We appreciate your interest in Turbo Power And Marine System Inc part number 443843, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 443843 is listed with the NSN 5340-00-856-9078 and description “Bracket Angle.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Turbo Power And Marine System Inc under the CAGE Code 11449 or that similarly fall under the FSC 5340 Hardware Commercial, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 5340-00-856-9078 parts and Bracket Angle items your operations require, so request a quote today.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5340-00-856-9078 Item PartTypeName: BRACKET,ANGLE | 5340 | 008569078 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 65-11659-97 | 2 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ADLK | FIRST LEG LENGTH | 0.926 INCHES NOMINAL |
| ADLL | SECOND LEG LENGTH | 1.129 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | W/S: ENGINE,AIRCRAFT TF33-PW-102 (C-135E,EC-135H/K/P); AIRCRAFT,C-18A,EC-18B; ENGINE,AIRCRAFT,TF-33-P-7 (C-141A/B); ENGINE,AIRCRAFT TF33-P-3/5/9 (C/EC-135,B52H); JOINT STARS TARGET RADAR SYSTEM; AIRCRAFT,STRATOFORTRESS B-52; AIRCRA |
| AHRA | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.312 INCHES NOMINAL |
| AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| AJFP | FIRST LEG END RADIUS | 0.500 INCHES NOMINAL |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| AKBU | SECOND LEG STYLE | END RADIUS |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| STYL | STYLE DESIGNATOR | ANGLE |
| AHLF | SECOND LEG WIDTH | 0.625 INCHES NOMINAL |
| AHLK | FIRST LEG HOLE DIAMETER | 0.344 INCHES NOMINAL |
| AHLN | SECOND LEG HOLE DIAMETER | 0.219 INCHES NOMINAL |
| AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.312 INCHES NOMINAL |
| AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.310 INCHES NOMINAL |
| AHPW | FIRST LEG THICKNESS | 0.059 INCHES NOMINAL |
| AHPX | SECOND LEG THICKNESS | 0.059 INCHES NOMINAL |
| AHQN | FIRST LEG WIDTH | 0.625 INCHES NOMINAL |
| AJFQ | SECOND LEG END RADIUS | 0.500 INCHES NOMINAL |
| AJZU | FIRST LEG STYLE | END RADIUS |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CSSQ | FIRST LEG ANGLE | 75.0 DEGREES NOMINAL |
| FEAT | SPECIAL FEATURES | THIS PART MEETS THE Y REQUIREMENTS DUE TO CRITICAL FEATURES,TOLERANCES,FIT RESTRICTIONS,MATERIAL PROPERTIES AND MANUFACTURING PROCESS. FAILURE COULD RESULT IN LOSS OR SUBSTANTIAL DAMAGE TO WEAPON SYSTEM,DEATH OR SERIOUS INJURY |
| MATT | MATERIAL | STEEL COMP 410 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | 66 FED STD SINGLE MATERIAL RESPONSE |
| SFTT | SURFACE TREATMENT | PASSIVATE |
| ZZZV | FSC APPLICATION DATA | ENGINE,ACFT,TURBO-FAN |
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