| Mfg Part Number: 4028800 | Manufacturer: United Technologies Corp |
| NSN : 5340-00-385-9275 | NIIN : 003859275 |
| Item Name : bracket angle | CAGE Code : 77445 |
| FSC : 5340 Hardware Commercial |
Thank you for your interest in our available 4028800 NSN part. This part number 4028800 is a Bracket Angle listed under the FSC 5340 Hardware Commercial, and it is manufactured by United Technologies Corp. At Internet of Components, all of our stock and inventory are available for purchase today, ready to ship with short lead times and competitive pricing. Whether you are in need of parts that are new, used, or obsolete, our team of industry experts is readily available 24/7x365 to fulfill all of your operational
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Internet of Components is a premier supplier of 4028800 NSN component, and we carry recently requested NSN components such as 5340003859275. We strive to only provide our customers with quality parts, which is why we choose to source our inventory from thousands of global manufacturers such as United Technologies Corp. If you are interested in this particular item, we invite you to begin the purchasing process for 4028800 today by filling out and submitting an Instant RFQ. Once received, a member of our staff will review and reach out to you in 15 minutes or less to provide a personalized quote that caters towards your individual needs. Get started on the purchasing process today and see how we are revolutionizing the purchasing process.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5340-00-385-9275 Item Description: Bracket Angle | 5340 | 003859275 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4028800 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | W/S:ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); AIRCRAFT, EAGLE F-15; SUPPORT EQUIPMENT, C-5 AIRCRAFT; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, F-16 |
| AHLK | FIRST LEG HOLE DIAMETER | 0.216 INCHES MINIMUM AND 0.226 INCHES MAXIMUM |
| AHLN | SECOND LEG HOLE DIAMETER | 0.276 INCHES MINIMUM AND 0.286 INCHES MAXIMUM |
| AHLS | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG LENGTH | 1.500 NOMINAL INCHES |
| AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.640 INCHES NOMINAL |
| AHPW | FIRST LEG THICKNESS | 0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
| AHPX | SECOND LEG THICKNESS | 0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
| AJZU | FIRST LEG STYLE | END RADIUS |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CSSQ | FIRST LEG ANGLE | 0.109 RADIANS MINIMUM AND 0.141 RADIANS MAXIMUM |
| MATT | MATERIAL | TITANIUM ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4911 NATIONAL SPEC SINGLE MATERIAL RESPONSE |
| STYL | STYLE DESIGNATOR | OFFSET ANGLE |
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