AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
Thank you for choosing to fulfill your operational requirements for the Bracket Angle NSN parts you require with Buy Ground Support Equipment. On this page, you can submit a quote request for Turbo Power And Marine System Inc part number 446169, a component that can also be found by inputting NSN 5340-00-344-2956 in our search engine. Alongside part number 446169, we also have a wide range of other related items available, all of which can be traced back to a wealth of trusted manufacturers on our Approved Vendor List (AVL).
Buy Ground Support Equipment works with numerous government and defense agencies, so we use CAGE Codes like 11449 to uniquely identify items and their manufacturers in a standardized manner. We also utilize Federal Supply Classes (FSCs) to organize our inventory, ensuring customers can find Turbo Power And Marine System Inc part number 446169 by the FSC designation 5340 Hardware Commercial with ease. That being said, we encourage you to complete the RFQ form below for NSN 5340003442956 or any others that you are interested in, and we will provide you with a customized sourcing solution in 15 minutes or less. For one-on-one assistance, contact us via phone or email at any time; we are available 24/7x365!
| 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 |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
Request for Quote
