NSN 1710-01-184-9714 · NIIN 011849714 · FSC 1710
NO DASHES 1710011849714
In Stock
ACTUATOR,HYDRAULIC
Aircraft Landing Equipment
Application: HELICOPTER LANDING SYSTEM
Technical characteristics
9 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABHP | OVERALL LENGTH | INCHES NOMINAL 10.630 |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 2.000 |
| AGAV | END ITEM IDENTIFICATION | HELICOPTER LANDING SYSTEM |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ACTUATOR-HYDRAULIC RSD RAST SYSTEM |
| FTLD | FUNCTIONAL DESCRIPTION | MATERIALS: ACTUATOR CYLINDER - CARBON OR ALLOY STEEL TUBING; MANDREL DRAWN: ASTM A513/A513M GR 1015-1026 |
| SPCL | SPECIAL TEST FEATURES | HYDRAULICS WORKING PRESSURE: 3000PSI; PROOF PRESSURE: 4500PSI; LEAK RATE: 1 DROP PER 25 CYCLE MAXIMUM ; BORE SIZE: 1.25 NOMINAL; ROD SIZE: 0.750 NOMINAL; STROKE: 1.12 + OR - 0.02" |
| SUPP | SUPPLEMENTARY FEATURES | ITEM WHEN INSTALLED SHALL MEET THE TEMPERATURE (EXPOSED EQUIPMENT), SHOCK (GRADE A), VIBRATION AND SALT FOG REQUIREMENTS OF MIL-R-85111 (AS) PARAGRAPH 3.4.5 AND MAXIMUM FLUID TEMPERATURE RANGE OF -40 DEGREES TO +200 DEGREES FAHRENHEIT |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | UNIT WEIGHT: 6.45LBS |
| ZZZK | SPECIFICATION/STANDARD DATA | PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD 05047-AS-E Y14.100 |