Welcome to our online Request for Quote (RFQ) service, where you can fill out and submit the form provided below to obtain tailored procurement options from our team of industry experts. You have taken interest in part number 17P1F6162-503, which is a Gear Spur item from Boeing Company The that is listed with the NSN 3020-01-422-4106 for quick identification. Should you wish to move forward with quotation for this listing, be sure that you supply us with key details like your target pricing, quality, and delivery date. This information is what we will base presented quotes on, with responses offered shortly after the receipt and review of each form.
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To ensure that customers only procure exact items of need, we present our offerings with as much relevant data as possible. For example, part number 17P1F6162-503 was specifically produced by Boeing Company The under the CAGE Code 88277, providing traceability. Furthermore, with the NSN 3020-01-422-4106, one can also determine that this listing falls under Federal Supply Class (FSC) 3020 Gear Pulley Sprocket and Transmission Chain. Alongside such details, all purchases will come delivered with any applicable qualifying certifications, furthering the reliability of our purchasing options. With this in mind, be sure to request a quote on part number 17P1F6162-503, and we will be in touch.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 3020-01-422-4106 Item Description: Gear Spur | 3020 | 014224106 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 17p1f6162-503 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ANTP | Bore Style | INVOLUTE SPLINE BOTH ENDS |
| CTQY | Mounting Hole Type And Quantity | 4 THREADED AXIALLY THROUGH BODY, FIRST END |
| MRC | Decoded Requirement | Clear Text Reply |
| CWPP | Pressure Angle | 20.0000 DEGREES |
| CWRM | Face Nominal Width | 0.265 INCHES |
| CWZN | Bolt Hole Circle Nominal Diameter | 2.906 INCHES AXIALLY THROUGH BODY, FIRST END |
| STYL | Style Designator | ONE PROTRUDING HUB, ONE RECESSED HUB |
| AJLA | Teeth Quantity | 128 |
| ABSA | Spline Quantity | 23 BOTH ENDS |
| BDTX | Spline Pitch Diameter | 0.7187 INCHES NOMINAL BOTH ENDS |
| CWQR | Nominal Distance Between Body Face And Recessed Hub End | 0.130 INCHES SECOND END |
| AGJS | Pitch Diameter | 4.0000 INCHES NOMINAL |
| SFTT | Surface Treatment | PASSIVATE OVERALL |
| CWCD | Nominal Outside Diameter | 4.062 INCHES |
| CMLK | Mounting Hole Thread Series Designator | UNJF AXIALLY THROUGH BODY, FIRST END |
| CWRS | Bore Nominal Diameter | 0.787 INCHES BOTH ENDS |
| AGAV | End Item Identification | AIRCRAFT, AIRLIFTER C-17A |
| ABSX | Attachment Method | MOUNTING HOLE |
| CQLT | Mounting Hole Nominal Thread Size | 0.112 INCHES AXIALLY THROUGH BODY, FIRST END |
| STDC | Surface Treatment Document And Classification | QQ-P-35 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| MDCL | Material Document And Classification | AMS5659 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| CWQL | Nominal Distance Between Body Face And Protruding Hub End | 0.031 INCHES FIRST END |
| AAQL | Body Style | WEBBED, OFFSET, SOLID |
| MATT | Material | STEEL COMP XM-12 OVERALL |
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