Buy Mil Spares is your sourcing solution for top-quality military and defense parts, aerospace parts, and other similar products that are necessary for operational fulfillment. You have reached the RFQ page for part number 4050727, a Bracket Angle item that is listed with the NSN 5340-01-066-7130 for an ease of identification. Manufactured by Turbo Power And Marine System Inc and readily available for procurement today, you are always welcome to request a quote on this NSN part to receive tailored pricing information and fulfillment options from our team. Simply offer us important information like your desired quantity, price, and fulfillment timeframe, and our team will supply you with a tailored quote on part number 4050727 in 15 minutes or less.
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To ensure that customers quickly identify and procure exact items, we list everything with as much relevant information as possible. For example, while part number 4050727 is manufactured by Turbo Power And Marine System Inc, it is specifically done so under CAGE Code 11449, a unique identifier assigned to a specific facility by the DLA that supplies to various government or defense agencies. Furthermore, using the first digits of the NSN 5340-01-066-7130, one can also determine that this part falls under FSC 5340 Hardware Commercial. With this in mind, continue exploring our website today, and see how we can help you secure competitive pricing and rapid lead times on all desired NSN parts.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5340-01-066-7130 Item PartTypeName: BRACKET,ANGLE | 5340 | 010667130 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4050727 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ACHY | MOUNTING HOLE TYPE | COUNTERBORED |
| ADLL | SECOND LEG LENGTH | 1.105 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | W/S:ENGINE,AIRCRAFT,F100-PW-200 (F-16A/B/C/D); SUPPORT EQUIPMENT,C-5 AIRCRAFT; AIRCRAFT,F-16; ENGINE,AIRCRAFT,F100-PW-100 (F-15A/B/C/D) |
| AHLF | SECOND LEG WIDTH | 1.881 INCHES NOMINAL |
| AHLK | FIRST LEG HOLE DIAMETER | 0.221 INCHES NOMINAL |
| AHLN | SECOND LEG HOLE DIAMETER | 0.281 INCHES NOMINAL |
| AHLP | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.381 INCHES NOMINAL |
| AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| AHPW | FIRST LEG THICKNESS | 0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
| AHPX | SECOND LEG THICKNESS | 0.050 INCHES NOMINAL |
| 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 | 90.0 DEGREES NOMINAL |
| MATT | MATERIAL | TITANIUM ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4911 ASSN STD SINGLE MATERIAL RESPONSE |
| STYL | STYLE DESIGNATOR | ANGLE |
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