Whether you are in search of military and defense parts, aerospace parts, or other similar product solutions, Satellite To Submarine Parts is your one-stop shop. Thank you for your interest in part number 4038404, a United Technologies Corporation item that is listed alongside the description “Bracket Angle” and the NSN 5340003775658. To guarantee a swift procurement process for NSN part number 4038404, be sure to request a quote by filling out and submitting the RFQ form below, and one of our experts will offer a customized solution for your comparisons in response.
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We list everything with as much relevant information as possible to ensure that customers can swiftly identify and procure the exact products they need. For instance, while part number 4038404 is manufactured by United Technologies Corporation, it is specifically done so under CAGE Code 77445, a unique identifier assigned to a particular facility by the DLA that supplies to various government or defense agencies. Additionally, using the first digits of the NSN 5340-00-377-5658, one can also determine that this part falls under FSC 5340 Hardware Commercial. Keeping this in mind, initiate the purchasing process today to see why so many customers depend on us for the NSN items they require.
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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