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Arpolube Hydraulic Fluids
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ARPOL AIR 5606
U.S. MILITARY SPECIFICATION: MIL-H-5606G
NATO: H-515
HYDRAULIC FLUID, PETROLEUM BASE, AIRCRAFT MISSILE AND ORDNANCE
A BLEND OF THE HIGHEST QUALITY, LOW VISCOSITY, NAPTHENIC BASE STOCKS WITH A HIGHLY SHEAR STABLE VISCOSITY INDEX IMPROVER AND SELECTED ADDITIVES. FORMULATION OFFERS A PRODUCT WITH EXCEPTIONALLY GOOD VISCOSITY TEMPERATURE CHARACTERISTICS, CONTROLLED RUBBER SWELL, EXCELLENT OXIDATION STABILITY AND GOOD ANTI-WEAR PROPERTIES.
INTENDED FOR USE IN AUTOMATIC PILOTS, SHOCK ABSORBERS, SHOCK STRUTS, BRAKES, FLAP CONTROL MECHANISMS, MISSILE HYDRAULIC SERVO-CONTROLLED SYSTEMS, AND OTHER HYDRAULIC SYSTEMS USING COMPATIBLE ELASTOMERS AND SEALS.
ARPOLUBE 6083
U.S. MILITARY SPECIFICATION: MIL-PRF-6083F
NATO: C-635
HYDRAULIC FLUID PETROLEUM BASE FOR PRESERVATION AND OPERATION.
A PETROLEUM BASE, LOW VISCOSITY, HYDRAULIC AND PRESERVATIVE FLUID FOR AIRCRAFT AND ORDNANCE USE. A BLEND OF SELECTED PETROLEUM OILS WITH ADDITIVES TO GIVE A PRODUCT WITH EXCEPTIONALLY GOOD VISCOSITY-TEMPERATURE CHARACTERISTICS, GOOD ANTI-WEAR PROPERTIES, CONTROLLED RUBBER SWELL, GOOD SHEAR STABILITY AND EXCELLENT OXIDATION RESISTANCE.
INTENDED FOR USE IN AIRCRAFT, ORDNANCE AND OTHER GENERAL HYDRAULIC USE, AND FOR PRESERVING HYDRAULIC COMPONENTS, IT IS USED IN ACCEPTANCE TESTING OF HYDRAULIC COMPONENT INTENDED FOR USE IN MIL-H-5606 SERVICE.
ARPOLUBE 46170
U.S. MILITARY SPECIFICATION: MIL-H-46170B AM.2 TY 1
NATO: H-544
AN UNDYED SYNTHETIC HYDROCARBON BASED HYDRAULIC FLUID. INTENDED FOR USE IN TANK RECOIL MECHANISMS AND HYDRAULIC SYSTEMS, THIS PRODUCT HAS EXCELLENT FIRE, CORROSION AND RUST PREVENTION CHARACTERISTICS.
ARPOLUBE 83282
U.S. MILITARY SPECIFICATION: MIL-PRF-83282D AM.1
NATO: H-537
A BLEND OF SYNTHETIC HYDROCARBONS, THE FINEST LUBRICANT GRADE DIESTER AND SELECTED ADDITIVES. FORMULATION OFFERS A PRODUCT WITH EXCEPTIONALLY GOOD VISCOSITY-TEMPERATURE CHARACTERISTICS, COMPLETE SHEAR STABILITY, CONTROLLED RUBBER SWELL, EXCELLENT OXIDATION STABILITY, AND GOOD ANTI-WEAR PROPERTIES. IS RECOMMENDED IN CLOSED AIRLESS SYSTEMS FROM -65 DEGREE F TO +275 DEGREE F AND IN OPEN SYSTEMS UP TO +225 DEGREE F.
INTENDED FOR USE IN AUTOMATIC PILOTS, SHOCK ABSORBERS, SHOCK STRUTS, BRAKES, FLAP CONTROL MECHANISMS, MISSILE HYDRAULIC SERVO-CONTROLLED SYSTEMS, AND OTHER HYDRAULIC SYSTEMS USING COMPATIBLE ELASTOMERS AND SEALS.
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