SAE AMSP83461
Current
The latest, up-to-date edition.
Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Improved Performance at 275°F (135°C)
Hardcopy , PDF
English
01-04-1998
Important note : Users cannot be edited or removed once added to your Multi user PDF.This specification covers O-ring packings for use with petroleum based hydraulic fluids conforming to MIL-H-5606 and MIL-H-83282 over the temperature range of -65° to 275°F (-54° to 135°C).
| DevelopmentNote |
Supersedes MIL P 83461 (10/2003)
|
| DocumentType |
Standard
|
| Pages |
16
|
| PublisherName |
SAE International
|
| Status |
Current
|
This specification covers O-ring packings for use with petroleum based hydraulic fluids conforming to MIL-H-5606 and MIL-H-83282 over the temperature range of -65° to 275°F (-54° to 135°C). This material gives improved high temperature performance over materials conforming to MIL-P-25732.
| Standards | Relationship |
| MIL-P-83461 Revision B:1980 | Similar to |
| SAE ARP 5146 : 2015 | ASSESSMENT OF AIRCRAFT WHEEL SEALING SYSTEMS |
| SAE AIR1387D | Designing with Elastomers for use at Low Temperatures, Near or Below Glass Transition |
| SAE AS83461/2B | STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 RUBBER |
| MIL-STD-2003-3 Revision A:2009 | ELECTRIC PLANT INSTALLATION STANDARD METHODS FOR SURFACE SHIPS AND SUBMARINES (PENETRATIONS) |
| SAE AS83461/1B | M83461 O-RING MOLDED FROM AMS-P-83461 RUBBER |
| MIL-PRF-5503 Revision G:2013 | ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| SAE ARP5796 | Flight Critical Control Valves, Military Aircraft |
| MIL-DTL-25427 Revision B:2009 | COUPLING ASSEMBLY, HYDRAULIC, SELF SEALING, QUICK DISCONNECT, GENERAL SPECIFICATION FOR |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
| MIL-DTL-24231 Revision E:2013 | Connectors, Plugs, Receptacles, Adapters, Hull Inserts, and Hull Insert Plugs, Pressure-Proof, General Specification for |
| MIL-DTL-24127 Revision A:2016 | EDUCTORS, GASOLINE, OIL, OR WATER |
| SAE ARP4945A | Aerospace-Solenoid Valve, Hydraulic, Three Way, Two Position, Direct Acting |
| MIL-G-18997 Revision E:1991 | GAUGE, PRESSURE, DIAL INDICATING |
| MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
| SAE AS6235A | Face Seal Gland Design, Static, O-ring and Other Seals for Aerospace Hydraulic and Pneumatic Applications |
| MIL-DTL-23919 Revision C:2012 | REFERENCE CELL, IMPRESSED CURRENT CATHODIC PROTECTION (ICCP) - SILVER-SILVER CHLORIDE |
| SAE ARP1311C | Landing Gear Structures and Mechanisms |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| SAE AIR1364A | Age Control of Age Sensitive Elastomeric Materials |
| SAE AS4941B | Aerospace - General Requirements for Commercial Aircraft Hydraulic Components |
| SAE AIR4543C | Aerospace Hydraulics and Actuation Lessons Learned |
| SAE ARP4912C:2017 | DESIGN RECOMMENDATIONS FOR SPARE SEALS IN LANDING GEAR SHOCK STRUTS |
| SAE AIR786B | Elastomer Compatibility Considerations Relative to Elastomeric Sealant Selection |
| SAE ARP1311D | Landing Gear Structures and Mechanisms |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.