NSN 1620-01-171-3371
Part Details | LANDING GEAR CYLINDER AND PISTON ASSEMBLY
1620-01-171-3371 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: 810AS1500, AJ159237A, AJ159237, 1J3L147, 1J-3L147, 1620-01-171-3371, 01-171-3371, 1620011713371, 011713371
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | FEB 06, 1984 | 01-171-3371 | 61579 ( CYLINDER AND PISTON ASSEMBLY, LANDING GEAR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1620-01-171-3371
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 810AS1500 | 30003 | NAVAL AIR SYSTEMS COMMAND MANAGEDORIGINAL DESIGN ACTIVITY NOT |
| AJ159237A | 84561 | PARKER-HANNIFIN CORPORATIONDBA CYLINDER DIV |
| AJ159237 | 84561 | PARKER-HANNIFIN CORPORATIONDBA CYLINDER DIV |
| 1J-3L147 | 84561 | PARKER-HANNIFIN CORPORATIONDBA CYLINDER DIV |
Technical Data | NSN 1620-01-171-3371
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | STEEL CYLINDER BODY,AMS 5082; STEEL HEADS,CAPS,TIE RODS; AND PISTON ROD; PISTON ROD CASE HARDENED TO ROCKWELL C54, AND CHROME PLATED PER QQ-C-320, CL 2,TY 1; 1.000 IN. CYLINDER BORE; 10.880 IN. BODY LG; 12.000 IN. APPROX LG O/A; 5/16-24 UNF 2A THD CONNECTION END ON PISTON ROD; RECTANGULAR MTG FLANGE; FOUR 0.250 IN. DIA MTG HOLES; HOLES SPACED 2.000 IN. C TO C ALONG LG, AND 1.080 IN. ACROSS W; 2.500 IN. LG BY 1.500 IN. W BY 0.370 IN. MTG FLANGE THICKNESS |