NSN 1620-01-242-9594
Part Details | LANDING GEAR DIRECT ACTION SHOCK ABSORBER
1620-01-242-9594 A pneumatically or hydraulically damped coupling used to absorb forces generated by the contact of aircraft landing gear with a landing surface.
Alternate Parts: 74A4108501009, 74A410850-1009, 74A4108501009, 74A410850-1009, 74A4108501009, 74A410850-1009, 74A4108501009, 74A410850-1009, X74A4108501009, X74A410850-1009, 74A4108501009, 74A410850-1009, 10349265, 1620-01-242-9594, 01-242-9594, 1620012429594, 012429594
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | OCT 20, 1986 | 01-242-9594 | 38261 ( SHOCK ABSORBER, DIRECT ACTION, LANDING GEAR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1620-01-242-9594
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 74A410850-1009 | 32168 | ALL TOOLS INC.DBA E2 PRECISION PRODUCTS |
| 74A410850-1009 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 74A410850-1009 | 13002 | GOODRICH CORPORATIONDBA GOODRICH LANDING GEAR DIVISION |
| 74A410850-1009 | 5ZSC8 | HDI LANDING GEAR USA, INC.DBA HEROUX DEVTEK LANDING GEAR DIV |
| X74A410850-1009 | 85941 | MAGELLAN AEROSPACE, NEW YORK, INC. |
| 74A410850-1009 | 2M490 | NASSAU TOOL WORKS, INC. |
| 10349265 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
Technical Data | NSN 1620-01-242-9594
| Characteristic | Specifications |
|---|---|
| OPERATION METHOD | HYDRAULIC |
| HYDRAULIC SYSTEM FLUID CAPACITY | 183.0 CUBIC INCHES |
| FILLER PLUG | INCLUDED |
| SIDE ATTACHED FLUID TANK | NOT INCLUDED |
| COMPRESSED LENGTH | 22.280 INCHES NOMINAL |
| EXTENDED LENGTH | 35.400 INCHES NOMINAL |
| SPECIAL FEATURES | STROKE TOTAL 13.12 INCHES,PRIMARY CHAMBER 13.12 INCHES,SECONDARY CHAMBER 4.25 INCHES;WEIGHT-FILLED APPROXIMATE 62 POUNDS;FLUID MEDIUM-MIL-H-83282;PRESSURIZING AGENT (DRY NITROGEN)-MIL-P-27401;TEMPERATURE RANGE (AMBIENT) -65 DEGREES TO 270 DEGREES F;SERVICE PRESSURE RANGE (NOMINAL INTERNAL NITROGEN PRESSURE) WEIGHT OFF WHEELS TO MAX,AIRCRAFT TAKE OFF WEIGHT-51,900 LBS;PRIMARY (LOW PRESSURE) CHAMBER 150 TO 1,570 PSIG; SECONDARY (HIGH PRESSURE) CHAMBER 1,290 TO 2,960 PSIG;PROOF PRESSURE (OPERATING LIMIT) PRIMARY CHAMBER 14,770 PSIG;SECONDARY CHAMBER 9,472 PSIG |
| END ITEM IDENTIFICATION | USED ON (NON HSP) FIGHTER SUPPORT AIRCRAFT F/A-18 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NAVAIR TECH MANUAL-MAIN LANDING GEAR SHOCK ABSORBER ASSEMBLY-A1-421AC-150-000 |