NSN 1620-01-151-8137
Part Details | LANDING GEAR DIRECT ACTION SHOCK ABSORBER
1620-01-151-8137 A pneumatically or hydraulically damped coupling used to absorb forces generated by the contact of aircraft landing gear with a landing surface.
Alternate Parts: 74A4108501005, 74A410850-1005, 1620-01-151-8137, 01-151-8137, 1620011518137, 011518137
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | APR 22, 1983 | 01-151-8137 | 38261 ( SHOCK ABSORBER, DIRECT ACTION, LANDING GEAR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1620-01-151-8137
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 74A410850-1005 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 1620-01-151-8137
| 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 |