You have reached the Request for Quote (RFQ) page for part number 167251-6, an item sourced from Goodrich Corporation (CAGE Code 13002) that is classified with the item name Landing Gear Retractable. 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.
Important Details for Part Number 167251-6
The part number 167251-6 is associated with Goodrich Corporation, identified by the CAGE Code 13002, and is typically referenced under the item name Landing Gear Retractable. It is categorized under the NSN 1620-00-105-1581, with the NIIN 001051581, INC 60672, and NCB code 00 (USA). Additionally, this part falls under the Federal Supply Group (FSG) 16 and Federal Supply Class (FSC) 1620 Aircraft Landing Gear 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 167251-6, 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 |
|---|---|---|---|---|---|---|
| 1620-00-105-1581 Item PartTypeName: LANDING GEAR,RETRACTABLE | 1620 | 001051581 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 167251-8 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ADAY | WHEEL QUANTITY ACCOMMODATED | 1 |
| ADBT | LANDING SHOCK ABSORPTION AND DISSIPATION METHOD | AIR/OIL SHOCK STRUT |
| ADBU | GEAR EXTENSION AND RETRACTION METHOD | HYDRAULIC CYLINDER |
| APGF | DESIGN TYPE | MAIN LANDING GEAR |
| BXFZ | AIRCRAFT FOR WHICH DESIGNED | T-37 |
| FEAT | SPECIAL FEATURES | CYL AND PISTON ASSY 1,TORQUE ARM 2,EXTENDED LG 31.711 IN.,COMPRESSED LG 23.211 IN.,RIGHT HAND |
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