Aerospace Performance Parts is pleased to offer immediate purchasing options for United Technologies Corporation part number 4038404A, which you have taken interest in. This Bracket Angle item is listed alongside the NSN 5340-00-377-5658 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 4038404A or any other FSC 5340 Hardware Commercial components we carry from United Technologies Corporation under CAGE Code 77445, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 5340-00-377-5658 part number 4038404A today, knowing we will support all your operational needs with care.
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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