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Quality guaranteed We sell only warrantied and traceable partsIf you have been searching for 1284M50P001A of Bracket Angle components with NSN 5340012139985 under FSC 5340 Hardware Commercial, look no further than Limitless Aerospace. 1284M50P001A part is listed alongside the other Bracket Angle parts, and it has been manufactured by Lighthouse Manufacturing Llc (CAGE Code 53767). With current availability through our website, we invite you to request a quick and competitive quote for 1284M50P001A by filling out and submitting the RFQ form below. By providing us with information such as your target price and when you need your parts by, we can ensure that we offer a personalized solution that accommodates your individual needs and requirements.
NSN parts are those that follow the NSN system as dictated by the NATO Standardization Agreements, and they contain a 13-digit serial number to optimize the procurement, stocking, and issuing of items through the federal supply system. On Limitless Aerospace, we make finding the NSN parts and components you need easy, and customers may peruse our robust NSN part catalogues or use our search engine to find specific items with ease. As the only independent distributor with a no China sourcing pledge, we choose to only stock items from top global manufacturers such as Lighthouse Manufacturing Llc. Get started on the purchasing process for 1284M50P001A today and see how we can serve as your strategic sourcing partner for all of your operational needs.
| 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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