Thank you for taking interest in Turbo Power And Marine System Inc part number 446169, which is listed with the NSN 5340-00-344-2956 and a product description of “Bracket Angle.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number 446169, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Bracket Angle part with the NSN 5340-00-344-2956. For example, you can browse other Turbo Power And Marine System Inc components that were produced under CAGE Code 11449 or listings that belong to FSC 5340 Hardware Commercial with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 446169 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5340-00-344-2956 Item PartTypeName: BRACKET,ANGLE | 5340 | 003442956 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 446169 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | CASE ASSEMBLY,TURBINE; W/S: ENGINE,AIRCRAFT TF33-PW-102 (C-135E,EC-135H/K/P); ENGINE,AIRCRAFT,TF-33-P-7 (C-141A/B); AIRCRAFT,STRATOFORTRESS B-52; ENGINE,AIRCRAFT TF33-P-3/5/9 (C/EC-135,B-52H) |
| AHLF | SECOND LEG WIDTH | 1.509 INCHES NOMINAL |
| AHLG | SECOND LEG CORNER RADIUS | 0.250 INCHES NOMINAL |
| AHLK | FIRST LEG HOLE DIAMETER | 0.224 INCHES NOMINAL |
| AHLN | SECOND LEG HOLE DIAMETER | 0.286 INCHES NOMINAL |
| AHLP | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.009 INCHES NOMINAL |
| AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
| AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| AHPW | FIRST LEG THICKNESS | 0.062 INCHES NOMINAL |
| AHPX | SECOND LEG THICKNESS | 0.062 INCHES NOMINAL |
| AHQN | FIRST LEG WIDTH | 0.510 INCHES NOMINAL |
| AHRA | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
| AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| AJFP | FIRST LEG END RADIUS | 0.375 INCHES NOMINAL |
| AJZU | FIRST LEG STYLE | END RADIUS |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| AKBU | SECOND LEG STYLE | CORNER RADIUS |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CSSQ | FIRST LEG ANGLE | 130.0 DEGREES NOMINAL |
| CSSZ | SECOND LEG OFFSET ANGLE | 80.9 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 |
| STYL | STYLE DESIGNATOR | OFFSET ANGLE |
| ZZZV | FSC APPLICATION DATA | ENGINE,JET,AIRCRAFT |
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