| Mfg Part Number: 1284M50P001A | Manufacturer: Enginetics Corporation |
| NSN : 5340-01-213-9985 | NIIN : 012139985 |
| Item Name : bracket angle | CAGE Code : 60168 |
| FSC : 5340 Hardware Commercial |
Thank you for your interest in our available 1284M50P001A NSN part. This part number 1284M50P001A is a Bracket Angle listed under the FSC 5340 Hardware Commercial, and it is manufactured by Enginetics Corporation. 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 1284M50P001A NSN component, and we carry recently requested NSN components such as 5340012139985. 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 Enginetics Corporation. If you are interested in this particular item, we invite you to begin the purchasing process for 1284M50P001A 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 |
|---|---|---|---|---|---|---|
| 5340-01-213-9985 Item Description: Bracket Angle | 5340 | 012139985 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1284M50P001A | 5 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ACHY | MOUNTING HOLE TYPE | PLAIN |
| AGAV | END ITEM IDENTIFICATION | W/S: ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT F110-GE-400; ENGINE, AIRCRAFT, F110-GE-100/129 (F-16 C/D); ENGINE, AIRCRAFT, F-108 (CFM-56, KC-135A) |
| AHLK | FIRST LEG HOLE DIAMETER | 0.274 INCHES MINIMUM AND 0.288 INCHES MAXIMUM |
| AHLN | SECOND LEG HOLE DIAMETER | 0.274 INCHES MINIMUM AND 0.288 INCHES MAXIMUM |
| AHPW | FIRST LEG THICKNESS | 0.060 INCHES MINIMUM AND 0.066 INCHES MAXIMUM |
| AHPX | SECOND LEG THICKNESS | 0.060 INCHES MINIMUM AND 0.066 INCHES MAXIMUM |
| AJZU | FIRST LEG STYLE | ANGLE |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| AKBU | SECOND LEG STYLE | ANGLE |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| MATT | MATERIAL | NICKEL ALLOY 625 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5599 ASSN STD SINGLE MATERIAL RESPONSE |
| STYL | STYLE DESIGNATOR | ANGLE |
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