Thank you for taking interest in the Turbo Power And Marine System Inc part number 421117, a Bracket Angle product that we stock that is presented alongside the NSN 5340-00-808-1002 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 421117 specifically traces back to Turbo Power And Marine System Inc through the CAGE Code 11449, a distinct identifier for one of their physical locations. Moreover, with the NSN 5340-00-808-1002, this listing falls within Federal Supply Code (FSC) 5340 Hardware Commercial, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 421117 here on Aero OEM Parts 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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