The NSN 5340-00-835-7556 part numbers such as 566437, 566437, 566437, 566437 manufactured by Gould E A And Co, Rogerson Kratos, Turbo Power And Marine System Inc, United Technologies Corporation are available in RFQ Experts’ inventory. An ASAP Semiconductor owned and operated website, RFQ Experts has over six billion parts in its inventory for NSN 5340-00-835-7556. ASAP is committed to streamlining the parts procurement process for our customers, making it easy for them to search through billions of parts to find exactly what they are looking for. We have dedicated account managers ready to solve procurement issues our clients face, whether it’s a need for obsolete parts, or an aircraft on ground situation. As an AS9120B, ISO 9001:2015, and FAA AC 0056B certified company, each and every part that we ship goes through numerous quality checks and inspections, to ensure that we sell only the highest-quality parts.
| Alternative NSN: 5340-00-835-7556 |
| Item Name: Bracket Double Angl |
| Federal Supply Class (FSC): 5340 Hardware, Commercial |
| NIIN: 008357556 |
| NCB Code: USA (00) |
| Manufacturers: Gould E A And Co, Rogerson Kratos, Turbo Power And Marine System Inc, United Technologies Corporation |
| Part No | NSN | Item Name | QTY | RFQ |
|---|---|---|---|---|
| 566437 | 5340-00-835-7556 | bracket double angl | Avl | RFQ |
| 566437 | 5340-00-835-7556 | bracket double angl | Avl | RFQ |
| 566437 | 5340-00-835-7556 | bracket double angl | Avl | RFQ |
| 566437 | 5340-00-835-7556 | bracket double angl | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD (NON-CORE) | MACHINED |
| ADLK | FIRST LEG LENGTH | 0.590 INCHES NOMINAL |
| ADLL | SECOND LEG LENGTH | 0.590 INCHES NOMINAL |
| AHLF | SECOND LEG WIDTH | 0.837 INCHES NOMINAL |
| AHLK | FIRST LEG HOLE DIAMETER | 0.281 INCHES NOMINAL |
| AHLN | SECOND LEG HOLE DIAMETER | 0.219 INCHES NOMINAL |
| AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.230 INCHES NOMINAL |
| AHPW | FIRST LEG THICKNESS | 0.059 INCHES NOMINAL |
| AHPX | SECOND LEG THICKNESS | 0.059 INCHES NOMINAL |
| AHPZ | CENTER SECTION HEIGHT | 1.604 INCHES NOMINAL |
| AHQA | CENTER SECTION WIDTH | 1.404 INCHES NOMINAL |
| AHQB | CENTER SECTION THICKNESS | 0.059 INCHES NOMINAL |
| AHQU | FIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.118 INCHES NOMINAL |
| AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.220 INCHES NOMINAL |
| AJFQ | SECOND LEG END RADIUS | 0.375 INCHES NOMINAL |
| AJZU | FIRST LEG STYLE | CORNER RADIUS |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| AKBU | SECOND LEG STYLE | END RADIUS |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| CSSR | SECOND LEG ANGLE | 90.0 DEGREES NOMINAL |
| MATT | MATERIAL | TITANIUM ALLOY |
| AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.263 INCHES NOMINAL |
| AHQN | FIRST LEG WIDTH | 1.618 INCHES NOMINAL |
| AHQP | FIRST LEG CORNER RADIUS | 0.250 INCHES NOMINAL |
| AHRA | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CSSQ | FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| STYL | STYLE DESIGNATOR | DOUBLE ANGLE |
| ZZZV | FSC APPLICATION DATA | TURBOJET ENGINE,ACFT |
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