You are currently exploring our in-stock options for part number 167251-5 with the NSN 1620001051580. This product is listed with the description “Landing Gear Retractable” and is manufactured by Honeywell International Inc. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number 167251-5 is listed alongside the NSN 1620-00-105-1580 and belongs to the FSC 1620 Aircraft Landing Gear Components. Additionally, it is also under the CAGE Code 55284, which is assigned to Honeywell International Inc. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number 167251-5 seamless.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1620-00-105-1580 Item PartTypeName: LANDING GEAR,RETRACTABLE | 1620 | 001051580 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 167251-7 | 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.,LEFT HAND |
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