Thank you for considering The Boeing Company part number 39 10794 4, an item we carry that is listed with the NSN 5340-00-808-1002 and product description “Bracket Angle.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number 39 10794 4 was specifically produced by The Boeing Company under CAGE Code 82918, and with the NSN 5340-00-808-1002, it belongs to FSC 5340 Hardware Commercial. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number 39 10794 4 today, knowing we will be in touch shortly after reviewing your information.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5340-00-808-1002 Item PartTypeName: BRACKET,ANGLE | 5340 | 008081002 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 39-10794-4 | 2 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ADLL | SECOND LEG LENGTH | 0.970 INCHES NOMINAL |
| AHQY | FIRST LEG DISTANCE BETWEEN FIRST AND SECOND HOLE CENTERS ALONG WIDTH | 0.959 INCHES NOMINAL |
| CSSQ | FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | AMS 2400 ASSN STD SINGLE TREATMENT RESPONSE |
| STYL | STYLE DESIGNATOR | ANGLE |
| ADLK | FIRST LEG LENGTH | 0.730 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | W/S:ENGINE,AIRCRAFT TF33-PW-102 (C-135E,EC-135H/K/P); AIRCRAFT,STRATOFORTRESS B-52; ENGINE,AIRCRAFT,TF-33-P-7 (C-141A/B); ENGINE,AIRCRAFT TF33-P-3/5/9 (C/EC-135,B-52H) |
| AHLF | SECOND LEG WIDTH | 4.220 INCHES NOMINAL |
| AHLG | SECOND LEG CORNER RADIUS | 0.219 INCHES NOMINAL |
| AHLK | FIRST LEG HOLE DIAMETER | 0.339 INCHES MINIMUM AND 0.349 INCHES MAXIMUM |
| AHPW | FIRST LEG THICKNESS | 0.028 INCHES MINIMUM AND 0.034 INCHES MAXIMUM |
| AHPX | SECOND LEG THICKNESS | 0.028 INCHES MINIMUM AND 0.034 INCHES MAXIMUM |
| AHQW | FIRST LEG DISTANCE BETWEEN LOWER HOLE CENTERS ALONG WIDTH | 1.919 INCHES NOMINAL |
| AHQX | FIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG LENGTH | 0.031 INCHES NOMINAL |
| AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | THREE HOLES |
| AKBU | SECOND LEG STYLE | CORNER RADIUS |
| MATT | MATERIAL | STEEL COMP 4130 OR STEEL COMP 8630 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6350 ASSN STD 1ST MATERIAL RESPONSE OR AMS 6355 ASSN STD 2ND MATERIAL RESPONSE |
| SFTT | SURFACE TREATMENT | CADMIUM |
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