You have reached the Request for Quote (RFQ) page for part number 71202-22207-102, an item sourced from Sikorsky Aircraft Corporation (CAGE Code 78286) that is classified with the item name Stringer Aircraft. Here, you can utilize our online form to quickly secure tailored pricing and procurement options from our staff as the first step of procurement. With responses always being quick, be sure to get started as soon as possible if you would like to learn more about this part number.
The part number 71202-22207-102 is associated with Sikorsky Aircraft Corporation, identified by the CAGE Code 78286, and is typically referenced under the item name Stringer Aircraft. It is categorized under the NSN 1560-01-564-4342, with the NIIN 015644342, INC 41030, and NCB code 01 (USA). Additionally, this part falls under the Federal Supply Group (FSG) 15 and Federal Supply Class (FSC) 1560 Airframe Structural Components. For more information, these classifications provide further context about the component.
With the form provided, be sure to present our staff with key details on your needs, such as your target pricing, required quantity, and expected turnaround time. Once we receive and review your request for part 71202-22207-102, a member of our staff will contact you in 15 minutes or less to present customized solutions for your comparisons. Once you make a purchase with us, you can expect our staff to work closely with you through each step of fulfillment to ensure that all needs are met with care and efficiency.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-564-4342 Item PartTypeName: STRINGER,AIRCRAFT | 1560 | 015644342 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 71202-22207-102 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| FEAT | Special Features | J SHAPED STRINGER HAVING 89 DEGREE ANGLE ON LARGER SIDE CONNECTION AND 91 DEGREE ANGLE ON SHORTER SIDE CONNECTION; HAVING TWO THRU HOLES LOCATED AT 5.000 AND 15.970 INCHES FROM LEFT END; ALSO HAVING TWO ADDITIONAL THRU HOLES LOCATED BETWEEN LEFT END AND THE 5.000 INCH HOLE; LARGER SIDE PORTION HAS 21 THRU HOLES EVENLY SPACED BETWEEN THE BENDS IN THE STRINGER |
| AGAV | End Item Identification | MH60 |
| CZEJ | Aircraft Station Number | WL261.20 AND WL256.70 |
| MDCL | Material Document And Classification | AMS-QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE |
| CXCY | Part Name Assigned By Controlling Agency | (INAVY)STRINGER INSTALLATIOON, SIDE FUSELAGE |
| CZEK | Aircraft Mission Design Series | MH60 |
| MRC | Decoded Requirement | Clear Text Reply |
| MATT | Material | ALUMINUM ALLOY 7075 |
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