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Aerospace - Commercial Aircraft Hydraulic Systems

A-6A1 Commercial Aircraft Committee
  • Aerospace Standard
  • AIR5005A
  • Current
Published 2015-09-21 by SAE International in United States
This SAE Aerospace Information Report (AIR) has been compiled to provide information on hydraulic systems fitted to commercial aircraft. Data has been provided for following aircraft types: a Wide body jet airliners b Narrow body jet airliners c Turboprop/commuter aircraft d Business jet aircraft The airliners that have been included in this document are generally in operational service with either airlines or cargo operators. Information on aircraft that have been retired from in-service use has been included for reference purposes. No information is presented for aircraft that are currently being developed. The following information is provided for each aircraft Design requirements: Governing airworthiness regulations System pressure: Fluid power system operating pressure Hydraulic fluid: Type of fluid the hydraulic system uses Number of hydraulic systems: Number and identification of independent hydraulic systems System temperature: Minimum and maximum design operating temperatures Main hydraulic pump data: Flow, pressure, displacement Auxiliary pump data: System auxiliary pump or back-up data Hydraulic motor data: System hydraulic motor requirements Accumulator data: Usage, volume and precharge requirements Reservoir data: Type, volume and pressure…
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Aerospace - Lightning Effects on Hydraulic Transport Elements on Aircraft

A-6A1 Commercial Aircraft Committee
  • Aerospace Standard
  • AIR6185
  • Current
Published 2015-08-28 by SAE International in United States
This SAE Aerospace Information Report (AIR) describes hydraulic system design and installation to minimize the effects of lightning, especially when the aircraft structure is composite. Techniques for effective electrical bonding, hydraulic system lightning protection, and lightning protection verification techniques are discussed.
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Aerospace - General Requirements for Commercial Aircraft Hydraulic Components

A-6A1 Commercial Aircraft Committee
  • Aerospace Standard
  • AS4941B
  • Current
Published 2015-03-09 by SAE International in United States
This SAE Aerospace Standard (AS) provides general requirements for components that are used in commercial aircraft hydraulic systems. It also includes the 14 CFR Part 25/CS 25 regulations that apply to hydraulic components. It also provides information to be included in the Procurement Specification in Appendix A and a checklist for design reviews in Appendix B. It does not provide requirements for distribution elements such as hoses, pipe fittings and general tubing.
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Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems

A-6A1 Commercial Aircraft Committee
  • Aerospace Standard
  • ARP4925B
  • Current
Published 2014-10-09 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a commercial transport rotorcraft hydraulic system, including the applicable airworthiness regulations that affect the hydraulic system. This ARP also provides information and guidelines on the many factors that arise in the design process to provide cost effectiveness, reliability, maintainability and accepted design and installation practices.
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Test Requirements and Means for Commercial Aircraft Hydraulic Systems

A-6A1 Commercial Aircraft Committee
  • Aerospace Standard
  • ARP6200
  • Current
Published 2014-10-08 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) describes the recommended tests and their associated test means for commercial aircraft hydraulic systems at the system level that are required to demonstrate compliance with the 14 CFR Part 25 and EASA CS 25 airworthiness regulations, and to show that the required level of maturity at the aircraft entry into service (EIS) has been achieved.
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Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems

A-6A1 Commercial Aircraft Committee
  • Aerospace Standard
  • ARP4752B
  • Current
Published 2013-12-02 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) provides guidance for the design and installation of a commercial aircraft hydraulic system to meet the applicable requirements, including the applicable airworthiness regulations that affect the hydraulic system design. This ARP also provides information and guidelines on the many factors that arise in the design process to provide cost effectiveness, reliability, maintainability and accepted design and installation practices.
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Aerospace Fluid Power - FAA Regulatory History - Transport Airplane Hydraulic Systems

A-6A1 Commercial Aircraft Committee
  • Aerospace Standard
  • AIR5696
  • Current
Published 2013-11-22 by SAE International in United States
This SAE Aerospace Information Report (AIR) contains regulatory and guidance information related to transport airplane hydraulic systems. It contains certain Civil Air Regulations (CAR) and Federal Aviation Regulations (formerly referred to as FARs) from Title 14 Code of Federal Regulations (CFR) in their current version as well as the historical versions. This gives the reader an ability to assemble certain CAR/CFR parts as they existed at any date in the past (referred to as a Regulatory Basis). A certain amount of preamble explanatory material is included, which led to the regulatory rule changes (Amendments to the CFR).
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External Hydraulic Leakage for In-Service Components

A-6A1 Commercial Aircraft Committee
  • Aerospace Standard
  • ARP1084A
  • Current
Published 2013-10-04 by SAE International in United States
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide guide lines for allowable leakage for in-service aircraft hydraulic components at a nominal 100 °F (38 °C) temperature and to outline the procedure for measuring such leakage. The limits to be applied to any specific aircraft should be adjusted before inclusion in a maintenance manual.
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Placarding of Aircraft Hydraulic Equipment to Identify Phosphate Ester Fluid Compatibility

A-6A1 Commercial Aircraft Committee
  • Aerospace Standard
  • ARP1288B
  • Current
Published 2012-07-11 by SAE International in United States
This ARP defines a recommended placard for readily identifying equipment with aircraft phosphate ester fluid to be used in the aircraft hydraulic systems to assure compatibility between the internal seals/materials and the system fluid. A definition is provided for a durable type and semipermanently attached placard with prescribed text for the permissible fluid are included in the document.
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Inspection of Inservice Airborne Accumulators for Corrosion and Damage

A-6A1 Commercial Aircraft Committee
  • Aerospace Standard
  • AIR4150A
  • Current
Published 2009-01-06 by SAE International in United States
This document has been declared "CANCELLED" as of January 2009 and has been superseded by ARP4150. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by ARP4150.