NSN 1620-00-105-1580 of Landing Gear Retractable - Parts Details
| Alternative NSN: 1620001051580 |
| Item Name: Landing Gear Retractable |
| FSG: 16 Aircraft Components and Accessories |
| Federal Supply Class (FSC): 1620 Aircraft Landing Gear Components |
| NIIN: 001051580 |
| NCB Code: USA (00) |
| Manufacturers: Goodrich Corporation , Honeywell International Inc |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers 172953, 167251-9, 167251-7, 167251-5 under NSN 1620-00-105-1580 of Landing Gear Retractable manufactured by Goodrich Corporation, Honeywell International Inc.
Federal Supply Class of NSN 1620-00-105-1580 is FSC 1620 contains part details of Aircraft Landing Gear Components. Quote for your desired part numbers.
Part Number's List for NSN 1620-00-105-1580, 1620001051580
-
Part No Manufacturer Item Name QTY RFQ 172953 Goodrich Corporation landing gear retractable Avl RFQ 172953 Honeywell International Inc landing gear retractable Avl RFQ 167251-9 Goodrich Corporation landing gear retractable Avl RFQ 167251-9 Honeywell International Inc landing gear retractable Avl RFQ 167251-7 Honeywell International Inc landing gear retractable Avl RFQ 167251-7 Goodrich Corporation landing gear retractable Avl RFQ 167251-5 Honeywell International Inc landing gear retractable Avl RFQ
Characteristics Data of NSN 1620001051580MRC 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
| 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 |