SAE AS5440A
Current
Current
The latest, up-to-date edition.
Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For
Published date
03-01-2011
Publisher
Sorry this product is not available in your region.
Provides the design and installation requirements for Types I and II military aircraft hydraulic systems.
DevelopmentNote |
REPLACES MIL-H-5440H
|
DocumentType |
Standard
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
This specification covers the design and installation requirements for Types I and II military aircraft hydraulic systems.
SAE ARP4493A | Aerospace - Direct Drive Servovalves |
SAE AIR5699 | A Guide for the Damaging Effects of Tire and Wheel Failures |
SAE ARP994B | Design of Tubing Installations for Aerospace Hydraulic Systems |
SAE ARP94910 | Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For |
DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-DTL-5523 Revision E:2011 | VALVE; RELIEF, HYDRAULIC PRESSURE |
DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
SAE ARP4378C | Accumulator, Hydraulic, Welded Bellows, Factory Pre-Charged |
SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
MIL-PRF-5503 Revision G:2013 | ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
SAE ARP5796 | Flight Critical Control Valves, Military Aircraft |
SAE AS85720B | Fittings, Tube, Fluid Systems, Separable, High Pressure Beam Seal, 5000/8000 psi, General Specification For |
SAE ARP1802B | Selection and Application of Polytetrafluoroethylene (PTFE and TFE) Backup Rings for Hydraulic and Pneumatic Fluid Power Applications |
SAE ARP4945A | Aerospace-Solenoid Valve, Hydraulic, Three Way, Two Position, Direct Acting |
SAE AIR 5992 : 2015 | DESCRIPTIONS OF SYSTEMS INTEGRATION TEST RIGS (IRON BIRDS) FOR AEROSPACE APPLICATIONS |
MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
SAE AIR560C | Missile Hydraulic Pumps |
MIL-DTL-19068 Revision B:2006 | VALVES, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 2 SYSTEMS |
SAE AS5586 | Aerospace - General Requirements for Hydraulic System Reservoirs |
SAE AS19692B | Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
SAE AS85421A | Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification For |
SAE AIR 1922 : 2017 | AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
SAE ARP5891 | Achieving Cleanliness Standards for Aircraft Hydraulic Systems During Manufacture |
SAE AS1709A | Coupling Assembly, Hydraulic Self Sealing, Quick Disconnect |
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
SAE ARP584D | Coiled Tubing - Corrosion Resistant Steel, Hydraulic Applications, Aerospace |
MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
SAE ARP4386D | Terminology and Definitions for Aerospace Fluid Power, Actuation and Control Technologies |
SAE AIR 5829 : 2008 | AIR IN AIRCRAFT HYDRAULIC SYSTEMS |
JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
MIL-PRF-32287 Revision A:2011 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT |
MIL PRF 0032287 : 0 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT |
SAE ARP6200 | Test Requirements and Means for Commercial Aircraft Hydraulic Systems |
SAE ARP4146C | Coiled Tubing – Titanium Alloy, Hydraulic Applications, Aerospace |
SAE ARP4752B | Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems |
SAE J1782_201305 | Ship Systems and Equipment - Hydraulic Systems - Noise Control |
MIL-DTL-5508 Revision C:2007 | FUSES, AIRCRAFT AUTOMATIC QUANTITY-MEASURING, HYDRAULIC |
SAE AIR737F | Aerospace Hydraulic and Pneumatic Specifications, Standards, Recommended Practices, and Information Reports |
SAE AIR4094A | Aircraft Flight Control Systems Descriptions |
SAE AIR 5451 : 2017 | A GUIDE TO LANDING GEAR SYSTEM INTEGRATION |
SAE ARP5555 | Recommendations for Installation of Seals in Standard Glands |
SAE AS94900 | Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For |
SAE ARP5794 | Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard |
SAE ARP4925B | Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems |
SAE AIR4543C | Aerospace Hydraulics and Actuation Lessons Learned |
SAE ARP 4379 : 2016 | AEROSPACE - ACCUMULATOR, HYDRAULIC, CYLINDRICAL, PISTON SEPARATED |
SAE ARP 988 : 2016 | ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |
SAE ARP994C | Design of Tubing Installations for Aerospace Hydraulic Systems |
SAE AIR5992 | Descriptions of Systems Integration Test Rigs (Iron Birds) for Aerospace Applications |
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.