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| Mfg Part Number: 167251-5 | Alternate P/N: 1672515 | NSN : 1620-00-105-1580 |
| NIIN : 001051580 | CAGE Code : 55284 | Manufacturer: Honeywell Aerospace |
| Item Name : Landing Gear Retractable | FSC : 1620 Aircraft Landing Gear Components |
We at Integrated Purchasing are here to help you secure top quality Landing Gear Retractable parts like 167251-5. This particular NSN component is listed alongside the part number 167251-5, having been manufactured by Honeywell Aerospace. Reach out by filling out an RFQ for a timely quote and please let us know your desired quantity, price, and shipping time frame so we can make the purchasing process as efficient as possible to meet your specific needs. We have experts working around-the-clock and guarantee a response to your completed form within 15 minutes.
In addition to NSN 1620-00-105-1580, we offer a vast inventory of parts at competitive pricing. We understand the importance of fully informed purchasing and therefore list every item with all applicable information. For example, you can find NSN 1620-00-105-1580 and part number 167251-5 which are manufactured by Honeywell Aerospace under the CAGE Code 55284. Let us provide you with any information you require in a timely and detailed manner. We have experts working around-the-clock to answer any questions in addition to quotes. Do not hesitate to contact us and allow Integrated Purchasing to do the work for your sourcing, logistics, shipments, and quality so that you can focus on building. Call or email us today to get started!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1620-00-105-1580 Item Description: Landing Gear Retractable | 1620 | 001051580 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 167251-5 | 2 | 1 | C | A |
| 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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