercial. If you have any questions regarding our services or the NSN 5340-00-377-5658 items that we sell, you may always give us a call or email, as we would be delighted to assist you in any way that we can. Otherwise, we encourage you to request a quote for part number 4038404 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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