Thank you for your interest in Turbo Power And Marine System Inc part number 421117, a Bracket Angle item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 5340-00-808-1002, 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 421117, you may browse our platform further for similar components produced by Turbo Power And Marine System Inc under the CAGECode 11449, as well as additional products that are categorized under FSC 5340 Hardware Commercial. If you have any questions regarding our services or the NSN 5340-00-808-1002 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 421117 at your earliest convenience.
| 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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