Part Details | LANDING GEAR CYLINDER AND PISTON ASSEMBLY
1620-01-053-0501 The main shock absorption portion of an aircraft landing gear, consisting of the main cylinder and piston and other associated parts. May be with or without axle(s). Excludes LANDING GEAR, FIXED and LANDING GEAR, RETRACTABLE.
Alternate Parts: 64060213, 6-40602-13, 64060213, 6-40602-13, 64060213, 6-40602-13, 1620-01-053-0501, 01-053-0501, 1620010530501, 010530501
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | DEC 24, 1977 | 01-053-0501 | 61579 ( CYLINDER AND PISTON ASSEMBLY, LANDING GEAR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1620-01-053-0501
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6-40602-13 | 22915 | NORTHROP GRUMMAN CORPELECTRONIC SYSTEMS DEFENSIVE SYSTEM |
| 6-40602-13 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 6-40602-13 | 0JRC1 | NORTHROP GRUMMAN TECHNICAL SERVICES,INC. |
Technical Data | NSN 1620-01-053-0501
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | U/A: MAIN LANDING GEAR CYLINDER; ALUM ALLOY 7075-T411, 231.010IN APPROX LG, 18.332IN H, 3.126IN INSIDE BORE DIA |
| END ITEM IDENTIFICATION | T-38/F-5 AIRCRAFT |