SAE AIR4543C
Current
The latest, up-to-date edition.
Aerospace Hydraulics and Actuation Lessons Learned
Hardcopy , PDF
English
09-02-2017
1. SCOPE
2. REFERENCES
3. TECHNICAL INFORMATION
4. NOTES
Provides Lessons Learned from aerospace actuation, control and fluid power systems technologies.
DocumentType |
Standard
|
Pages |
111
|
ProductNote |
This version is stabilized
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
This SAE Aerospace Information Report (AIR) contains Lessons Learned from aerospace actuation, control and fluid power systems technologies. The lessons were prepared by engineers from the aerospace industry and government services as part of SAE Committee A-6, Aerospace Fluid Power, Actuation, and Control Technologies, and were presented to the A-6 during meetings held from 1989 through 1999. The document is organized into five sections covering systems, actuation, hydromechanical components, electrical components and miscellaneous, each further divided into subsections. The lessons are presented in a concise format of Problem, Issue, Solution and Lesson Learned, often with accompanying descriptive diagrams and illustrations for clarity and understanding.Because of the potential growth in the size of the document as new lessons are published, those presented to the A-6 Committee in 2000 and later years are planned to be released in separate slash number documents, AIR4543/1, AIR4543/2 and so on.
SAE ARP5796 | Flight Critical Control Valves, Military Aircraft |
SAE AS4941B | Aerospace - General Requirements for Commercial Aircraft Hydraulic Components |
SAE AIR 1922 : 2017 | AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
SAE ARP4763 | Aerospace - General Requirements for Hydraulic Relief Valves |
SAE AS5586 | Aerospace - General Requirements for Hydraulic System Reservoirs |
SAE ARP4752B | Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems |
SAE ARP 4379 : 2016 | AEROSPACE - ACCUMULATOR, HYDRAULIC, CYLINDRICAL, PISTON SEPARATED |
SAE AS4716B | Gland Design, O-ring and Other Elastomeric Seals |
SAE AIR1569A | Handling and Installation Practice for Aerospace Hose Assemblies |
SAE AS620G | Hose Assemblies, Convoluted Polytetrafluoroethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft |
MIL-PRF-6083 Revision G:2013 | HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
MIL-PRF-46170 Revision E:2013 | HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544 |
MIL-F-8815-2 Revision A:1975 | FILTER, FLUID, PRESSURE, HYDRAULIC LINE, 3000 PSI, ABSOLUTE 15 MICRON, STYLE B, NON BYPASS, -65 DEGREES TO +275 DEGREES F |
SAE ARP4553A | Aerospace - Accumulator, Hydraulic, Self-Displacing |
SAE AS4623E | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3,000 psi, 275 °F, Heavy Duty, Aircraft Hydraulic Systems |
SAE ARP 4379 : 2016 | AEROSPACE - ACCUMULATOR, HYDRAULIC, CYLINDRICAL, PISTON SEPARATED |
MIL-R-83485 Base Document:1976 | RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES |
SAE AS28775A | PACKING, PREFORMED - MS28775 O-RING |
MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
NAS1638:2011 | CLEANLINESS REQUIREMENTS OF PARTS USED IN HYDRAULIC SYSTEMS |
MS27595 Revision E:2006 | RETAINER, PACKING BACKUP, CONTINUOUS RING, POLYTETRAFLUOROETHYLENE |
MIL-P-87175 Base Document:1982 | PACKING, PREFORMED, PETROLEUM, HYDRAULIC FLUID RESISTANT, PHOSPHONITRILIC FLUOROELASTOMER |
MIL-PRF-17331 Revision K:2013 | LUBRICATING OIL, STEAM TURBINE AND GEAR, MODERATE SERVICE |
SAE AMSR83485A | Rubber, Fluorocarbon Elastomer, Improved Perfrormance At Low Temperatures |
SAE AS5440A | Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For |
SAE AMSP83461 | Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Improved Performance at 275°F (135°C) |
MS28774 Revision M:2009 | RETAINER, PACKING BACKUP, SINGLE TURN, POLYTETRAFLUOROETHYLENE |
MIL-PRF-680 Revision C:2010 | DEGREASING SOLVENT |
MIL F 24402 : E | FILTER, FILTER ELEMENTS (25 MICROMETER ABSOLUTE), AND FILTER DIFFERENTIAL PRESSURE INDICATORS |
MS28775 Revision E:1984 | PACKING, PREFORMED, HYDRAULIC, PLUS 275 DEG. F. (O RING) |
MIL-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
SAE AS83461/2B | STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 RUBBER |
SAE AIR1243D | Anti Blow-By Design Practice for Cap Seals |
MIL-G-5514 Revision G:1993 | GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR |
MIL R 25988 : B | RUBBER, FLUOROSILICONE ELASTOMER, OIL AND FUEL RESISTANT, SHEETS, STRIPS, MOLDED PARTS AND EXTRUDED SHAPES |
SAE ARP4378C | Accumulator, Hydraulic, Welded Bellows, Factory Pre-Charged |
SAE ARP 4150 : 1996 | PROCEDURE FOR INSPECTION OF INSERVICE AIRBORNE ACCUMULATORS FOR CORROSION DAMAGE |
SAE AS83461/1B | M83461 O-RING MOLDED FROM AMS-P-83461 RUBBER |
MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
MIL-PRF-81836 Revision B:1998 | FILTER AND DISPOSABLE ELEMENT, FLUID PRESSURE, HYDRAULIC, 3 MICRON ABSOLUTE |
SAE AIR4150A | Inspection of Inservice Airborne Accumulators for Corrosion and Damage |
SAE AS 8775 : 1998 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
MIL F 8815 : D | FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
SAE AS1339G | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Lightweight, Hydraulic and Pneumatic |
SAE AS 4059F : 2013 | AEROSPACE FLUID POWER - CONTAMINATION CLASSIFICATION FOR HYDRAULIC FLUIDS |
MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
MIL-DTL-5498 Revision G:2013 | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
MIL-P-83461 Revision B:1980 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C) |
SAE AS604E | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Heavyweight, Hydraulic |
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