Aerospace Engineering Solutions is proud to offer immediate purchasing options on The Boeing Company part number 39 10794 4, a Bracket Angle product we carry that is listed with the NSN 5340-00-808-1002 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to The Boeing Company through the CAGE Code 82918, as well as categorized under FSC 5340 Hardware Commercial based on the first four digits of the NSN 5340-00-808-1002. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number 39 10794 4 and other NSN items of need.
| 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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